U.S. patent number 3,905,720 [Application Number 05/486,441] was granted by the patent office on 1975-09-16 for apparatus for adjusting turbine guide vanes and the like.
This patent grant is currently assigned to Motoren- und Turbinen-Union Munchen GmbH. Invention is credited to Christian Greune, Hilbert Holzhauer.
United States Patent |
3,905,720 |
Greune , et al. |
September 16, 1975 |
Apparatus for adjusting turbine guide vanes and the like
Abstract
Apparatus for adjusting a movable member, for example a guide
vane for a gas turbine engine, including an actuating cylinder, and
an actuating piston slidably disposed in said cylinder, with one of
the cylinder and piston connected in a direct drive linkage for
moving the guide vane. A control valve is provided for controlling
the opening and closing of respective inlet and exhaust ports
leading to a control chamber which effects movement of the
actuating piston. This control valve includes a control valve
member having one end face acted upon by a fluid control pressure
and one arm of a two armed elastically loaded lever contacting the
control valve member to force the same against the fluid control
pressure. The other arm of the lever includes a roller and is in
contact with a predetermined generating line provided in a cavity
of the actuating piston such that movement of the actuating piston
changes the resistance to movement of the control valve member
exerted by way of the lever, whereby a precise and accurate
positioning of the actuating piston, irrespective of the reactive
forces acting on the actuating piston is obtained.
Inventors: |
Greune; Christian
(Furstenfeldbruck, DT), Holzhauer; Hilbert (Stetten,
DT) |
Assignee: |
Motoren- und Turbinen-Union Munchen
GmbH (DT)
|
Family
ID: |
5886270 |
Appl.
No.: |
05/486,441 |
Filed: |
July 8, 1974 |
Foreign Application Priority Data
Current U.S.
Class: |
415/148; 91/368;
91/417R |
Current CPC
Class: |
F01D
17/26 (20130101); F15B 9/12 (20130101) |
Current International
Class: |
F01D
17/00 (20060101); F15B 9/12 (20060101); F01D
17/26 (20060101); F15B 9/00 (20060101); F03B
015/04 () |
Field of
Search: |
;415/148,150,151,37,51
;91/382,384,417,368 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Raduazo; Henry F.
Attorney, Agent or Firm: Craig & Antonelli
Claims
We claim:
1. Apparatus for imparting adjusting movements to a movable member,
comprising:
an actuating cylinder,
an actuating piston slidably disposed in said cylinder,
one of said actuating cylinder and actuating piston including means
for connecting same to said movable member for movement
therewith,
a control chamber communicating with a first face of said actuating
piston such that supply of fluid under pressure to said control
chamber effects movement of said actuating piston in a first
direction and drainage of fluid from said control chamber perm its
movement of said actuating piston in a second direction opposite
said first direction,
control chamber inlet means for communicating fluid under pressure
to said control chamber,
control chamber exhaust means for exhausting fluid from said
control chamber,
a control valve for controlling the opening and closing of said
control chamber inlet and exhaust means, said control valve
including a control valve member acted upon in one direction by a
fluid control pressure and in the other opposite direction by a
control biasing force,
said actuating piston including a cavity bounded in part by a
generating surface which is spaced from a centerline of said
actuating piston by varying amounts along the length of said
actuating piston, and interconnecting means in contact with both
said control valve member and said generating surface for effecting
changes in said control biasing force as a function of the position
of said actuating piston along the travel path thereof in said
actuating cylinder.
2. Apparatus according to claim 1, wherein said cavity forms part
of said control chamber, wherein a second face of said actuating
piston which faces oppositely of and is smaller than said first
face is continuously communicated with the fluid under pressure
supplied to said control chamber inlet means, wherein said fluid
under pressure is a hydraulic fluid,
wherein said interconnecting means is an elastically bendable
two-armed lever having one arm thereof in contact with said control
valve member and the other arm thereof in contact with said
generating surface, and wherein said two-armed lever is supported
intermediate the ends thereof at a part fixed with said actuating
cylinder so as to apply an elastic stressing force as said control
biasing force.
3. Apparatus according to claim 2, wherein said control valve
member is constrained to move transversely to the direction of
movement of said actuating piston.
4. Apparatus according to claim 3, wherein said control valve means
includes means for opening one of said control chamber inlet and
exhaust means upon minimal movement of said control valve member
from a central position thereof.
5. Apparatus according to claim 4, wherein said movable member is a
guide vane of a gas turbine engine or the like.
6. Apparatus according to claim 1, wherein the inclination of the
generating surface relative to the centerline of the actuating
piston: is relatively great near one end of the cavity to define a
drive range, is relatively small along an intermediate portion of
the cavity, and is relatively great at the end of the cavity
opposite said one end to define a deceleration range.
7. Apparatus according to claim 5, wherein the inclination of the
generating surface relative to the centerline of the actuating
piston: is relatively great near one end of the cavity to define a
drive range, is relatively small along an intermediate portion of
the cavity, and is relatively great at the end of the cavity
opposite said one end to define a deceleration range.
8. Apparatus according to claim 2, wherein the inclination of the
generating surface relative to the centerline of the actuating
piston: is relatively great near one end of the cavity to define a
drive range, is relatively small along an intermediate portion of
the cavity, and is relatively great at the end of the cavity
opposite said one end to define a deceleration range.
9. Apparatus according to claim 2, wherein said control valve
member is constructed with cylindrical valve member end portions at
the ends thereof having control edges for controlling openings of
said control chamber inlet and exhaust means, said control edges
being located at the juncture of said end portions with a central
portion of said control valve member which has a smaller diameter
than either of said end portions such that the annulus formed
around said central portion forms part of the control chamber.
10. Apparatus according to claim 8, wherein said control valve
member is constructed with cylindrical valve member end portions at
the ends thereof having control edges for controlling openings of
said control chamber inlet and exhaust means, said control edges
being located at the juncture of said end portions with a central
portion of said control valve member which has a smaller diameter
than either of said end portions such that the annulus formed
around said central portion forms part of the control chamber.
11. Apparatus according to claim 2, wherein said control valve
member has an inlet control edge at one end and an exhaust control
edge at the other end, wherein said control chamber communicates
with said control valve member by an opening having a width in the
direction of movement of said control valve member which is the
same as the distance between said inlet and exhaust control edges,
and wherein a control cylinder within which said control valve
member is slidably guided exhibits an uncontrolled inlet duct and
an uncontrolled exhaust duct at respective opposite axial sides of
said opening with respect to movement of said control valve
member.
12. Apparatus according to claim 11, wherein said uncontrolled
inlet duct communicates with a pressure line and said uncontrolled
exhaust duct communicates with a drain line.
13. Apparatus according to claim 8, wherein said control valve
member has an inlet control edge at one end and an exhaust control
edge at the other end, wherein said control chamber communicates
with said control valve member by an opening having a width in the
direction of movement of said control valve member which is the
same as the distance between said inlet and exhaust control edges,
and wherein a control cylinder within which said control valve
member is slidably guided exhibits an uncontrolled inlet duct and
an uncontrolled exhaust duct at respective opposite axial sides of
said opening with respect to movement of said control valve
member.
14. Apparatus according to claim 2, wherein the one arm of said
lever is of forked configuration with two spaced fork parts,
wherein said control valve member is flattened on two opposite
sides to accommodate said contact of said fork parts in said
flattened sides in a longitudinal center plane of the control valve
member.
15. Apparatus according to claim 8, wherein the one arm of said
lever is of forked configuration with two spaced fork parts, and
wherein said control valve member is flattened on two opposite
sides to accommodate said contact of said fork parts in said
flattened sides in a longitudinal center plane of the control valve
member.
16. Apparatus according to claim 9, wherein the one arm of said
lever is of forked configuration with two spaced fork parts, and
wherein said control valve member is flattened on two opposite
sides to accommodate said contact of said fork parts in said
flattened sides in a longitudinal center plane of the control valve
member.
17. Apparatus according to claim 11, wherein the one arm of said
lever is of forked configuration with two spaced fork parts, and
wherein said control valve member is flattened on two opposite
sides to accommodate said contact of said fork parts in said
flattened sides in a longitudinal center plane of the control valve
member.
18. Apparatus according to claim 2, wherein a restrictor duct
communicates said control chamber inlet means with a face of said
control valve member acted upon by said fluid control pressure, and
wherein said last-mentioned face of said control valve member is
arranged in direct fluid communication with a mechanism for
controlling the magnitude of said fluid control pressure, said
mechanism including means operable by a variable electromagnetic
force to vary said magnitude of said fluid control pressure.
19. Apparatus according to claim 8, wherein a restrictor duct
communicates said control chamber inlet means with a face of said
control valve member acted upon by said fluid control pressure, and
wherein said last-mentioned face of said control valve member is
arranged in direct fluid communication with a mechanism for
controlling the magnitude of said fluid control pressure, said
mechanism including means operable by a variable electromagnetic
force to vary said magnitude of said fluid control pressure.
20. Apparatus according to claim 9, wherein a restrictor duct
communicates said control chamber inlet means with a face of said
control valve member acted upon by said fluid control pressure, and
wherein said last-mentioned face of said control valve member is
arranged in direct fluid communication with a mechanism for
controlling the magnitude of said fluid control pressure, said
mechanism including means operable by a variable electromagnetic
force to vary said magnitude of said fluid control pressure.
21. Apparatus according to claim 11, wherein a restrictor duct
communicates said control chamber inlet means with a face of said
control valve member acted upon by said fluid control pressure, and
wherein said last-mentioned face of said control valve member is
arranged in direct fluid communication with a mechanism for
controlling the magnitude of said fluid control pressure, said
mechanism including means operable by a variable electromagnetic
force to vary said magnitude of said fluid control pressure.
22. Apparatus according to claim 18, wherein said mechanism
controls a drain for varying the back pressure build up from the
fluid communicated by said restrictor duct to said face of said
control valve member.
23. Apparatus according to claim 2, wherein said control valve
includes a control valve cylinder for accommodating sliding
movement of said control valve member, and wherein a damping duct
communicates said control chamber exhaust means with a face of said
control valve member which faces oppositely to the face of said
control valve member which is acted upon by said fluid control
pressure.
24. Appararatus according to claim 8, wherein said control valve
includes a control valve cylinder for accommodating sliding
movement of said control valve member, and wherein a damping duct
communicates said control chamber exhaust means with a face of said
control valve member which faces oppositely to the face of said
control valve member which is acted upon by said fluid control
pressure.
25. Apparatus according to claim 9, wherein said control valve
includes a control valve cylinder for accommodating sliding
movement of said control valve member, and wherein a damping duct
communicates said control chamber exhaust means with a face of said
control valve member which faces oppositely to the face of said
control valve member which is acted upon by said fluid control
pressure.
26. Apparatus according to claim 11, wherein said control valve
includes a control valve cylinder for accommodating sliding
movement of said control valve member, and wherein a damping duct
communicates said control chamber exhaust means with a face of said
control valve member which faces oppositely to the face of said
control valve member which is acted upon by said fluid control
pressure.
27. Apparatus according to claim 18, wherein said control valve
includes a control valve cylinder for accommodating sliding
movement of said control valve member, and wherein a damping duct
communicates said control chamber exhaust means with a face of said
control valve member which faces oppositely to the face of said
control valve member which is acted upon by said fluid control
pressure.
28. Apparatus according to claim 2, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing being
radially spaced from internal walls of said hollow portion by
sealing rings.
29. Apparatus according to claim 28, wherein said bushing is of
stepped diameter with the maximum diameter at an end thereof which
is axially fixed to said actuator housing, whereby axial insertion
of said bushing and sealing rings is accommodated.
30. Apparatus according to claim 8, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing being
radially spaced from internal walls of said hollow portion by
sealing rings.
31. Apparatus according to claim 9, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing being
radially spaced from internal walls of said hollow portion by
sealing rings.
32. Apparatus according to claim 11, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing being
radially spaced from internal walls of said hollow portion by
sealing rings.
33. Apparatus according to claim 18, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing radially
spaced from internal walls of said hollow portion by sealing
rings.
34. Apparatus according to claim 23, wherein said control valve
includes a bushing inserted into a hollow portion of an actuator
housing fixed with said actuating cylinder, said control valve
member being slidable inside of said bushing, said bushing being
radially spaced from internal walls of said hollow portion by
sealing rings.
35. Apparatus according to claim 8, wherein the inclination of the
generating surface relative to the centerline of the actuating
piston is greater in said deceleration range than in said drive
range.
Description
BACKGROUND AND SUMMARY OF THE INVENTION
The present invention relates to appratus for adjusting a movable
member, for example turbine guide vanes and the like. The present
invention is more specifically related to an improved actuator
which has an actuating piston slidable in an actuating cylinder in
accordance with a predetermined characteristic in response to fluid
pressure acting on said piston.
Previously contemplated fluid pressure responsive actuators of the
just-mentioned category utilize a cam disk for maintaining and
giving the predetermined characteristic. (See British Pat. No.
1,055,319). A disadvantage of such previously contemplated actuator
is that additional means are required to operate the cam disk by
means of a hydraulic or electrical input signal in an automatically
occurring process. A further disadvantage of such actuators is seen
in that an actuating rod extending through a control chamber
between the actuating piston and a control valve for fluid supply
to said actuating piston, in parallel with the control valve for
endwise movement imparted to it by the cam disk against the force
of a spring and carrying a rotatably mounted two-armed lever leads
through the housing of the hydraulic actuator. Such a lead-in of
the lever through the housing is difficult to seal off, causes
friction, and poses further design problems related to hydraulic
thrust imposed on the actuating rod.
The present invention overcomes the above-mentioned disadvantages
by providing a pressure medium operated piston-cylinder actuator
which achieves respective intended positions of the actuating
piston with great precision and relatively moderate complexity of
the actuating means. According to the invention, the previously
contemplated actuating rod, the lead-in through the actuator
housing, and the cam disk bearing the characteristic are all
eliminated and a hydraulic input signal is supplied to the
hydraulic actuator directly and in the absence of intervening
mechanical links. In this way, the characteristic curve for
changing the control force on the control valve in dependence upon
the relative position of the actuator piston and cylinder can be
constructed in a simple manner to be linear, nonlinear, or not
uniformly linear.
More specifically, the present invention contemplates apparatus for
imparting adjusting movements to a movable member, such as a
linkage member in an actuating train for a guide vane on a
vehicular gas turbine engine, which apparatus includes an actuating
cylinder, an actuating piston slidably disposed in the cylinder,
means for connecting one of the actuating cylinder and actuating
piston to a movable member for movement therewith, a control
chamber communicating with a first face of the actuating piston
such that supply of fluid under pressure to the control chamber
effects movement of the actuating piston in a first direction and
drainage of fluid from the control chamber permits movement of said
actuating piston in a second direction opposite the first
direction, control chamber inlet means for communicating fluid
under pressure to the control chamber, control chamber exhaust
means for exhausting fluid from the control chamber, a control
valve for controlling the opening and closing of the control
chamber inlet and exhaust means, said control valve including a
control valve member acted upon in one direction by a fluid control
pressure and in the other opposite direction by a control biasing
force, the actuating piston including a cavity bounded in part by a
generating surface which is spaced from the centerline of said
actuating piston by varying amounts along the length of said
actuating piston, and interconnecting means in contact with both
the control valve member and the generating surface for effecting
changes in the control biasing force as a function of the position
of the actuating piston along the travel path thereof in the
actuating cylinder. According to a further aspect of the invention,
the apparatus just described is constructed such that the cavity
forms part of the control chamber, wherein a second face of the
actuating piston which faces oppositely of and is smaller than the
first face is continuously communicated with the fluid under
pressure supplied to the control chamber inlet means, wherein the
fluid under pressure is a hydraulic fluid, wherein the
interconnecting means is a two-armed lever having one arm thereof
in contact with the control valve member and the other arm thereof
in contact with the generating surface, and wherein the two-armed
lever is supported intermediate the arms thereof at a part fixed
with said actuator cylinder.
In preferred embodiments of the invention, the actuating piston,
which is constructed as a differential area piston, will not move
so long as the force of control pressure acting on said end face of
said control valve member is equal to the force of flexural preload
of the lever acting on the control valve member in the axially
opposite direction. Said preload of the lever varies with the
position of the actuating piston as a result of the form of the
generating line. When a change occurs in control pressure the
resulting discrepancy between said two forces causes the control
valve member to move away from its shut-off position in one or the
other axial direction. This movement of the control valve member
either pressurizes the larger face of the actuating piston in the
control chamber and the actuating piston is moved in its one axial
direction, or exhausts the control chamber and the actuating piston
is moved in the opposite direction while the control chamber is
being emptied accordingly. Movement of the actuating piston, due to
the form of the generating line, causes the force of lever preload
to change until equibrium is achieved with the new force of control
pressure, which returns the control valve to its shut-off position.
The actuating piston comes to rest in very precisely the intended
position.
With the apparatus of the present invention, the actuating piston
travels, as a function of control pressure, an intended distance
which is independent of the magnitude, direction and change in load
resistance acting on the actuating piston. In use for adjusting
turbine engine guide vanes, the load resistance has its origin
especially in the gas forces acting on the guide vanes. The
actuating means of the present invention is relatively simple and
free from complexity. Forces are balanced one against the other and
a lead-in in the housing is eliminated together with its
above-mentioned disadvantages. Due to the simplicity of design, the
actuating means of the present invention can be a robust
construction. The actuating means of the present invention is also
practically insensitive to vibrations, which prevents wear on its
parts and noise.
The actuating accuracy of the hydraulic actuator of the present
invention can be improved by increasing the inclination of the
generating line relative to the centerline of the actuating piston.
Depending upon the desired characteristic acceleration and
deceleration of the member being adjusted (e.g. turbine guide
vane), the generating line may be curved over part of all of its
length or it may angleoff in a straight line, according to the
present invention. In the case of non-uniform linearity between the
pressure signal and the stroke of the actuating piston, a preferred
embodiment varies the inclination of the generating line relative
to the centerline of the actuating piston to effect drive, neutral
and deceleration ranges respectively, where more particularly the
inclination is relatively great at first (drive range), then
relatively small, and finally relatively great again (deceleration
range). The actuating accuracy is thus made relatively great in the
drive range and in the deceleration range, as it would indeed be
desireable in use. In between the accuracy of actuation, and with
it the inclination, may well be less. The gradient of the
generating line is preferably steeper in the drive range than in
the deceleration range according to the present invention.
In a preferred embodiment of the present invention a control
cylinder inlet, with a pressure line connecting to it, communicates
with that portion of the control cylinder chamber adjacent to the
control pressure end face of the control valve member through a
restrictor duct. This last-mentioned portion of the control
cylinder chamber communicates with a control nozzle, for
controlling the magnitude of the control pressure arranged ahead of
which is a control member loaded by a variable electromagnetic
force for controlling the control nozzle. The restrictor duct is
preferably located in the control valve member but may optionally
be provided also in the valve body. The control valve thus likewise
functions also as a pilot restrictor for the pressurization of the
control oil or for the control pressure circuit. For pressurization
of the control oil, hydraulic medium flows from the inlet of the
control cylinder, through the restrictor duct, into said portion of
the control cylinder chamber and into a control pressure chamber
surrounding the area of the control nozzle inlet, in which spaces
the hydraulic medium backs up until it attains the control pressure
at which the force of control pressure acting on the control member
and the electromagnetic force are in equilibrium. In this balanced
condition the control nozzle is in a somewhat open position and
allows control pressure medium to escape from it continuously. When
a change occurs in the electromagnetic force, a new control
pressure results, the force of which on the control valve is equal
to the new electromagnetic force. The continuous flow of medium
through the restrictor duct and the control nozzle also serves to
cool the actuating means of the hydraulic actuator.
The actuating means of the present invention can be used, e.g., for
varying the blade angle of the guide vanes of an inlet stator of a
power turbine of a two-spool gas turbine engine.
These and further objects, features and advantages of the present
invention will become more obvious from the following description
when taken in connection with the accompanying drawings which show,
for purposes of illustration only, several embodiments in
accordance with the present invention.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGS. 1 and 2 of the accompanying drawings are longitudinal
sections illustrating an embodiment of the actuating means
assembled in accordance with the present invention for varying the
blade angle of gas turbine guide vanes of a vehicular gas turbine
engine, where FIG. 1 shows the hydraulic actuator with its
actuating piston and control valve in a section taken at their
centerlines (longitudinal section) and FIG. 2 shows in longitudinal
section the transducer furnishing the control pressure;
FIG. 3 of the drawings illustrates an alternative preferred
embodiment of the control valve and body in a section taken at the
centerline of the control valve and at right angles to the
centerline of the actuating piston; and
FIG. 4 of the drawings illustrates a further alternative preferred
embodiment of a control valve body and valve as seen in partial
longitudinal section from FIG. 1.
DETAILED DESCRIPTION OF THE DRAWINGS
The actuating means of FIGS. 1 and 2 essentially comprise an
actuator (FIG. 1) exhibiting a cylindrical actuating piston 10 and
a cylindrical control valve 11, and a transducer (FIG. 2) in the
form of an electromagnetic device for motivating a control member
46 for a control nozzle 21, where the member 46 is under a magnetic
force which varies proportionally to the variation in input voltage
-- arrowheads 88 -- to a solenoid 47.
The centerline 30 of the actuating piston and the centerline 36 of
the control valve 11 are at right angles to one another and in the
plane of projection. The actuator housing essentially consists of a
cylinder 12 accommodating the actuating piston 10, and a cylinder
head 13 accommodating the control valve 11. The cylinder 12 and its
head 13 are fixedly connected, more particularly screwed, one to
the other, or they may alternatively be a solid construction. The
cylinder head 13 is essentially about centerline 30. The cylinder
head 13 and the actuating piston 10 are each fitted with a lug 63
and 64, respectively. Lug 63, which stiffens the cylinder head 13
to resist distortion constitutes a fixed point of the actuator,
while lug 64 connects - this is not shown - to a guide vane
actuating ring gear via further connecting members and absorbs the
load. See the above-mentioned British Pat. No. 1,055,319 for a
showing of a system with guide vanes and mechanism for adjusting
same.
One face 14, of the actuating piston 10 is half the size of another
face 15, part of which face 14 is formed by an axially arranged
central cavity 16. An oil pump, details omitted on the drawing,
supplies oil pressure p to face 14 through a pressure line 60
(arrowhead 89) extending from the pump. Installed in pressure line
60 is a pressure limiter valve 44 set at the maximum allowable oil
pressure. The cavity 16 and the adjacent members in the interior of
the actuator form a chamber which is filled with oil and closed off
by control valve 11. The actuating piston 10 is at rest in the
position illustrated in FIG. 1.
In this control chamber a double-armed lever 20 is carried on
knife-edge on a bearing member 19 of a cylindrical cover fixedly
connected to head 13. The lever 20 extends through an opening in
the cover and can be loaded flexurally in that its upper arm as
seen in the drawing consists of a relatively short and relatively
stiff portion. Attached to said upper arm, by riveting or
otherwise, is a relatively long leaf spring 23 with a ball and
socket 25 or alternatively a sliding member or a roller at its
extreme end. This leaf spring 23 is disposed fully within cavity 16
as illustrated. Ball 25 rests against the generating line of the
cavity 16, whereas the end of the other arm of lever 20 forks
around a centrally arranged cylinder control valve member 51
flattened on both sides at that point. The one visible (FIG. 1) of
the two flattened lands, which are arranged symmetrically with
respect to the plane of projection, is indicated with the numeral
35. The two parts of the fork, which approximately takes up the
outer half of said arm, contact with their rounded ends with the
two equidirectional faces 39 of the two lands 35 in the
longitudinal plane 40 of the control valve 11 at right angles to
the plane of projection. In this manner a balance undisturbed by
tilting moment is achieved between the spring force of lever 20 and
a force acting axially on control valve 11 of a control pressure p'
of the oil.
The lever 20 or its leaf spring 23 are preloaded by this force of
control pressure. The control pressure p' comes to bear in a
portion 41 of the control cylinder chamber, in a hole of an
adjacent member, in a connecting line 43 -- for which see FIG. 1,
and FIG. 2 for its connecting portion -- and in a control pressure
chamber 45 of the transducer. Control pressure p' acts on a control
pressure end face 48 of the control valve 11. With the respective
force of control pressure being equal to the preload on the lever;
the control valve 11 is at rest.
The generating line or surface of the cavity 16 is formed to suit
an intended or given characteristic, i.e., to suit the intended
travels of the actuating piston, ultimately the desired change in
blade angle of the guide vanes, as a function of said input
voltage, or the control pressure p' proportional to it or the
magnetic force. The characteristic schematically depicted to the
right of the actuating cylinder 12 in FIG. 1, includes two
relatively flat and short straight lines, line 26 for drive range
.DELTA. s.sub.F and line 28 for deceleration range .DELTA. s.sub.B
of the guide vanes, and a relatively steep and long straight
intermediate line 27 for an intermediate range with a neutral
position s.sub.N of the actuating piston 10 or of the guide vanes.
The full travel of the actuating piston is indicated with the
symbol .DELTA. s.sub.G. Accordingly, the generating line consists
of two short, straight and, with respect to centerline 30,
relatively steep runs 31, for drive range .DELTA. s.sub.F, and 33,
for deceleration range .DELTA. s.sub.B, and of a relatively flat
and long straight intermediate run 32. The ball 25 rests against
the straight run 33 in the illustrated rest position.
The control valve 11 and the cylinder head 13 are simple
constructions. The control valve 11 exhibits, at each end of valve
member part 51, a cylindrical member part 49 and 50, respectively,
having a diameter larger than that of valve member 51 and, at the
level of the respective said end, an inlet control edge 52 and an
outlet control edge 53, respectively. The control cylinder 54 and
the cylinder head 13 respectively exhibit an annular inlet slot 55
controlled by inlet edge 52 and an annular outlet slot 56
controlled by outlet edge 53. This inlet connects to a pressure
line 61 diverted from pressure line 60. The annulus 57 surrounding
the valve memmber 51 forms part of the control chamber. The
distance of the edge 52 and 53 from one another is equal to that
between the two inner controlling edges of annular slots 55 and
56.
The pressure line 61 connects to an inlet duct 62 which in turn
connects to annular inlet slot 55. The annular inlet slot 55
communicates with portion 41 of the cylinder chamber via an annular
slot, an axially arranged central hole and an axially arranged
central restrictor port 42 of the control valve 11 or the valve
member 49, causing pressure oil to flow from the annular inlet slot
55 into portion 41 of the cylinder chamber for duty as control
pressure oil. The force of control pressure of the oil acting on
control member 46 (FIG. 2) is in balance with the magnetic force
applied by solenoid 47, solenoid 47 being of known construction.
Control nozzle 21 is always in a somewhat open position and allows
oil to drain continuously into an oil reservoir not shown on the
drawings, as indicated by arrowhead 90. The extent of opening of
control nozzle 21, and hence the value of control pressure p' is
controlled by voltage input 88. The control pressure p' is
therefore always smaller than the oil pressure p prevailing in the
annular inlet slot 55.
With reference now to FIG. 2, it is noted that the control pressure
p' acts, in control pressure chamber 45, on a diaphragm 17 and, via
a connecting duct 38 in a control pressure chamber 22, on a
diaphragm 18 the effective portion of which is somewhat smaller
than that of diaphragm 17, so that the resulting force of oil
pressure on control member 46, which is in fixed and oil-tight
connection with diaphragms 17 and 18, is very modest and therefore
requires not more than an equally modest magnetic force and, thus,
only a relatively small-sized electromagnetic means.
Annular outlet slot 56 communicates with an outlet duct 29 from
which a drain line 37 leads to an oil reservoir not shown on the
drawings, as indicated by arrowhead 91. A gland leakage line
(dashed line at right side of FIG. 1) likewise discharges into this
reservoir. In order to attenuate axial vibrations of control valve
11, this outlet of the control cylinder and a portion 59 of the
control cylinder chamber adjacent to the end face 58 of control
valve 11 are in communication through a damping duct formed in
valve body 13 by a slot 24 extending in parallel with centerline
36.
When the input voltage 88 falls off, the magnetic force is reduced,
the control nozzle 21 is opened wider and the control pressure p'
is thus reduced until balance is established between the associated
force of control pressure on control member 46 and the reduced
magnetic force. When the input voltage is raised, the process is
reversed. The oil pressure p in the annular inlet slot 55 is the
maximally attainable control pressure p' for the reasons noted
above. Any reduction or rise in control pressure p' causes the
control valve 11 to move from its shut-off position in its one
axial direction, or opposite it, to establish communication between
the annular inlet slot 55 and the cavity 16 or between it and the
annular outlet slot 56. This causes face 15 to come under oil
pressure p and the actuating piston 10 to be moved away from
control valve 11, or actuating piston 10 to be moved in the
opposite direction as the control chamber is being emptied
accordingly. In the process of movement of actuating piston 10, the
form of the generating line causes the ball and socket 25 to travel
farther apart from centerline 30 or closer to it, or the preload on
the lever to fall or rise until balance is established with the new
force of control pressure, thus pushing control valve 11 back to
its shut-off position. The actuating piston 10 therefore comes to
rest very accurately in the position that relates to control
pressure p' or the input voltage producing it.
The control valve 79 and the cylinder head 78 shown in FIG. 3 are
equally simple constructions. This cylindrical control valve 79,
here shown in its shut-off position, exhibits a centrally arranged
cylindrical valve member 70 having an inlet control edge 71 at its
one end and an outlet control edge 72 at its other. The control
chamber (cavity 16 and portion opening to the control valve are
described in FIG. 1 above) leads, with a cylindrical duct or
opening 73, to the valve member 70 where it is as wide as the
distance 74 between control edge 71 and control edge 72. The
diameter of the duct 73 is equal to this distance 74. The two fixed
edges are formed by the wall of duct 73 and the wall of a control
cylinder 75. The control cylinder 75 exhibits, outside the valve
member 75 axially, an uncontrolled inlet duct 76 on the one axial
side and an uncontrolled outlet duct 77 on the other. This FIG. 3
control valve operates in the FIG. 1 system in a manner as
described above for control valve 11.
In accordance with the arrangement in FIG. 4 a control valve 11 is
seated for sliding movement in a bushing 80 having a controlled
inlet slot 81 and a controlled outlet slot 82 and being seated in a
cavity 84 of the actuator housing, here of cylinder head 83. The
bushing 80 is connected, at the seating port of cavity 84, with
cylinder head 83 for a fixed position axially but at a distance
radially from the cavity 84. When a load is applied at a lug 64
(see FIG. 1) with the actuator housing secured in an abutment lug
63 (see FIG. 1) of cylinder head 83, the forces occurring in the
cylinder head 83 will not affect the control valve 11 if use is
made of this bushed design. This FIG. 4 arrangement otherwise
operates as described in connection with FIG. 1.
Sealing rings, here represented by O-rings, arranged between the
bushing 80 and the cavity 84 serve to seal differently pressurized
chambers one from the other. So that bushing 80 may readily permit
insertion axially in cylinder head 83 the outer diameter of the
bushing and the inner diameter of the cavity are widened counter
the direction of insertion in several steps. As a result the
O-rings will be seated, as shown, between the respective bushing
sections and cavity sections.
While we have shown and described several embodiments in accordance
with the present invention, it is understood that the same is not
limited thereto but is susceptible of numerous changes and
modifications as known to those skilled in the art and we therefore
do not wish to be limited to the details shown and described herein
but intend to cover all such changes and modifications as are
encompassed by the scope of the appended claims.
* * * * *