U.S. patent number 3,610,163 [Application Number 05/012,233] was granted by the patent office on 1971-10-05 for high-speed ground transportation system.
This patent grant is currently assigned to Tube Transit Corp.. Invention is credited to Lawrence K. Edwards, Bruce E. Skov.
United States Patent |
3,610,163 |
Edwards , et al. |
October 5, 1971 |
HIGH-SPEED GROUND TRANSPORTATION SYSTEM
Abstract
A high-speed ground transportation system comprising a tube
through which a vehicle is adapted for propulsion from a first
station to a second station, the tube having an entrance valve
adjacent the first station and an exit valve adjacent the second
station adapted, when closed, to block off an evacuated section of
the tube from valve-to-valve. Each valve comprises a toroidal
cylinder and a gate constituted by a piston movable between a
closed position blocking the tube, in which the piston extends out
of an open end of the cylinder, and an open position clearing the
tube, in which the piston is withdrawn into the cylinder. The gate
of the entrance valve is actuated by vacuum derived from the tube;
the gate of the exit valve is automatically opened and is closed by
action of atmospheric air.
Inventors: |
Edwards; Lawrence K. (Palo
Alto, CA), Skov; Bruce E. (Palo Alto, CA) |
Assignee: |
Tube Transit Corp. (Palo Alto,
CA)
|
Family
ID: |
21753984 |
Appl.
No.: |
05/012,233 |
Filed: |
February 18, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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710582 |
Mar 5, 1968 |
|
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Current U.S.
Class: |
104/156; 137/527;
251/44 |
Current CPC
Class: |
B61B
13/122 (20130101); Y10T 137/7898 (20150401) |
Current International
Class: |
B61B
13/12 (20060101); B61b 013/10 (); F16k
001/20 () |
Field of
Search: |
;104/138,156 ;137/527
;251/44 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Hoffman; Drayton E.
Parent Case Text
CROSS-REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of our copending U.S.
Pat. application Ser. No. 710,582 filed Mar. 5, 1968, now
abandoned, entitled High-Speed Ground Transportation System.
Claims
What is claimed is:
1. In a high-speed ground transportation system having an evacuated
tube adapted for propulsion of a vehicle therethrough, a station
for the vehicle in communication with the earth's atmosphere, and a
valve for the tube adjacent the station, said valve comprising a
toroidal cylinder on the outside of the tube having its toroidal
axis transverse to the tube, said cylinder having one end open to
the tube on that side of said axis toward the station, and a gate
constituted by a piston rotatable about said axis between a closed
position extending out of said open end of the cylinder into the
tube and blocking the tube and an open position within the cylinder
clear of the tube.
2. In a high-speed ground transportation system as set forth in
claim 1, said cylinder having a port in communication with the
atmosphere, and a check valve for said port adapted to open in the
direction for flow of air from the cylinder to the atmosphere.
3. In a high-speed ground transportation system as set forth in
claim 2, said port being located intermediate the ends of the
cylinder and being blocked by the piston as it rotates past said
port, and said cylinder having a bleed at its other end in
communication with the atmosphere for bleeding atmospheric air into
said other end of the cylinder.
4. In a high-speed ground transportation system as set forth in
claim 3, means for drawing a vacuum in the cylinder via said
port.
5. In a high-speed ground transportation system as set forth in
claim 4, said means for drawing a vacuum in the cylinder comprising
an interconnection between said port and a source of vacuum, and a
pilot valve in said interconnection.
6. In a high-speed ground transportation system as set forth in
claim 5, said source of vacuum being said tube.
7. In a high-speed ground transportation system as set forth in
claim 5, said interconnection including a check valve therein
adapted to open in the direction for flow of air from the cylinder
to said source of vacuum.
8. In a high-speed ground transportation system as set forth in
claim 5, said piston being a differential piston having an enlarged
section adjacent its end toward said other end of the cylinder
providing a pressure face facing toward said open end of the
cylinder, and means for selectively applying atmospheric air or
vacuum to said pressure face.
9. In a high-speed ground transportation system as set forth in
claim 8, said means for selectively applying atmospheric air or
vacuum to said pressure face comprising a chamber in communication
with the cylinder, and a pilot valve having a connection to the
atmosphere and a connection to said source of vacuum and adapted in
a first position to establish communication from the atmosphere to
said chamber and in a second position to establish communication
between said chamber and said source of vacuum.
10. In a high-speed ground transportation system as set forth in
claim 5, said piston being connected to an auxiliary toroidal
piston rotatable in an auxiliary toroidal cylinder, said auxiliary
cylinder having one end interconnected with said first-mentioned
cylinder, and means for selectively applying atmospheric air or
vacuum to the other end of said auxiliary cylinder.
11. In a high-speed ground transportation system as set forth in
claim 10, said means for selectively applying atmospheric air or
vacuum to said auxiliary cylinder comprising a chamber in
communication with said auxiliary cylinder, and a pilot valve
having a connection to the atmosphere and a connection to said
source of vacuum and adapted in a first position to establish
communication from the atmosphere to said chamber and in a second
position to establish communication between said chamber and said
source of vacuum.
12. In a high-speed ground transportation system as set forth in
claim 1, said tube having an enlarged section providing an annular
seat therearound engageable by the end of the piston in the tube in
the closed position of the piston.
13. In a high-speed ground transportation system as set forth in
claim 12, overcentering biasing means for the piston acting to bias
it in closing direction when the piston is in closed position and
to bias it in opening direction after the piston has swung open a
predetermined amount.
14. In a high-speed ground transportation system as set forth in
claim 12, said enlarged section of the tube being shaped so that
the piston, in swinging open away from said seat, swings through a
finite angle before communication of air is established between the
tube and the station.
15. In a high-speed ground transportation system as set forth in
claim 14, means for counterbalancing the piston with the center of
gravity of the piston and said counterbalancing means located to
overcenter as the piston swings between closed and open positions
so that the piston is biased in closing direction when in its
closed position and in opening direction after it has swung open
through said finite angle.
16. In a high-speed ground transportation system as set forth in
claim 1, said piston being of hollow toroidal form.
17. In a high-speed ground transportation system as set forth in
claim 1, said piston comprising a first member constituting a
driver and a second member constituting a cap.
18. In a high-speed ground transportation system as set forth in
claim 17, said driver and said cap each comprising a conical shell
and arranged with their apices adjacent one another and their axes
generally at right angles to one another.
19. In a high-speed ground transportation system as set forth in
claim 17, said piston being connected to an auxiliary piston
rotatable in an auxiliary toroidal cylinder, the first-mentioned
cylinder being closed at its other end, a passage having a pilot
valve therein interconnecting the tube and the first-mentioned
cylinder adjacent its said closed end, an air inlet interconnecting
said passage and the closed end of the first-mentioned cylinder
having a check valve and a pilot valve therein, said auxiliary
cylinder being open at one end and closed at the other and having a
vacuum vent adjacent its closed end having a pilot valve therein,
and relatively large atmospheric vent adjacent its closed end and
small atmospheric vent at its closed end each having a pilot valve
therein.
20. In a high-speed ground transportation system as set forth in
claim 17, said piston being connected to an auxiliary piston
rotatable in an auxiliary toroidal cylinder open at one end and
closed at the other, said first-mentioned cylinder being closed at
its other end and having an atmospheric outlet with a check valve
therein adjacent its closed end, an air inlet with a pilot valve
therein at its closed end and a bias port intermediate its ends
connected to vacuum and having a pilot valve therein, said
auxiliary cylinder having a relatively large atmospheric vent
adjacent its closed end and a relatively small atmospheric vent at
its closed end each having a pilot valve therein.
21. In a high-speed ground transportation system as set forth in
claim 17, said piston being connected to an auxiliary piston
rotatable in an auxiliary toroidal cylinder open at one end and
closed at the other, the first-mentioned cylinder being closed at
its other end, a passage having a pilot valve therein
interconnecting the tube and the first-mentioned cylinder adjacent
its said closed end, an air inlet interconnecting said passage and
the closed end of the first-mentioned cylinder having a check valve
and a pilot valve therein, said auxiliary cylinder having a vacuum
vent adjacent its closed end having a pilot valve therein, and
relatively large atmospheric vent adjacent its closed end and small
atmospheric rent at its closed end each having a pilot valve
therein, said first-mentioned cylinder having an atmospheric outlet
with a check valve therein adjacent its closed end, an air inlet
with a pilot valve therein at its closed end and a bias port
intermediate its ends connected to vacuum and having a pilot valve
therein.
Description
BACKGROUND OF THE INVENTION
The invention is in the field of high-speed ground transportation
systems particularly of the type shown in U.S. Pat. No. 3,438,337
of Lawrence K. Edwards, issued Apr. 15, 1969, entitled High-Speed
Ground Transportation System. In that patent is shown a system
comprising a duct or tube through which a vehicle is adapted for
propulsion as a free piston. Valves are provided adjacent the ends
of the tube, with stations constituted by airlocks open to the
atmosphere outward of the valves. The section of the tube between
the valves is preevacuated. With the vehicle in a first station, on
opening the respective valve acting as an entrance valve,
atmospheric air pressure on the rear of the vehicle propels it into
said section of the tube. After the vehicle has passed the entrance
valve, the latter is closed to trap a slug of air between the
entrance valve and the rear of the vehicle. This trapped slug of
air expands to apply propulsion force to the rear of the vehicle,
with attenuation of the air behind the vehicle to restore vacuum in
the tube, and with compression of air ahead of the vehicle. The
valve at the other end of said section of the tube, acting as an
exit valve, opens when the pressure ahead of the vehicle reaches a
predetermined value and the vehicle passes therethrough and stops
in the second station, the exit valve then closing. A problem
attendant upon such a system is that of providing suitable entrance
and exit valves, and this invention is directed to the solution of
this problem.
SUMMARY OF THE INVENTION
Among the several objects of this invention may be noted the
provision of a valve construction suitable for use either as an
entrance valve or exit valve in a system such as above described,
or in similar systems; the provision of such a valve construction
which, as regards its use as an entrance valve, is operated by
vacuum derived from the evacuated tube, no separate power source
for valve operation being required; the provision of such a valve
construction which, as regards its use as an exit valve, opens
automatically, no control action being required; the provision of a
valve construction such as described which, while not requiring
extensive machining of parts and therefore being economical to
construct, is adapted effectively to maintain vacuum in the tube;
and the provision of such a valve construction adapted to be
readily opened in the event of an emergency.
In general, a valve of this invention, located adjacent a station,
comprises a toroidal cylinder on the outside of the tube having its
toroidal axis transverse to the tube. As used herein, "toroidal
cylinder" refers to a toroidal cavity or void adapted to
accommodate a piston, which will be described. "Toroid" is used in
the classical sense, i.e., it need not be circular in cross
section; however, in this context the toroidal cylinder and the
toroidal piston of one embodiment of the invention are segments of
toroids rather than complete ones. This cylinder has one end open
to the tube on that side of said axis toward the station. A gate
constituted by a piston is rotatable about said axis between a
closed position extending out of said open end of the cylinder into
the tube and blocking the tube, and an open position within the
cylinder clear of the tube. Control means is provided for effecting
opening of the gate enabling use of the valve as an entrance valve.
In its use as an exit valve, the gate of the valve is adapted
automatically to open via pressure of air built up between the
front of the approaching vehicle and the gate. Other objects and
features will be in part apparent and in part pointed out
hereinafter.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGS. 1A-1E are diagrammatic views showing the operation of a
section of a high-speed ground transportation system equipped with
valves of this invention at its entrance and exit ends;
FIG. 2 is a longitudinal section of a valve of this invention, the
gate of the valve being shown in its closed position blocking the
tube;
FIG. 3 is a transverse section on line 3--3 of FIG. 2;
FIG. 4 is a view similar to FIG. 2 showing the valve in its open
position clear of the tube;
FIG. 5 is a transverse section on line 5--5 of FIG. 4;
FIG. 6 is a transverse section on line 6--6 of FIG. 2;
FIG. 7 is a perspective of the gate per se of the valve;
FIG. 8 is a longitudinal section of a modified version of the
valve;
FIG. 9 is a transverse section on line 9--9 of FIG. 8;
FIG. 10 is a vertical section on line 10--10 of FIG. 9;
FIG. 11 is a longitudinal section showing another modification;
FIG. 12 is a transverse section on line 12--12 of FIG. 11;
FIG. 13 is a side elevation of another modification of the
valve;
FIG. 14 is an end view of FIG. 13;
FIG. 15 is a diagrammatic sectional view showing the FIG. 13
modification;
FIG. 16 is a view similar to FIG. 15 showing the use of the FIG. 13
valve as an entrance valve; and
FIG. 17 is a view similar to FIG. 15 showing the use of the FIG. 13
valve as an exit valve.
Corresponding reference characters indicate corresponding parts
throughout the several views of the drawings.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring to the drawings, there is indicated at 1 in FIGS. 1A-1E a
duct or tube, typically a subterranean tube, in which a vehicle 3
is adapted for propulsion as a free piston by differential pressure
between the front and rear of the vehicle. The tube 1 is shown as
extending from a station S1 to a station S2 along the route of a
transportation system. Entrance of the vehicle from station S1 to
the tube is via an entrance valve A at the entrance end of the
tube. Exit of the vehicle from the tube to station S2 is via an
exit valve B at the exit end of the tube.
Valves A and B, when closed, block off a section 1a of the tube
from valve-to-valve between stations S1 and S2. Provision is made
for evacuating this section of the tube down to low pressure (of
the order of 1 p.s.i., for example) as by means of suitable
evacuating pump equipment. Each station S1 and S2 is in
communication with the earth's atmosphere and hence at atmospheric
pressure. FIG. 1A shows both valves A and B closed, and the vehicle
3 in the station S1 about to start a trip from station S1 to
station S2. Section 1a of the tube between the valves has been
evacuated down to low pressure, e.g., of the order of 1 p.s.i. The
trip is initiated by opening valve A, resulting in atmospheric
pressure, acting on the rearward end of the vehicle, propelling it
past valve A into the tube section 1a (see FIG. 1B). After the
rearward end of the vehicle has passed by valve A and a
predetermined amount of air (at atmospheric pressure) has been
allowed to enter the tube behind the vehicle, valve A is closed
(see FIG. 1C). This traps a slug of air in the tube between valve A
and the rearward end of the vehicle, and expansion of this slug of
air causes the vehicle to accelerate until it reaches a point where
the pressure ahead of the vehicle is approximately equal to the
pressure behind the vehicle. The vehicle then begins to decelerate,
compressing air between the forward end of the vehicle and valve B,
with attenuation of air behind the vehicle. As the vehicle
approaches valve B, pressure in the tube ahead of the vehicle
increases to the point where it causes valve B to open, and the
vehicle comes to a stop in station S2, valve B closing behind
it.
This invention is particularly concerned with a valve construction
and operating system therefor suitable for each of the entrance and
exit valves A and B. It will be understood that valves A and B may
be identical, and simply installed in reversed positions at the
station S1 and S2 ends of the tube 1. Referring to FIGS. 2-7,
showing the valve A at station S1, there is indicated at 5 a valve
housing located at the top of the tube 1. This housing is formed to
provide a toroidal cylinder generally designated 7 on the outside
of the tube. This cylinder has a span of about 100.degree. to
180.degree.. It extends lengthwise with respect to the tube, that
is, the toroidal axis of the cylinder extends horizontally
crosswise of the tube above the tube. The toroidal cylinder 7 has a
relatively long section 7a of relatively large bore and a
relatively short section 7b of smaller bore. The small-bore section
7b is on the side of the toroidal axis toward the station S1, and
opens into the tube 1 as indicated at 7c. A shaft 9 is journaled in
the valve housing 5 on the toroidal axis of cylinder 7. Keyed on
this shaft is a gate 11 constituted by a differential rotary
toroidal piston which is adapted to swing about the axis of shaft 9
between the closed position in which it is illustrated in FIGS. 2
and 3 extending out of the open end of the cylinder 7 into the tube
1 blocking the tube 1 and an open position within the cylinder
wholly withdrawn and clear of the tube (see FIGS. 4 and 5). The
differential rotary piston 11 has a relatively long section 11a
having a diameter corresponding to that of the bore of cylinder
section 7b, and a relatively short section 11b at its upper end
having a diameter corresponding to that of the bore of cylinder
section 7a. As shown, the piston 11 may be of hollow construction
to decrease its weight. A counterweight 13 for the piston is keyed
on shaft 9 outside cylinder 7. The center of gravity of
counterweight and piston combination is indicated at G, and it will
be observed that this overcenters as the piston swings between its
closed and open position.
The lower end face of the toroidal piston 11 (i.e., the lower end
of its smaller-diameter section 11a) is designated 15. The upper
end face of the toroidal piston 11 (i.e., the upper end of its
larger-diameter section 11b) is designated 17. The face of the step
between the larger-diameter section 11b and the smaller-diameter
section of the piston is designated 19. The valve housing has an
auxiliary chamber 21 which is in communication with the cylinder 7
at the juncture of the cylinder sections 7a and 7b, the arrangement
being such that face 19 of the piston (which faces in the direction
toward the open end 7c of the cylinder) is subject to pressure in
chamber 21.
The cross-sectional diameter of section 11a of the piston 11 is
somewhat larger than the internal diameter of the tube 1, and, when
the piston is in its closed position of FIGS. 2 and 3, the margin
of its lower end face 15 seals against an annular shoulder or seat
23 in an enlarged section 25 of the tube. This section 25 is shaped
with a curvature such that the piston must swing through a
predetermined finite angle Y, which may be about 15.degree., for
example, before there is communication of air between the tube and
the station.
The valve housing 5 is formed with a port 27 for communication from
cylinder section 7a to the atmosphere. This port is located
intermediate the ends of cylinder 7, nearer to its closed end 7d
than its open end 7c, and has a check valve 29 therein which is
adapted to open in the direction for flow from the cylinder section
7a to the atmosphere. Housing 5 is also formed with a vacuum
manifold 31 in communication with the evacuated tube 1 on the
vacuum side of the valve A via a check valve 33 which is adapted to
open in the direction for flow of air from the manifold 31 into the
tube. Manifold 31 is adapted for communication with the port 27 via
a pilot valve 35, and for communication with chamber 21 via a pilot
valve 37. The latter is a two-way valve, adapted in a first
position to block communication between manifold 31 and chamber 21
while establishing communication between the earth's atmosphere and
chamber 21 via an atmospheric air inlet port 38, and in a second
position to block port 38 while establishing communication between
manifold 31 and chamber 21. The valve housing is also formed with a
bleed passage 39 for supplying air at atmospheric pressure from a
chamber 41 in communication with the earth's atmosphere to the
closed end 7d of cylinder section 7a.
The pressure in tube 1 acting on the lower end face 15 of the
toroidal gate or piston 11 is designated P1. The pressure in
cylinder section 7a acting on the upper end face 17 of the piston
11 is designated P2. The pressure in chamber 21 acting on the face
19 of the piston 11 is designated P3. The pressure in manifold 31
is designated P4. The pressure in the tube at the end of the
station is designated P5.
Valve B at station S2 is identical to valve A, being installed in
reversed position in respect to valve A, as will appear from FIGS.
1A-1E.
Operation is as follows:
Considering conditions prior to a trip of the vehicle from station
S1 to station S2, the vehicle will be poised at rest in station S1.
Valves A and B are closed (i.e., their pistons or gates 11 are
closed). Section 1a of the tube 1 between valves A and B will have
been evacuated down to low pressure, e.g., of the order of 1 p.s.i.
Pilot valve 35 of the operating system for each of valves A and B
is closed. Pilot valve 37 of the operating system for each of
valves A and B is set as shown in FIG. 2 for admission of air at
atmospheric pressure to chamber 21 while blocking passage 31 from
chamber 21. As to each of valves A and B, pressures P1-P5 are then
as follows:
---------------------------------------------------------------------------
Valve A Valve B
__________________________________________________________________________
P1 Vacuum Vacuum P2 Atmospheric Atmospheric P3 Atmospheric
Atmospheric P4 Vacuum Vacuum P5 Atmospheric Atmospheric
__________________________________________________________________________
The trip in initiated by opening valve A. This is accomplished by
opening pilot valve 35 of valve A, dropping P2 to vacuum. With P1
and P2 vacuum, the P3 atmospheric pressure acting on the pressure
face 19 of the piston 11 swings the piston 11 open. As the piston
moves past port 27, residual air in cylinder section 7a is trapped
and compressed, along with air entering cylinder section 7a via the
bleed 39. Thus, pressure P2 rises and slows the piston. Ultimately,
pressure P2 exceeds atmospheric pressure, and air is forced out
through the bleed 39 back to the atmosphere and the piston is
brought to a soft cushioned stop at the position shown in dotted
lines in FIG. 4. After the piston stops, air at atmospheric
pressure enters cylinder section 7a through the bleed 39 and slowly
moves the piston back to a position as shown in solid lines in FIG.
4 wherein the port 27 is partially opened, and the bleed is
balanced by flow of air (via pilot valve 35, which is open) into
manifold 31.
On opening of the piston or gate 11 of valve A, the vehicle 3 is
propelled into section 1a of the tube 1 via atmospheric pressure
acting on the rear of the vehicle. After the vehicle has passed
valve A, the pilot valve 35 of valve A is closed. A predetermined
amount of atmospheric air is allowed to enter section 1a of the
tube 1 from the station S1 behind the vehicle, and then the piston
or gate 11 of valve A is closed. This is accomplished by setting
pilot valve 37 in position for communication between chamber 21 and
manifold 31, and for blocking the atmospheric air inlet port 38. At
this time, pressures P1 and P5 are atmospheric. Pressure P2 is
atmospheric since pilot valve 35 has been closed, and the bleed 39
has supplied atmospheric air to the portion of cylinder section 7a
below port 27 (i.e., to the left of face 17 in FIG. 4). Thus, a
force equal to atmospheric pressure times the area of pressure face
19 of the piston, i.e., the amount by which the area of face 17
exceeds the effective area of face 15, acts to close the piston. As
the piston closes, the air in cylinder section 7a expands, meaning
that pressure P2 decreases. Pressure P1 also decreases due to
throttling of air rushing into the tube 1 behind the vehicle. The
chambers in the valve and its passages are dimensioned so that the
forces on the piston cause it to slowly and softly seat against the
shoulder 23 at the S1 end of section 1a of the tube. Pressure P2 in
cylinder section 7a returns to atmospheric pressure while pressure
P1 continues to decrease, insuring that the piston face 15 seats
firmly against the shoulder 23. Pilot valve 37 is then returned to
its initial FIG. 2 position for admission of air at atmospheric
pressure to chamber 21 while blocking manifold 31 from chamber
21.
When the piston or gate 11 of valve A is closed, expansion of the
slug of air trapped in the tube 1 between the rear of the vehicle
and this gate supplies an accelerating force on the rear of the
vehicle, and the vehicle continues to accelerate until it reaches
the point where the pressure ahead of the vehicle is approximately
equal to the pressure behind the vehicle. The vehicle then begins
to decelerate, compressing residual air in the tube 1 ahead of the
vehicle (with attenuation of air behind the vehicle). Thus, as the
vehicle approaches valve B, it compresses air between the forward
end of the vehicle and the end face 15 of the piston or gate 11 of
valve B, meaning that pressure P1 acting on end face 15 of valve B
rises. This may be envisioned by referring to FIG. 2 and
considering that it shows valve B (instead of valve A) and station
S2 (instead of station S1) and that the vehicle is approaching the
end face 15 of the piston from the left.
As pressure P1 acting on the end face 15 of piston 11 of valve B
rises, pressures P2, P3 and P5 are atmospheric. Pressure P1
ultimately rises above atmospheric pressure, and a force equal to
pressure P1 minus 1 atmosphere times the area of the end face 15 of
piston 11 of valve B acts to swing the latter open. The piston
travels through angle Y before communication is established between
the tube section 1a and the station S2. Thus, it travels through
this angle before pressure P1 is reduced to atmospheric pressure.
As the piston 11 of valve B travels through this angle, the center
of gravity G of the counterweight and piston combination
overcenters (i.e., passes over the axis of rotation of the piston),
and the resulting gravity bias on the piston in conjunction with
its inertia insure that the piston opens fully. Pressure P2 remains
at atmospheric pressure due to venting via the check valve 29 until
the piston passes the port 27 and, when this occurs, air is trapped
in cylinder section 7a, causing P2 to rise, slowing the motion of
the piston and bringing it to a soft cushioned stop.
With the piston or gate 11 of valve B open, the vehicle passes
through the valve and proceeds into the station B. As the rearward
end of the vehicle passes the valve B, P1 and P5 drop to vacuum.
With P2 and P3 at atmospheric pressure, the piston 11 of valve B
starts to close. As it closes, air in cylinder section 7a is
expanded and its pressure P2 decreases. As P2 decreases to near
vacuum, face 19 of piston 11 acts against atmospheric pressure P3
in chamber 21 to slow the motion of the piston, so that the closing
motion is soft. Air then bleeds into cylinder section 7a via the
bleed port 39 to raise P2 to atmospheric pressure to insure that
the piston seats firmly against shoulder 23.
With valve B closed, entry of air into station S2 behind the
vehicle is limited to leakage from atmosphere around the piston 11.
Hence, as the train proceeds into the station, pressure P5 remains
low and the effect is to continue to decelerate the vehicle until
it stops in station S2 (FIG. 1E).
In case of an emergency, it may be necessary to flood the tube with
air by opening one or the other or both of valves A and B. This can
be readily accomplished by opening the pilot valve 35 of the
desired valve or valves. With the pilot valve 37 in the position
shown in FIG. 2 so that pressure P3 in chamber 21 is atmospheric,
the piston 11 opens quickly on opening valve 35 (which effects
dropping P2 to vacuum).
FIGS. 8-10 illustrate a modification of the above-described
construction for valves A and B, which operates on the same basic
principles, but which utilizes an auxiliary piston for driving the
gate instead of utilizing a single differential piston as the gate.
As shown therein, the valve comprises a main toroidal cylinder 47
extending lengthwise of the tube 1 at the top of the tube, i.e.,
the toroidal axis of the cylinder extends horizontally transversely
of the tube above the tube. The toroidal bore of this cylinder is
of uniform diameter throughout its extent, and opens at 47c into
the tube on that side of the toroidal axis toward the station. A
shaft 49 is journaled on the toroidal axis of cylinder 47. Keyed on
this shaft is a gate 51 constituted by a toroidal piston adapted to
swing about the axis of the shaft between a closed position
extending out of the open end 47c of the cylinder into the tube
blocking the tube and an open position within the cylinder clear of
the tube. This gate or piston 51 is of uniform diameter throughout
its extent, corresponding to the bore of cylinder 47, and may be of
hollow construction as illustrated to reduce its weight. The lower
end face of piston 51 is designated 53 and its upper end face is
designated 55. When the piston is in its closed position, its lower
end face 53 seals against shoulder 23 around the tube, as
above.
Cylinder 47 has a port 27a (corresponding to port 27) provided with
a check valve 29a (corresponding to check valve 29), and a vacuum
manifold 31a (corresponding to manifold 31) provided with a check
valve 33a (corresponding to check valve 33). Manifold 31a is
adapted for communication with port 27a via a pilot valve 35a
(corresponding to pilot valve 35). A bleed 39a (corresponding to
bleed 39) is provided for supplying air at atmospheric pressure
from a chamber 41a (corresponding to chamber 41) to the closed end
of cylinder 47.
An auxiliary toroidal cylinder 57 is located alongside the tube 1
and main cylinder 47 in coaxial relation to the latter. The shaft
49 extends from the main cylinder over to the auxiliary cylinder
and has a toroidal auxiliary piston 59 keyed thereon working in the
auxiliary cylinder. The ends of this auxiliary piston are
designated 59a and 59b. The auxiliary cylinder has a chamber 61 at
one end (corresponding to chamber 21) and a pilot valve 37a
(corresponding to pilot valve 37). The other end of the auxiliary
cylinder is interconnected with the main cylinder as indicated at
63. The auxiliary piston serves as a counterweight for the main
piston 51, and the center of gravity of the combination of the two
pistons is indicated at G. It will be observed that this
overcenters as the main piston 51 swings between its closed and
open positions.
The sum of the area of the upper end face 55 of the main piston 51
and the area of the lower end face 59a of the auxiliary piston is
equal to the area of the upper face 17 of piston 11; the area of
the lower end face 53 of the main piston 51 and the area of the
upper end face 59b of the auxiliary piston 59 are respectively
equal to the area of the lower end face 15 of piston 11 and area of
the upper end face 19 of piston 11. Accordingly, the operation of
the valve is basically the same as that of the valve A or B
described above. Thus, as to the entrance valve function of the
valve shown in FIGS. 8-10, on opening pilot valve 35a, dropping P2
to vacuum, P3 acting on face 59b of the auxiliary piston 59 swings
the auxiliary piston counterclockwise as viewed in FIG. 10 to swing
the piston or gate 51 open, and valve 35a is then closed. On
setting pilot valve 37a in position for communication between
chamber 61 and vacuum manifold 31a, the auxiliary piston is swung
in clockwise direction as viewed in FIG. 10 to swing the piston or
gate 51 closed. As to the exit valve function of the valve shown in
FIGS. 8-10, rise in P1 on approach of the vehicle swings the piston
or gate 51 open.
FIGS. 11 and 12 show another modification of the valve construction
of FIGS. 2-7 wherein the bore of the toroidal cylinder is generally
of uniform diameter throughout its length. The cylinder is here
designated 7e to distinguish it from cylinder 7. The toroidal
piston, designated 11c to distinguish it from piston 11, has a
cross-sectional diameter somewhat less than that of the bore in
cylinder 7e, and is provided at its upper end with a sealing ring
11d, forming an enlargement corresponding to 11b, and providing a
pressure face 19a corresponding to face 19. This sealing ring,
accommodated in an annular groove 71 in the piston, is in sliding
sealing engagement with the bore of the cylinder. The effect of the
smaller cylinder bore 7b of the construction shown in FIGS. 2-7 is
provided by a sealing ring 73 mounted in the cylinder below chamber
21, with which the piston is in sliding sealing engagement. Two
counterweights 13 are shown in FIG. 12 for the piston. Otherwise
the construction corresponds to that shown in FIGS. 2-7, and the
operation is the same.
FIGS. 13-17 illustrate a further modification of the valve similar
to the modification in FIGS. 8-10 but having a special gate
construction. As shown, this further modification has a main
toroidal cylinder or chamber 77 (similar to 47) which curves upward
away from tube 1 and which is open at its lower end indicated at
77c to the tube on that side of the toroidal axis toward the
station S. The short section of the tube 1 on the station side of
the valve is referred to as the airlock AL. A shaft 79 (like shaft
49) is journaled on the toroidal axis of the chamber 77. The latter
is of circular cross section and its toroidal axis is transverse to
and slightly above the tube. The upper end of the chamber 77 is
closed as indicated at 77d, with this closure being of inwardly
directed frustoconical form.
The gate of the modification shown in FIGS. 13-17 is designated in
its entirety by the reference numeral 80. It is constituted by two
conical members 81 and 83 mounted with their axes generally at
right angles on a frame 85 which extends radially outward from
shaft 79. These two conical members are preferably formed as hollow
conical shells, 81 being the lower and 83 the upper of the two.
Member 81, which may be referred to as the cap, has its apex
secured to the frame 85 adjacent the outer end of the latter as
indicated at 87 and extends on the bottom side of the frame with
its conical axis at a 45.degree. angle to the frame. Member 83,
which may be referred to as the driver, has its apex secured to the
frame 85 adjacent the outer end of the frame as indicated at 89 and
extends on the top side of the frame with its conical axis at a
45.degree. angle to the frame. The gate 80 is swingable on the axis
of shaft 79 between the closed position shown in solid lines in
FIG. 15 and the open position shown in dotted lines in FIG. 15. In
the closed position, frame 85 is generally at an angle of
45.degree. below horizontal, and the rim 81a of the cap 81 is in
sealing engagement with the shoulder 23 around the tube 1. In the
open position, wherein the gate is swung upward, both conical
members 81 and 83 are retracted into the chamber 77 clear of the
tube 1, the driver (i.e., the upper conical member) nesting over
the conical upper end closure 77d of chamber 77. The driver 83 is
preferably slightly larger than the lower conical member and has a
slightly greater moment arm about shaft 79 than the cap 81. Its rim
83a fits in chamber 77 with a small clearance C therebetween.
An auxiliary cylinder or chamber 89 is located alongside the tube 1
and the main cylinder or chamber 77 in coaxial relation to the
latter. This auxiliary chamber 89 is a partial toroid, preferably
of rectangular cross section, having a lower end 89a which is open
to the atmosphere and an upper end 89b which is closed. The shaft
79 extends from the main chamber into the auxiliary chamber. An
impeller 91 in the form of a vane extends radially outward from the
shaft 79 in chamber 89 and has a relatively tight sliding fit in
chamber 89 to serve as a piston therein. It is also so weighted and
so located on the shaft 79 as to constitute a counterweight for the
gate 80, preferably establishing the center of mass of the entire
gate/impeller assembly (which assembly may be referred to as the
rotor R) adjacent to or on the axis of rotation of this assembly
(i.e., the axis of shaft 79).
The position of the rotor R is controlled by controlling the
pressures in the main chamber 77 and the auxiliary chamber 89. For
this purpose, the auxiliary chamber 89 has a vacuum vent 92 having
a pilot valve 93 therein extending from a point near its upper end
to a vacuum manifold 95. It also has a relatively large atmospheric
vent 97 having a pilot valve 99 therein and a relatively small
atmospheric vent 101 having a pilot valve 103 therein at its upper
end. These pilot valves are linked together in suitable manner such
that the two atmospheric vents 97 and 101 are open when the vacuum
vent 92 is closed and vice versa.
The main chamber 77 has an atmospheric outlet 105 at the top with a
check valve 107 therein that allows for flow of air out of chamber
77 to the atmosphere while checking against flow back into the
chamber; a relatively large air inlet 109 having a check valve 111
and a pilot valve 113; and a relatively small air inlet 115 with a
pilot valve 117 therein. A passage 119 interconnects the tube 1 on
the side of gate 80 away from the station and chamber 77 adjacent
its upper end. This passage has a pilot valve 121 therein. Air
inlet 109 is connected to passage 119. At 123 is indicated a bias
port which extends from about the midpoint of the outer side of
chamber 77 to the vacuum manifold 95 and which has a pilot valve
125 and baffles 127 therein.
The relative angular location and size of the vacuum vent 119 and
atmospheric outlet 105 of the main chamber 77 and the vacuum vent
92 and atmospheric vents 97 and 101 of the auxiliary chamber shown
in the drawings are illustrative only. The operation of the FIG. 13
valve depends on the proper location and sizing of each of these
items (one example of which is shown in FIG. 15). They can be
installed at different lateral locations so that any angular
location is possible for any of these items.
The operation of the valve shown in FIGS. 13-15 is described below
in conjunction with a trip of a train from station S1 to station S2
to FIG. 1A. The description uses the nomenclature and valve numbers
from FIG. 15. For convenience and clarity, FIGS. 16 and 17 show the
entrance valve A and exit valve B, respectively, each oriented to
correspond to FIG. 1A. Further, FIG. 16 shows only those features
necessary for the valve to operate as an entrance valve and FIG. 17
shows only the features required for the valve to operate as an
exit valve; the pilot valves or check valves associated with the
various features not shown are always closed for the situation
illustrated.
ENTRANCE VALVE OPENING (FIG. 16)
Before the trip begins, the train is stationary in station S1,
valves A and B are closed, and the tube has been evacuated (FIG.
1A). The condition of the pilot valves of entrance valve A and
various pressures within this valve are as follows:
---------------------------------------------------------------------------
Pilot Valve Condition Chamber Pressure*
__________________________________________________________________________
93 closed Main** 77 A 99 and 103 open Auxiliary*** 89 A 113 closed
Tube 1 V 117 closed Airlock AL A 121 closed 125 closed
__________________________________________________________________________
The forward end of the train is in the airlock so that flow of
atmospheric air from the station S1 into the airlock is
prevented.
The trip is initiated by opening entrance valve A. This is
accomplished by opening the pilot valve 121 of valve A. The
pressure in the main chamber 77 rapidly decreases as air flows out
through the vacuum vent 119 into the tube 1. As the pressure nears
tube pressure, the rotor R begins to move because the torque caused
by the pressure difference across the driver 83 exceeds that caused
by the pressure difference across the cap 81. This happens somewhat
before the pressure reaches tube pressure, since the driver 83 has
a slightly larger area and moment arm than the cap 81. As the main
chamber 77 drops to tube pressure, the rotor R rapidly accelerates
until the valve has opened sufficiently for the atmospheric air in
the airlock AL to escape into the tube 1. The acceleration is
somewhat impeded by expansion of the air in the auxiliary chamber
89 until the impeller 91 passes the large atmospheric vent 97,
after which there is essentially no pressure difference on the
impeller. After the air has escaped from the airlock AL, the rotor
R coasts with virtually no acceleration or deceleration until the
driver 83 begins to cross the vacuum 119 of the main chamber 77. As
the driver crosses the vent, the flow of air out of the chamber 77
is progressively cut off and the thin air is compressed, causing a
braking torque which brings the rotor R to a soft stop shortly
after the driver has fully passed the vent 119. The clearance C
around the driver 83 provides sufficient damping to eliminate any
tendency to bounce. It seems desirable to locate the center of mass
of the rotor R such that the force of gravity will provide a small
torque that insures that the rotor continues to move slowly until
the driver rests against the conical closure 77d of the main
chamber 77.
With entrance valve A open, the train proceeds into the tube 1, as
indicated in FIG. 1B, and pilot valve 121 of entrance valve A is
closed.
ENTRANCE VALVE CLOSING (FIG. 16)
When the rear end of the train has passed entrance valve A, the
condition of the pilot valves of entrance valve A and various
pressures within the valve are as follows:
---------------------------------------------------------------------------
Pilot Valve Condition Chamber Pressure
__________________________________________________________________________
93 closed Main 77 A 99 and 103 open Auxiliary 89 A 113 closed Tube
1 A 117 closed Airlock AL A 121 closed 125 closed
__________________________________________________________________________
The gate assembly 80 is clear of the tube 1 with the driver 83
resting against the conical closure 77d of the main chamber 77.
Entrance valve A is readied for closing by opening pilot valve 113,
thus opening the large inlet 109. The valve does not move, however,
because no pressure differential exists. When the train has
proceeded a predetermined distance into the tube, entrance valve A
is closed on command. This is accomplished by a single operation
that closes pilot valves 99 and 103 and opens pilot valve 93. The
air in the auxiliary chamber 89 is quickly exhausted via the vacuum
vent 92 and atmospheric pressure acting on the impeller 91 drives
the valve A closed. Pressure in the main chamber 77 remains
essentially equal to tube pressure because of the large inlet 109.
As the impeller 91 crosses the vacuum vent 92, it begins to
compress the thin air in the auxiliary chamber 89. When the
pressure exceeds atmospheric, it slows the rotor R and brings it to
soft stop just before the cap 81 engages the seat 23. Damping is
provided by a fixed leakage past the impeller 91. This occurs even
though a pressure drop develops across the cap 81 as it impinges
upon the flow. This pressure drop causes the cap 81 to seat firmly
as the compressed air in the auxiliary chamber 89 leaks past the
impeller 91. Once entrance valve A is closed, pilot valves 93 and
113 are closed and pilot valves 99 and 103 are reopened thus
returning the entrance valve to the conditions that prevailed
before the trip began.
The train continues on its trip to station B as shown in FIG.
1C.
During entrance valve operations, only pilot valves 93, 99, 103,
113 and 121 were used and the check valve 107 did not open. If the
valve were never to be used as an exit valve, pilot valves 117 and
125, check valve 105, and their associated ducting (FIG. 15) would
not be needed as indicated on FIG. 16. System considerations,
however, may make it desirable for all valves to be alike so that
the trains can be operated in reverse if necessary.
EXIT VALVE OPENING (FIG. 17)
As the train approaches station B, the condition of the pilot
valves of exit valve B and various pressures within the valve are
as follows:
---------------------------------------------------------------------------
Pilot Valve Condition Chamber Pressure
__________________________________________________________________________
93 closed Main 77 4 99 and 103 open Auxiliary 89 A 113 closed Tube
1 less than A 117 closed Airlock AL A 121 closed 125 open
__________________________________________________________________________
With pilot valve 125 open, there is a continuous flow of air from
the airlock AL, past the driver 83 which has a small amount of
clearance C around it, into the main chamber 77, and out through
the bias port 123 to the vacuum manifold 95. The bias port is sized
so that this flow results in a predetermined pressure (P) in the
main chamber 77 that is somewhat less than atmospheric. The bias
port may contain baffles as indicated at 127 so that the pressure
drop from the main chamber 77 to the vacuum manifold occurs in
several steps, thereby avoiding a potential source of noise.
As the train approaches exit valve B, it is rapidly compressing the
air ahead in the tube 1. When the tube pressure reaches a pressure
somewhat less than the bias pressure P in the main chamber 77, the
exit valve begins to open. This occurs before the pressure reaches
P because the area and moment arm of the driver 83 are slightly
larger than those of the cap 81. The rotor R accelerates rapidly as
the tube pressure continues to rise. The air in the auxiliary
chamber 89 expands until the large atmospheric vent 99 is passed by
the impeller 91, but the resisting force on the impeller is small
compared to that pushing the cap 81.
As the gate assembly 80 moves into the main chamber 77, the
pressure in the main chamber 77 rapidly rises to atmospheric since
the bias port 123 does not have sufficient capacity to hold the
bias. When the pressure reaches atmospheric, air exhausts through
the atmospheric outlet 105 as well as the bias port 123 thus
maintaining approximately atmospheric pressure in the main chamber
77 until the driver 83 crosses the bias port 123 and atmospheric
outlet 105. As it crosses the atmospheric outlet 105, flow is
progressively cut off and the driver 83 compresses the air bringing
the rotor R to a soft stop. Again, bounce is prevented by the
damping effect of the clearance C around the driver 83. The rotor R
comes to rest with the driver 83 against the conical closure 77d of
the main chamber 77 and the train proceeds through the exit valve B
as shown in FIG. 1D.
EXIT VALVE CLOSING (FIG. 17)
Once the train has passed through exit valve B into station B, the
valve must be closed to preserve the vacuum in the tube 1. The air
that was trapped behind the train when the entrance valve A closed
has been expanded to near vacuum. The train has nearly stopped and
its rear end is in the airlock AL blocking flow of air from the
station S2 into the tube 1. The condition of the pilot valves of
exit valve B and various pressures within the valve are as follows:
---------------------------------------------------------------------------
Pilot Valve Condition Chamber Pressure
__________________________________________________________________________
93 closed Main 77 V 99 and 103 open Auxiliary 89 A 113 closed Tube
1 V 117 closed Airlock AL V 121 closed 125 closed
__________________________________________________________________________
As soon as the rear end of the train has passed through the exit
valve, pilot valve 117 is opened and air enters the main chamber 77
through the small inlet 115. With vacuum operating on the other
surfaces of the gate assembly 80, the rotor R accelerates until it
reaches a speed that is limited by the flow rate through the small
inlet 115. The rotor R continues at this speed until the exit valve
is nearly closed. When the impeller 91 crosses the atmospheric vent
99, it begins compressing the air trapped in the auxiliary chamber
89 which brakes the rotor R and brings it to a stop with the cap 81
seated. Leakage past the impeller 91 and flow of air through the
small atmospheric vent 103 allows the compressed air to escape so
that the cap 81 remains seated with no bounce.
The train comes to a stop in station B as shown in FIG. 1E and the
pilot valve 117 of exit valve B is closed so that the valve is
ready to be biased for the approach of the next train.
When the valve is used only as an exit valve, pilot valves 93, 99,
103, 113 and 121 are not used, as indicated in FIG. 17.
In view of the above, it will be seen that the several objects of
the invention are achieved and other advantageous results
attained.
As various changes could be made in the above constructions without
departing from the scope of the invention, it is intended that all
matter contained in the above description or shown in the
accompanying drawings shall be interpreted as illustrative and not
in a limiting sense.
* * * * *