U.S. patent number 3,561,392 [Application Number 04/769,289] was granted by the patent office on 1971-02-09 for unit of propulsion by hydrodynamic reaction.
Invention is credited to Guillermo Federico Baez.
United States Patent |
3,561,392 |
Baez |
February 9, 1971 |
UNIT OF PROPULSION BY HYDRODYNAMIC REACTION
Abstract
The improved unit of propulsion by hydrodynamic reaction
consists of an integral turbine which has a pair of adjacent,
counterrotating rotors, driven either by one motor through suitable
gearings, or by two separate motors. The casing which encloses this
counterrotating turbine ends in a nozzle. A conical or bullet
shaped element provided with one or two baffles is housed in the
casing between the second rotor and the nozzle and directs the jet
towards the said nozzle which has movable sidewalls for regulating
the outlet.
Inventors: |
Baez; Guillermo Federico
(Buenos Aires, AR) |
Family
ID: |
3461524 |
Appl.
No.: |
04/769,289 |
Filed: |
October 21, 1968 |
Foreign Application Priority Data
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|
|
|
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Oct 23, 1967 [AR] |
|
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210,440 |
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Current U.S.
Class: |
440/43 |
Current CPC
Class: |
B63H
11/103 (20130101); B63H 23/14 (20130101); B63H
2011/081 (20130101); B63H 2023/0216 (20130101); B63H
2011/085 (20130101) |
Current International
Class: |
B63H
23/14 (20060101); B63H 5/00 (20060101); B63H
5/16 (20060101); B63H 11/00 (20060101); B63H
23/00 (20060101); B63H 11/103 (20060101); B63h
011/10 () |
Field of
Search: |
;115/12,14,16
(Cursory)/ |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Buchler; Milton
Assistant Examiner: O'Connor; G.
Claims
I claim:
1. A hydrodynamic-reaction propulsion unit comprising:
A casing for attachment along the keel of a vessel, said casing
including an upstream fluid inlet and a downstream fluid outlet
nozzle;
means to provide counterrotation within said casing and to
eliminate cavitation therewithin comprising turbine rotor means in
said casing between said inlet and outlet for generating fluid
pressure in the casing to be emitted from said outlet nozzle, said
turbine rotor means comprising two coaxial adjacent,
counterrotating rotors, each said rotor carrying a plurality of
blades, the blades of one rotor having a reversed helical pitch
relative to the blades of the other rotor;
power means operatively connected to said coaxial adjacent rotors
for rotating each said rotor in an opposite direction to each other
and about a longitudinal axis extending generally along the keel to
which said casing is attached;
means to regulate and maneuver operatively connected to said casing
in relation to said outlet nozzle for controlling fluid pressure
emission relative to the axis of said turbine rotor means
comprising opposed sidewall portions of said outlet nozzle, said
opposed sidewall portions comprising plates hinged intermediately
of said sidewalls and including upstream and downstream portions
positionable into or out of said outlet nozzle; and
at least one internal baffle means downstream from said two coaxial
adjacent turbine rotors, said internal baffle means extending
longitudinally.
Description
The present invention refers to an improved unit of propulsion by
hydrodynamic reaction. The application of reaction to propulsion
has been known and used for some years and this principle, which is
commonly known as "Jet Propulsion," both in aircraft and in
waterborne vessels, consists of exerting and forcing out a charge
in the opposite direction to that in which it is desired to travel;
said charge being a heated gas when used in aviation and water when
used in a vessel.
The well-known method of propulsion by hydrodynamic reaction
consists of an intake opening in or near the keel of the vessel,
provided with a filter-screen, a horizontal shaft directly coupled
to a motor passing through a substantially horizontal tubular
casing connected to said intake opening, an outlet in the form of a
nozzle provided with jet-regulating means, a plurality of turbine
wheels or rotors provided with fixed blades attached to said shaft
and a corresponding set of stationary wheels, or stators, similarly
provided with fixed blades, duly interposed between said rotors,
the whole series of rotors and stators ending with a stator so as
to transform the resulting helicoidal current into an axial current
that is ejected from the nozzle and moves the craft.
The above description of a unit is merely given as an example and
can be modified in different ways and parts to increase output or
efficiency, facilitate maneuvering, etc.
The present invention, based upon the method described above,
introduces the principle of counterrotation between turbine wheels,
whereby a substantially improved unit of hydraulic propulsion is
obtained and the vessel becomes more readily maneuverable; the
novel unit of propulsion by reaction also having an improved outlet
nozzle.
DESCRIPTION
When compared with the known jet propulsion units consisting of a
series of rotors and stators the last of which is a stator, the
improved unit of the present invention presents the following
advantages:
1. Immediate production of high pressure, due to counterrotation,
allowing of high speed starting.
2. Improved hydrodynamic efficiency, due to the reduction of
friction surfaces and fewer changes in the direction of flow.
3. Better equilibrium due to the torsion-coupling of
counterrotation.
4. Reduction in volume of the propulsion unit. This reduction can
be as much as 50 percent without modification of the power unit or
loss of efficiency.
5. Potential production of super pressure in cases of
emergency.
When applied exclusively to marine and river vessels the improved
unit presents certain inherent advantages derived from reaction
propulsion, namely:
1. Navigation in shallow waters.
2. Navigation in muddy or weedy waters.
3. Elimination of many causes of breakdown.
A special advantage of the improved unit is in its more efficient
yield of motor power due to the elimination of cavitation in the
interior of the same, such as often occurs in conventional turbines
at high speed, when this cavitation unavoidably reduces the
efficiency of the plant.
Compared with multistep, hydrodynamic turbine pumps consisting of
alternately disposed rotors and stators, the improved unit of the
present invention is of much simpler construction and therefor
enjoys a far more unlikely retention of foreign matter that could
penetrate into the propulsion cavity, as occurs frequently in the
case of units with several stages of rotors and stators, or
fixed-flow directing blades.
One preferred embodiment of the improved unit of hydrodynamic
propulsion by reaction is characterized in that the integral
turbine of this unit consists of a pair of coaxial adjacent,
counterrotating rotors, mounted upon coaxial shafts, the inner of
which shafts carries one of said rotors fixed to same, while the
other rotor is fixed upon the outer shaft, which outer shaft is
operatively coupled to the motor through the inner shaft and by a
suitable reverse rotating gear; the interior of the casing
enclosing said rotors being provided with a pair of fixed,
directing baffles, disposed diametrically opposite each other and
extending longitudinally within the tubular outlet end of the
casing which ends in a nozzle provided with movable sidewalls that
can be regulated.
In another embodiment the two rotors are coupled to two separate,
counterrotating engines, such as are used in many screw-driven
river boats, which may thus be transformed into turbine-propelled
crafts with a minimum of modifications.
IN THE DRAWINGS
FIG. 1 shows a longitudinal section of the propulsion unit in
position for advance at full throttle.
FIGS. 2, 2a, 2b, 2c and 2d show various positions in plan of the
regulating means in the unit that offer the different maneuvering
possibilities.
FIG. 3 is a transverse section of the propulsion unit through line
III-III in FIG. 1 to indicate the position of the current aligning
baffles.
FIG. 4 is a view in plan of one of the aligning baffles illustrated
in FIG. 3.
FIG. 5 is a modified embodiment of the unit illustrated in FIG.
1.
FIG. 6 is a schematic longitudinal section of a propulsion unit
powered by two separate, counterrotating engines.
FIG. 7 is a diagram showing the average theoretical vectorial
values of the counterrotation applied in the improved propulsion
unit.
The propulsion unit consists of a casing 1 of substantially
horizontal channel shape having an enlarged, downwardly inclined
end terminating in an inlet opening 2, in the keel of the craft,
protected by a screen to prevent the entry of foreign matter. The
other end 4 of said casing 1 is reduced truncoconically and
finishes in a nozzle 5 of prismatic shape and preferably of
rectangular cross section. The casing 1 is provided with a tubular,
longitudinal shaft 6 that carries one rotor or set of turbine
blades 7, and a solid shaft 8 that passes coaxially through the
said tubular shaft 6 and extends beyond both ends of same. At one
end, adjacent the rotor 7, the interior shaft 8 carries a rotor 9
the blades of which are preferably inclined in the opposite
direction to that of the blades of the rotor 7 on the outer,
tubular shaft 6. At the other end said interior shaft 8 is coupled
to a motor (not shown in the drawings). The outer, tubular shaft 6
is coupled to the motor through the inner shaft 8 by means of a
planetary reversing gear in which the gear wheel 10 engages gear
wheel 12 through a pinion 11, said gear wheel 12 being fixedly
disposed upon the tubular, outer shaft 6, whereby the inner shaft 8
receives approximately two thirds of the motor power and the outer,
tubular shaft 6 receives approximately one third of said power
during their respectively contrary revolutions.
The inlets of shafts 6 and 8 on the casing 1 are provided with
adequate glands to prevent the entry of water and the portion of
the casing 13 that encloses the gear-wheels 10, 11 and 12 is
disposed at a suitable distance from the main body of said casing
1. These glands are not shown in the drawings, being of any
suitable type and the portion 13 of the casing is not the only form
in which the gear-wheels can be enclosed, neither do these
gear-wheels indicate the only manner in which counterrotation could
be applied to the rotors.
The truncoconic reduction 4 of the casing 1 that forms the outlet
for the turbulent liquid is provided internally with a pair of
diametrically opposed baffles 14, 14a, that extend longitudinally
within the unit. As can be seen in FIG. 4 these fixed blades or
baffles 14, 14a consist respectively of flat plates having curved
ends where adjacent to the rotor 9, said curves being in the
direction of aligned current flow and therefore being curved in
opposite directions. These fixed baffles 14, 14a therefore serve to
align the flow of water that emerges with tangential movement at
high pressure from the second rotor 9, as the curved ends tend to
reduce the impact and help to avoid any sharp change in direction
of the current which thus suffers a minimum loss of power on being
changed from giratory to axial flow.
Inside the truncoconic reduction 4 of the casing a conic or
bullet-shaped element 18 is disposed so as to prevent the
turbulence of the flow of water which streams out of the second
rotor 9. This element 18 thus cooperates with the baffles 14, 14a,
and can be independent of the adjacent rotor 9, as in FIG. 1, in
which case it is stationary and fixed to the casing 4 by means of
the baffles 14, 14a, or it can be fixed to the rotor 9 or form part
of its body, as in FIG. 5, in which case only one baffle 14b is
necessary and sufficient space must be left between the
bullet-shaped element 18a which forms part of the rotor 9 and thus
rotates, and the said baffle 14b which is stationary.
The prismatic outlet nozzle 5 receives the current of water thus
aligned and this current is ejected from said nozzle as shown by
arrows. The embodiment of the propulsion unit as described so far
would require the addition of a rudder and other elements for
changing the direction and the speed of the craft. According to
this invention, however, the prismatic nozzle 5 has sidewalls
formed by hinged plates that allow of changes in velocity and
direction of the jet and thereby serve as rudder and movement
astern. One of said sidewalls of the nozzle 5 can be seen in FIGS.
1 and 5 and the opposite sidewalls is identical. Each of these
sidewalls consists of a vertical hinge-rod 15 upon which the two
halves 16, 17 of the wall articulate. These half-walls 16, 17 can
be moved independently of each other and the halves of one sidewall
are independently movable with respect to the halves that form the
opposite side of the nozzle 5.
When both halves 16, 17 of both sidewalls are aligned as
illustrated in FIGS. 1 and 2 the jet is at full force, as the
outlet is then open to the maximum extent. This position,
therefore, corresponds to cruising speed and straight ahead
steering. When the outer edges of the outer halves 17 are moved
towards each other, as shown in FIG. 2a, the outlet area is
reduced, thus reducing the size of the jet, while increasing the
velocity of flow by the consequent increase of pressure and thus
raising the forward speed of he craft. FIG. 2b shows the position
to which the two inner halves 16 can be moved to close the main
outlet area, whereby side outlets controlled by the outer halves 17
are opened. This position 2b of the sidewalls produces a current
that is contrary to the forward movement of the vessel, which then
proceeds astern. FIGS. 2c and 2d show different positions of the
outer halves 17, whereby the craft can be steered to port or
starboard. In the case of large vessels this method of steering can
be assisted by means of the conventional mechanical rudder. The
gear for manipulating said side-walls 16, 17 of the nozzle is not
shown, as this can be of any suitable type that brings this control
within reach of the steersman. This can, therefore, be brought to
end on an instrument panel that also carries the motor controlling
means and indicating dials.
In the case of screw driven boats provided with two independent
motors, as happens in some larger river boats, the same can be
converted to turbine power by making use of the said two motors 19,
19a, as shown schematically in FIG. 6. No planetary gearing is
required since the impulse is given independently through pulley
20, belt 21 and pulley 22 from motor 19 to shaft 6 and through
pulley 20a, belt 21a and pulley 22a from engine 19a to shaft 8.
FIG. 7 is a theoretical representation of the average vectorial
values of counterrotation in a propulsion unit according to the
present invention. For the sake of clarity only two obliquely
disposed blades are shown and an ideal laminar current is assumed,
without dynamic losses due to turbulence or friction and without
volumetric losses due to the ideal absence of cavitation while
assuming the blades to be infinitely thin.
In the case of blade 7 we have the following values:
U.sub.1-- average tangential velocity at entry.
Ve.sub.1-- Axial velocity at entry of fluid.
R.sub.1-- relative velocity of fluid in respect to the blade.
U.sub.2-- tangential velocity at outlet.
R.sub.2-- relative velocity of fluid at pressure outlet (angle
.alpha..sub.2).
Vs.sub.1-- Absolute velocity of the fluid at outlet.
In the case of the second rotor, or blade 9, there are the
following values:
U.sub.3-- average tangential velocity of counterrotation. The
relation between Vs.sub.1 and U.sub.3 determines the relative
velocity R.sub.4 and therefore indicates the inclination of the
blades that corresponds to the counterrotation of the second rotor
blade 9 resulting in angle .alpha..sub.3.
U.sub.4-- average tangential velocity at outlet.
R.sub.5-- relative velocity of fluid at pressure outlet in respect
to angle .alpha..sub.4.
Vs.sub.2-- Absolute velocity of the fluid at the outlet. The
theoretical exit-pressure of the first rotor is given
hydrodynamically by the formula
Where H-- Exit pressure,
U.sub.2-- average tangential velocity at outlet,
Vw.sub.2-- Tangential velocity of rotation,
G-- gravity.
The consequence of counterrotation first becomes apparent in the
second rotor blade 9 on comparing the absolute velocity Vs.sub.1 of
the fluid when this blade 9 is mounted on the rotor at an angle
.beta..sub.1 and not axially as the first rotor blade 7. These
functional conditions create a tangential velocity of rotation or
transformation of kinetic energy as follows;
Vw.sub.4 = Vw.sub.2 + Vw.sub.3
the values of which can be found from the graph of FIG. 7. By the
application of this formula a unit of hydrodynamic propulsion can
be constructed that has greater efficiency than that of any of the
hydrodynamic propulsion units known in the art.
While certain preferred embodiments of the present invention have
been illustrated and described herein, it is to be understood that
the invention is not limited thereby, but is susceptible of changes
in form and detail within the scope of the appended claims.
* * * * *