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US2429005A - Liquid fuel pump governor - Google Patents

Liquid fuel pump governor Download PDF

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Publication number
US2429005A
US2429005A US503090A US50309043A US2429005A US 2429005 A US2429005 A US 2429005A US 503090 A US503090 A US 503090A US 50309043 A US50309043 A US 50309043A US 2429005 A US2429005 A US 2429005A
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Prior art keywords
pressure
pump
chamber
speed
liquid fuel
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US503090A
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Watson Ernest Ansley
Ifield Richard Joseph
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ZF International UK Ltd
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Joseph Lucas Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/04Feeding by means of driven pumps

Definitions

  • This invention relates to governors for automatically controlling in response to variations of speed the supply of liquid fuel from a pump to a prime mover, the object of the invention being to provide an improved governing means of the kind which is dependentupon th ac on of fluid pressure, this pressure being dependent on the speed of the prime mover.
  • the invention comprises the combination with a main governing means of the kind specified, of a supplementary governing means responsive (directly or indirectly) to a rate of change of speed.
  • FIG. 1 is a diagrammatic sectional elevation of a liquid fuel pump embodying the invention.
  • Figures 2 to 4 are similar diagrammatic fragmentary sectional side views illustrating respectively three modified forms of the invention.
  • the liquid fuel pump shown in the drawings comprises a rotary body part a arranged in a casing b and having formed around its axis a plurality of bores as c in each ofwhich is arranged a reciprocatory plunger d.
  • the body part a is adapted to be driven in any convenient manner by the prime mover (not shown) to be su-pplied with liquid fuel from the pump.
  • the plungers d are moved in one direction by an angularly movable swash plate e and in the opposite direction by springs as f, the latter being situated within'the bores c, and serving tohold an end face of the body part in contact with a flat seating g in the casing b.
  • the seating g is formed with a port 71. communicating with a liquid inlet 2' in the casing b, and with another port 9' communicating with a liquid outlet 7c in the casing.
  • the body part a is adapted to serve also as a censition of maximum obliquity, that is to say the trifugal pum p.
  • the body part 'a is formed with an axial bore m which at one end communicates with the inlet 1' through another port n in the seating g, and at the other end communicates with a plurality of radial passages as o in the body part. Liquid from the inlet i flows through the bore m and is expelled by centrifugal Within inner end of the cylinder is a rod s connected'to cylinder (which contains the spring 1) through a restricted passage 15.
  • the outer end of the cylinder p is provided with a small vent u which at its outer end forms a seating for a closure member uo-n one end of a lever w, the latter being pivoted at a position intermediate its ends on the outer endof the cylinder, and being loaded by a spring a: which tends to hold the closure member on its seating.
  • the lever w is contained in a chamber :11 formed on or secured to the adjacent end of the casing b, and this chamber communicates with the pump inlet 1.
  • the outer side of the chamber y is'bounded by a controlling diaphragm 2 having at its centre an abutment 2 which is adapted to bear on the end of the lever w remote from the closure member 1).
  • the diaphragm z At the outer side of and bounded in part by the diaphragm z is another chamber 3, this latter chamber being in communication with the above.- mentioned centrifugal pump through a passage 4 in the casing b. Also the diaphragm z is loaded by a spring 5 connected to an adjusting member '5, the latter being operable in any convenient manner by an attendant to vary the effect of the spring.
  • the swash plate Assuming the swash plate e to be in the poposition in which the pump gives its maximum output, the swash plate will remainin this position so long as the pressure in'the chamber 3 (and thus acting on the controlling diaphragm z) is below some predetermined amount. In this condition the vent closure member 1) is in its closed position and the liquid pressures at the two sides of the piston q are equal. But when the pressure acting on the diaphragm z exceeds the predetermined amount the diaphragm will move the closure memberv oiT its seating.
  • the central portions of the compartments 9, which accommodate the rod Hand the spring 5 are-separated from the main portions of these compartments by any convenient seal such as flexible metal bellows l3. Also the main portions of the two compartments 9, iii are interconnected by a restricted passage i4, and the.
  • main portion of the outer compartment l 0 is provided with an inlet l5 whereby it canbe connected to an airblower (not shown) driven by the prime mover, or to any other source of fluid pressure which varies with changes of speed of the prime mover.
  • an airblower (not shown) driven by the prime mover, or to any other source of fluid pressure which varies with changes of speed of the prime mover.
  • compartments 9, ID are equal, but rapid increase in the speed of the prime-movercauses pressure to be built up in the outer. compartment Ill and this pressure is transmitted through the second diaphragm 8 to the first diaphragm z for actuating the lever to of the closure member 11.
  • the required additional pressure in the chamber 3 is obtained by means of a piston 2 l which forms the movable core of an electromagnet, having an energising winding 22, the latter being supplied with current from a generator whose output is correlated with the speed of the prime mover and serving to move the piston against the action of a spring 24.
  • the additional pressure in the chamber 3 is obtained by means of a piston subject to the action of a centrifugal mechanism 26 which is responsive to the speed or the prime mover, and which serves action may be derived from a variety of dverent means (fluid, electromagnetic, or mechanical) adapted to exert pressure which is directly or indirectly dependent on change of speed of the prime mover.
  • Means for supplying liquid fuel to a prime mover comprising a variable-delivery pump having in combination a rotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate during rotary motion of the body part, an adjustable member for varying the stroke of the plungers and'thereby varying the output of the pump,
  • a main governing means adapted to vary the.
  • an adjustable member for varying the stroke of the varying the output of the transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump, and with a device responsive to fluid pressure dependent on the speed oi the said rotary body part for controlling the movement of the transmission member, and a supplementary governing means adapted to exert a further control on the movement of the transmission member by acting on the said device in response to the rate of change of the said speed.
  • Means for supplying liquid fuel to a prime mover comprising a variable-delivery pump having in'combination arotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate duringrotary motion of the body part, an adjustable member for varying the stroke of the plungers and thereby varying the output of the pump, a main governing means provided with a transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump, and with a device responsive to fluid pressure dependent on the speed of the said rotary body part for controlling a variable-delivery pump the movement of the transmission member, a supplementary governing means including a pressure-transmitting member movable by fluid pressure and adapted to exert a further control on the movement of the transmission-member in response to the rate of change of the said speed, and means connecting the said pressure-transmitting member to the said device.
  • Means for supplying liquid fuel to a primemover comprising a variable-delivery pump having in combination a rotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate during rotary motion of the body part, an adjustable member for varying the stroke of the plungers' and thereby varying the output of the pump, a main governing means provided with a transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump.
  • a device responsive to fluid pressure for controlling the movement of the transmission member a chamber bounded in part by the said device, a restricted passage through which fluid can enter the chamber at a pressure dependent on the speed of the said rotary body part, and a supplementary governing means comprising a cylinder in communication with the chamber, and a piston movable in the cylinder and adapted by varying the pressure in the said chamber to exert a further control on the movement of the transmission member in response to the rate of change of the said speed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electromagnetic Pumps, Or The Like (AREA)

Description

Patented Oct. 14, 1947 LIQUID FUEL PUMP GOVERNOR Ernest Ansley Watson and Richard Joseph Ifield, Birmingham, England, assignors to Joseph Lucas Limited. Birmingham, England Application September 20, v1943, Serial No. 503,090 In Great Britain May 28, 1942 7 Claims. (Cl. 103-162) This invention relates to governors for automatically controlling in response to variations of speed the supply of liquid fuel from a pump to a prime mover, the object of the invention being to provide an improved governing means of the kind which is dependentupon th ac on of fluid pressure, this pressure being dependent on the speed of the prime mover.
The invention comprises the combination with a main governing means of the kind specified, of a supplementary governing means responsive (directly or indirectly) to a rate of change of speed. I
In the accompanying sheet of explanatory drawings:
Figure 1 is a diagrammatic sectional elevation ofa liquid fuel pump embodying the invention.
Figures 2 to 4 are similar diagrammatic fragmentary sectional side views illustrating respectively three modified forms of the invention.
The liquid fuel pump shown in the drawings, comprises a rotary body part a arranged in a casing b and having formed around its axis a plurality of bores as c in each ofwhich is arranged a reciprocatory plunger d. The body part a is adapted to be driven in any convenient manner by the prime mover (not shown) to be su-pplied with liquid fuel from the pump. During rotation of the body part a the plungers d are moved in one direction by an angularly movable swash plate e and in the opposite direction by springs as f, the latter being situated within'the bores c, and serving tohold an end face of the body part in contact with a flat seating g in the casing b. The seating g is formed with a port 71. communicating with a liquid inlet 2' in the casing b, and with another port 9' communicating with a liquid outlet 7c in the casing.
To enable the pump above described to be governed in response tov variations in speed, the body part a is adapted to serve also as a censition of maximum obliquity, that is to say the trifugal pum p. Thus, the body part 'a is formed with an axial bore m which at one end communicates with the inlet 1' through another port n in the seating g, and at the other end communicates with a plurality of radial passages as o in the body part. Liquid from the inlet i flows through the bore m and is expelled by centrifugal Within inner end of the cylinder is a rod s connected'to cylinder (which contains the spring 1) through a restricted passage 15. The outer end of the cylinder p is provided with a small vent u which at its outer end forms a seating for a closure member uo-n one end of a lever w, the latter being pivoted at a position intermediate its ends on the outer endof the cylinder, and being loaded by a spring a: which tends to hold the closure member on its seating. The lever w is contained in a chamber :11 formed on or secured to the adjacent end of the casing b, and this chamber communicates with the pump inlet 1. The outer side of the chamber y is'bounded by a controlling diaphragm 2 having at its centre an abutment 2 which is adapted to bear on the end of the lever w remote from the closure member 1). At the outer side of and bounded in part by the diaphragm z is another chamber 3, this latter chamber being in communication with the above.- mentioned centrifugal pump through a passage 4 in the casing b. Also the diaphragm z is loaded by a spring 5 connected to an adjusting member '5, the latter being operable in any convenient manner by an attendant to vary the effect of the spring.
Assuming the swash plate e to be in the poposition in which the pump gives its maximum output, the swash plate will remainin this position so long as the pressure in'the chamber 3 (and thus acting on the controlling diaphragm z) is below some predetermined amount. In this condition the vent closure member 1) is in its closed position and the liquid pressures at the two sides of the piston q are equal. But when the pressure acting on the diaphragm z exceeds the predetermined amount the diaphragm will move the closure memberv oiT its seating. The liquid pressure in the outer portion of the cylinder p will now fall and the piston q will be moved by the fluid pressure in the inner portion of the cylinder against the action of the spring r, so moving the swashplate e" in the direction for reducing the pump output until a new condition of equilibrium is reached.
From the foregoing it will be seen that as th position of the swash plate e is dependent on the pressure oi the liquid in the chamber 3 and as this pressure is dependent on the speed of the pump,,the latter is governed by the speed of the prime mover which drives the pump.
In carrying the invention into effect we comblue with the chamber 3 supplementary governing means whereby additional pressure can be applied to the diaphragm z in of speed changes or the prime mover. Typical examples or such meansare illustrated in the drawings.
In the example shown in Figure 1 there is provided on the outer side or the chamber 3 another to move the piston against the action or a spring From the above described examples it will be seen that the required supplementary governing response'to the rate chamber which is divided by a second diaphragm 8 into two compartments 9, 10, this diaphragm being arranged parallel with the first diaphragm z, and being connected thereto by an axial rod l I passing through an opening I! in the adjacent side of the chamber 3. The outer compartment I is provided at its outer side with a central enlargement which accommodates the spring 5, the latter being connected at one end to the second diaphragm 8 and at the other end to the adjusting member 6. The central portions of the compartments 9, which accommodate the rod Hand the spring 5 are-separated from the main portions of these compartments by any convenient seal such as flexible metal bellows l3. Also the main portions of the two compartments 9, iii are interconnected by a restricted passage i4, and the.
main portion of the outer compartment l 0 is provided with an inlet l5 whereby it canbe connected to an airblower (not shown) driven by the prime mover, or to any other source of fluid pressure which varies with changes of speed of the prime mover.
Normally the fluid pressures in the compartments 9, ID are equal, but rapid increase in the speed of the prime-movercauses pressure to be built up in the outer. compartment Ill and this pressure is transmitted through the second diaphragm 8 to the first diaphragm z for actuating the lever to of the closure member 11.
In the example shown in Figure 2 the additional pressure is applied to the diaphragm 2 through the liquid in the chamber 3. Thus we provide in communication with the chamber 3 the larger end of a stepped, cylinder l6 containing a correspondingly stepped piston I! loaded by a spring l8, the smaller end of the cylinder being connected by a pipe I! to the pump outlet above described. Also the passage 4 connecting the chamber 3 with the centrifugal pump is provided with a restriction .which enables additional pressure to be established in the chamber by the action of the stepped piston l'l. With increasing pressure in the pump outlet the piston l1 moves against the action of its spring I! and displaces liquid from the cylinder i6 to the chamber '3,
thereby producing inthe chamber an additional pressure which is dependent on the rate of change of pressure in the pump outlet and the size of the restriction 20 in the passage 4.
In the example shown in Figure 3, the required additional pressure in the chamber 3 is obtained by means of a piston 2 l which forms the movable core of an electromagnet, having an energising winding 22, the latter being supplied with current from a generator whose output is correlated with the speed of the prime mover and serving to move the piston against the action of a spring 24.
In the example shown in Figure 4, the additional pressure in the chamber 3 is obtained by means of a piston subject to the action of a centrifugal mechanism 26 which is responsive to the speed or the prime mover, and which serves action may be derived from a variety of diilerent means (fluid, electromagnetic, or mechanical) adapted to exert pressure which is directly or indirectly dependent on change of speed of the prime mover.
By the use with a main fluid-operated governing means of a supplementary governing means responsive to and operative during a change of speed as above described, we are able to obtain a more satisfactory control of the fluid supply consequent on changes in the speed of the prime mover than is obtainable with the main governing means alone.
The invention is not, however, restricted to the examples given, as subordinate details may be varied to suit different requirements. Moreover the invention is applicable to liquid fuel pumps other than that above described,
Having thus described our invention what we claim as new and desire to secure by Letters Patent is: i
1. Means for supplying liquid fuel to a prime mover, comprising a variable-delivery pump having in combination a rotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate during rotary motion of the body part, an adjustable member for varying the stroke of the plungers and'thereby varying the output of the pump,
a main governing means adapted to vary the.
during rotary motion of the body part, an adjustable member for varying the stroke of the varying the output of the transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump, and with a device responsive to fluid pressure dependent on the speed oi the said rotary body part for controlling the movement of the transmission member, and a supplementary governing means adapted to exert a further control on the movement of the transmission member by acting on the said device in response to the rate of change of the said speed.
3. Means for supplying liquid fuel to a prime mover, comprising a variable-delivery pump having in'combination arotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate duringrotary motion of the body part, an adjustable member for varying the stroke of the plungers and thereby varying the output of the pump, a main governing means provided with a transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump, and with a device responsive to fluid pressure dependent on the speed of the said rotary body part for controlling a variable-delivery pump the movement of the transmission member, a supplementary governing means including a pressure-transmitting member movable by fluid pressure and adapted to exert a further control on the movement of the transmission-member in response to the rate of change of the said speed, and means connecting the said pressure-transmitting member to the said device.
4. Means for supplying liquid fuel to a primemover, comprising a variable-delivery pump having in combination a rotary body part provided with a plurality of bores, fluid inlet and outlet passages with which the bores communicate during rotary motion of the body part, an adjustable member for varying the stroke of the plungers' and thereby varying the output of the pump, a main governing means provided with a transmission member adapted to vary the position of the adjustable member under the pressure of fluid delivered by the pump. a device responsive to fluid pressure for controlling the movement of the transmission member, a chamber bounded in part by the said device, a restricted passage through which fluid can enter the chamber at a pressure dependent on the speed of the said rotary body part, and a supplementary governing means comprising a cylinder in communication with the chamber, and a piston movable in the cylinder and adapted by varying the pressure in the said chamber to exert a further control on the movement of the transmission member in response to the rate of change of the said speed.
5. Means as claimed in claim 4, in which the piston is movable by fluid pressure.
6. Means as claimed in claim 4 and having electromagnetic means for actuating the piston. '7. Means as claimed in claim 4 and having a c'entrifugal mechanism for actuating the piston.
ERNEST ANSLEY WATSON. RICHARD JOSEPH mam.-
. REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US503090A 1942-05-28 1943-09-20 Liquid fuel pump governor Expired - Lifetime US2429005A (en)

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Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2502546A (en) * 1947-03-28 1950-04-04 Denison Eng Co Hydraulic apparatus
US2555445A (en) * 1944-06-05 1951-06-05 Lucas Ltd Joseph Pump control means
US2606419A (en) * 1947-02-08 1952-08-12 Weatherhead Co Hydraulic speed control apparatus for regulating the fuel supply for combustion engines
US2621913A (en) * 1949-07-26 1952-12-16 Lucas Ltd Joseph Hydraulic governor for internal-combustion prime movers
US2659425A (en) * 1949-08-22 1953-11-17 Lucas Ltd Joseph Liquid fuel regulating means for use with prime movers
US2669094A (en) * 1947-02-01 1954-02-16 Niles Bement Pond Co Fuel control apparatus for jet engines
US2674191A (en) * 1949-08-22 1954-04-06 Lucas Ltd Joseph Hydraulic speed governor for prime movers
US2678698A (en) * 1946-11-15 1954-05-18 Niles Bement Pond Co Fuel and torque control apparatus for aircraft propulsion systems
US2686498A (en) * 1948-11-15 1954-08-17 Lucas Ltd Joseph Liquid fuel control system
US2687291A (en) * 1952-07-10 1954-08-24 Lucas Industries Ltd Hydraulic speed responsive pump and motor type governor
US2705590A (en) * 1949-10-28 1955-04-05 Rolls Royce Multi-stage axial-flow compressors with adjustable pitch stator blades
US2720752A (en) * 1950-02-10 1955-10-18 Niles Bement Pond Co Turbo-jet engine control
US2722894A (en) * 1949-02-09 1955-11-08 Lucas Ltd Joseph Fuel pump governor
US2738648A (en) * 1949-06-14 1956-03-20 Gen Electric Liquid fuel control system for a rocket engine
US2741089A (en) * 1951-01-26 1956-04-10 Armstrong Siddeley Motors Ltd Controlling fuel supply for an aircraft gas turbine engine during acceleration at different altitudes
US2741086A (en) * 1950-04-26 1956-04-10 Bendix Aviat Corp Automatic starter control
US2757511A (en) * 1951-01-26 1956-08-07 Armstrong Siddeley Motors Ltd System for regulating the supply of liquid fuel to a gas turbine
US2861422A (en) * 1951-06-18 1958-11-25 Herbert L Magill Power gas generator
US2910008A (en) * 1954-12-23 1959-10-27 Bendix Aviat Corp Pump
US2919548A (en) * 1952-11-26 1960-01-05 Rolls Royce Prime mover with means to control injection of cooling fluid into working medium thereof
US2939522A (en) * 1954-07-27 1960-06-07 Rolls Royce Fuel systems of gas turbine engines
US2946189A (en) * 1954-07-14 1960-07-26 Rolls Royce Fuel systems of gas-turbine engines
US3018621A (en) * 1956-07-26 1962-01-30 Bendix Corp Control apparatus for internal combustion engine
US3032983A (en) * 1959-09-11 1962-05-08 Curtiss Wright Corp Ramjet/afterburner tailpipe temperature and pressure limiter
US3080713A (en) * 1960-03-23 1963-03-12 Garrett Corp Load control valve for gas turbine compressors
US3089426A (en) * 1958-09-17 1963-05-14 New York Air Brake Co Engine
US3183667A (en) * 1962-11-05 1965-05-18 Chrysler Corp Fuel control system for a gas turbine engine
US3186167A (en) * 1962-10-08 1965-06-01 Continental Motors Corp Control for gas turbine fuel pump system
US3212260A (en) * 1962-05-22 1965-10-19 Ass Elect Ind Stall trip protective device for gas turbines

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR468122A (en) * 1914-02-06 1914-06-29 Henry Mariolle Des Ets Four-wheeled kitchen
US1130659A (en) * 1910-07-29 1915-03-02 Nathaniel Baldwin Governor mechanism.
US1509695A (en) * 1922-08-26 1924-09-23 Charmilles Sa Ateliers Apparatus for governing prime movers
US2129828A (en) * 1935-07-05 1938-09-13 Chrysler Corp Pump
US2129886A (en) * 1935-07-05 1938-09-13 Chrysler Corp Pump
US2177098A (en) * 1936-05-15 1939-10-24 Waterbury Tool Co Power transmission
USRE21758E (en) * 1941-04-01 Power transmission
US2273670A (en) * 1940-03-04 1942-02-17 George M Holley Fuel injection control system
US2292125A (en) * 1940-08-30 1942-08-04 Lucas Ltd Joseph Rotary fluid pump

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE21758E (en) * 1941-04-01 Power transmission
US1130659A (en) * 1910-07-29 1915-03-02 Nathaniel Baldwin Governor mechanism.
FR468122A (en) * 1914-02-06 1914-06-29 Henry Mariolle Des Ets Four-wheeled kitchen
US1509695A (en) * 1922-08-26 1924-09-23 Charmilles Sa Ateliers Apparatus for governing prime movers
US2129828A (en) * 1935-07-05 1938-09-13 Chrysler Corp Pump
US2129886A (en) * 1935-07-05 1938-09-13 Chrysler Corp Pump
US2177098A (en) * 1936-05-15 1939-10-24 Waterbury Tool Co Power transmission
US2273670A (en) * 1940-03-04 1942-02-17 George M Holley Fuel injection control system
US2292125A (en) * 1940-08-30 1942-08-04 Lucas Ltd Joseph Rotary fluid pump

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555445A (en) * 1944-06-05 1951-06-05 Lucas Ltd Joseph Pump control means
US2678698A (en) * 1946-11-15 1954-05-18 Niles Bement Pond Co Fuel and torque control apparatus for aircraft propulsion systems
US2669094A (en) * 1947-02-01 1954-02-16 Niles Bement Pond Co Fuel control apparatus for jet engines
US2606419A (en) * 1947-02-08 1952-08-12 Weatherhead Co Hydraulic speed control apparatus for regulating the fuel supply for combustion engines
US2502546A (en) * 1947-03-28 1950-04-04 Denison Eng Co Hydraulic apparatus
US2686498A (en) * 1948-11-15 1954-08-17 Lucas Ltd Joseph Liquid fuel control system
US2722894A (en) * 1949-02-09 1955-11-08 Lucas Ltd Joseph Fuel pump governor
US2738648A (en) * 1949-06-14 1956-03-20 Gen Electric Liquid fuel control system for a rocket engine
US2621913A (en) * 1949-07-26 1952-12-16 Lucas Ltd Joseph Hydraulic governor for internal-combustion prime movers
US2674191A (en) * 1949-08-22 1954-04-06 Lucas Ltd Joseph Hydraulic speed governor for prime movers
US2659425A (en) * 1949-08-22 1953-11-17 Lucas Ltd Joseph Liquid fuel regulating means for use with prime movers
US2705590A (en) * 1949-10-28 1955-04-05 Rolls Royce Multi-stage axial-flow compressors with adjustable pitch stator blades
US2720752A (en) * 1950-02-10 1955-10-18 Niles Bement Pond Co Turbo-jet engine control
US2741086A (en) * 1950-04-26 1956-04-10 Bendix Aviat Corp Automatic starter control
US2741089A (en) * 1951-01-26 1956-04-10 Armstrong Siddeley Motors Ltd Controlling fuel supply for an aircraft gas turbine engine during acceleration at different altitudes
US2757511A (en) * 1951-01-26 1956-08-07 Armstrong Siddeley Motors Ltd System for regulating the supply of liquid fuel to a gas turbine
US2861422A (en) * 1951-06-18 1958-11-25 Herbert L Magill Power gas generator
US2687291A (en) * 1952-07-10 1954-08-24 Lucas Industries Ltd Hydraulic speed responsive pump and motor type governor
US2919548A (en) * 1952-11-26 1960-01-05 Rolls Royce Prime mover with means to control injection of cooling fluid into working medium thereof
US2946189A (en) * 1954-07-14 1960-07-26 Rolls Royce Fuel systems of gas-turbine engines
US2939522A (en) * 1954-07-27 1960-06-07 Rolls Royce Fuel systems of gas turbine engines
US2910008A (en) * 1954-12-23 1959-10-27 Bendix Aviat Corp Pump
US3018621A (en) * 1956-07-26 1962-01-30 Bendix Corp Control apparatus for internal combustion engine
US3089426A (en) * 1958-09-17 1963-05-14 New York Air Brake Co Engine
US3032983A (en) * 1959-09-11 1962-05-08 Curtiss Wright Corp Ramjet/afterburner tailpipe temperature and pressure limiter
US3080713A (en) * 1960-03-23 1963-03-12 Garrett Corp Load control valve for gas turbine compressors
US3212260A (en) * 1962-05-22 1965-10-19 Ass Elect Ind Stall trip protective device for gas turbines
US3186167A (en) * 1962-10-08 1965-06-01 Continental Motors Corp Control for gas turbine fuel pump system
US3183667A (en) * 1962-11-05 1965-05-18 Chrysler Corp Fuel control system for a gas turbine engine

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