US2621632A - Liquid fuel control mechanism for internal-combustion prime movers - Google Patents
Liquid fuel control mechanism for internal-combustion prime movers Download PDFInfo
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- US2621632A US2621632A US199258A US19925850A US2621632A US 2621632 A US2621632 A US 2621632A US 199258 A US199258 A US 199258A US 19925850 A US19925850 A US 19925850A US 2621632 A US2621632 A US 2621632A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/08—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor
- F15B11/12—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action
- F15B11/121—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action providing distinct intermediate positions
- F15B11/125—Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action providing distinct intermediate positions by means of digital actuators, i.e. actuators in which the total stroke is the sum of individual strokes
Definitions
- This invention relates to a liquid-fuel control mechanism for an internal combustion prime mover, and particularly a jet engine, gas turbine, or the like, the mechanism being of the kind which includes a throttle under the manual control of the driver.
- the object of the invention is to provide an improved mechanism adapted to prevent an excessively rapid rate of increase of supply of fuel to the prime mover in the event of an excessively rapid actuation of the manually operable throttle.
- the invention comprises the combination with a throttle, of a liquid-operated servo-mechanism for v actuating the throttle, and valving means associated with the servo mechanisrn for controlling the movement of the throttle, the valving means comprising a manually operable valve for controlling the extent of movement, and a valve movable in part in response to movement of the servo mechanism and in part to fluid pres,- s'ure for controlling the rate of movement of the throttle.
- Figure -1 is a sectional diagram illustrating a system which includes a fuel control means embodying the invention.
- Figure v2 is a sectional diagram'illustrating a modlfied'constructi'on of the said mechanism.
- the fuel control mecha ni'sm shown at the left hand side of the diagram is arranged in association with a known formoi' variable delivery liquid fuel pump, and means for controlling the pump output.
- the pump com-- prises a rotary body a contained in a housing?) and provided with 'reciprocatory plungers c whicjh co-operate with an angularly adjustable swash plated.
- liquid fuel enters the pump along the passage ⁇ 2 and is discharged along the passage 3.
- the swash plate is angularly ad'ju'stable by -:a servo-mechanism which comprises a piston fig slidable in a cylinder 71. and loaded by a spring 5.
- Liquid fuel can. enter the cylinder from the passage :7, and can emerge through a passage k to a -vent m which is controlled-by a valve n.
- the valven When the valven is closed, liquid acts. with equal pressures on the two sides of the piston g, and the spring 2' then moves the piston to the right for increasing thev obliquity of the swash plate, so enabling the causing it to move to the-left againsttheaction of the spring i for reducing the obliquityof the swash plate and thereby reducing the- 'pump output.
- the vent m and valve 11. are contained-in a chambered part 0 which is divided into two com-' partments by a flexible diaphragm p, and on the latter is mounted a lever q which carries the valve n.
- the lever 'q is loaded by a spring -r and is subject to the pressure of the liquid fuel in the-pas-' sage fwhich pressure acts on the lever through a plunger s.
- the lever is subject to atmospheric pressure admittedto the said body part at i, this pressure acting on the lever through an evacuated deformable capsule a.
- the pump output is under the automatic control of atmospheric pressure and thepressure in communication with a passage a leading from the said housing.
- One side of the chamber w is bounded by a flexible diaphragm y loaded by a tension spring z, and to the diaphragm is connected by a stem 3 a lever 4' carrying a valve ,5
- an axially slid'able throttle l I having at one end a conical or otherwise suitably shaped endior varying the eil'ective size of the throat. ⁇ 0.
- the other end of I the throttle has formed on or secured to it 'a' piston 1-2 slida-ble in a cylindrical chamber 43 m described: are already known, and are described only as-an' the body part I, the side of the piston remote from the throttle being loaded by compression springs, I4, I5.
- the spring I 4 is supported at one end by a shoulder in the chamber I3.
- the other spring I5 serves to transmit motion from the piston I2 to a valve I6 to be hereinafter described.
- the cylindrical chamber I3 opens into a compartment I! which is bounded at one side by one of a pair of flexible and interconnected coaxial diaphragms I8, I9 of diiferent effective areas, these diaphragms being loaded by another spring 20.
- admits atmospheric or other related pressure from the part above described, to the region between the diaphragms, and a chamber 22 associated with the diaphragm I9 is adapted to receive liquid from the pipe 1: at a pressure related to the speed of the prime mover.
- the diaphragms I8, I9 are interconnected by an annulus 24.
- a duct 25 terminating in a vent 26 with which co-operates the normally-closed valve I carried by the diaphragm I8. Motion is transmissible from the spring I5 to this diaphragm and valve by a thrust piece 2'! which is gapped so that it extends around the duct 25.
- the duct 25 communicates with a passage 28 in the part I leading to the end of the cylindrical chamber I3 below the piston, which end is also in communication with the liquid fuel inlet 8 through a restricted orifice 29.
- an axial bore is formed in the throttle II and piston I2 and in this bore is contained a slidable valve 30 controlling ports 3
- the other end of the valve 30 extends through the throttle and the adjacent portion of the body part, and at its outer end is adapted for attachment to any convenient manually operable actuating means.
- the action of the mechanism is as follows: Starting with the throttle I in any steady working position, the valve I6 is closed and the valve 30 is open. Liquid can then flow past the valve 30 and through the piston I2 to the passage 32 leading to a sump or to the inlet passage e of the pump. To obtain an increased rate of fuel supply the driver moves the valve 30 to any desired extent for closing the ports 3
- the modification shown in Figure 2 is essentially similar in principle to the mechanism above described and differs mainly in certain details of arrangement.
- a cylindrical chamber I3 which contains the piston I2 and compression spring I4.
- the throttle II extends from the piston through a throat I0 lying between the liquid fuel inlet passage 8' and outlet passage 9.
- the inlet 8 communicates with one end of the chamber I3, and liquid can pass to the other end of the chamber through a restricted orifice 29 in the piston.
- From the throttle extends a stem 34, and through the piston, throttle, and a part of the stem is formed an axial passage leading to ports 3
- the manually operable valve controls the inlet to this passage.
- the end of the stem 34 remote from the piston I2 is connected to the diaphragm I8 by means of a tension spring 35.
- the two diaphragms I8, I9 (which are of different effective areas) are interconnected by an intermediate piece 24, and the diaphragm I9 is provided with a gapped yoke piece 21 which carries the normally-open valve I5. Also this diaphragm is connected to the body part by a tension spring 36.
- the valve I 6' co-operates with a vent 26' on a duct 25' which extends between the sides of the yoke piece 27, and this duct communicates with the ports 3
- passage 26 may be further controlled by a normally-open valve 3? which'can be actuated by any convenient means responsive to, for example, exhaust gas, or combustion chamber, temperature.
- the said means comprises a solenoid 38 operable by current derived from a thermo-couple in the hot region.
- Liquid under pressure related to the speed of the pump acts on the diaphragm I8 and is led to this diaphragm from the pump through the passage :c.
- the region above the diaphragm I9 communicates with a sump or the pump inlet through a passage 32. Air at atmospheric or other pressure is led to the region between the diaphragm through a passage 2
- the mode of action is as follows:
- valve I6 With the throttle in a steady working position, the valve I6 is open (as is also the valve 31 when this is provided), and the valve 30 is closed. To obtain an increased rate of fuel supply the driver opens the valve 30 to any desired extent. Liquid can then escape from the lower part of the cylinder I3 through the ports 3
- diaphragm used in the foregoing description is intended to include an equivalent "piston slidable in a cylindrical chamber.
- a liquid-operated servo-mechanism comprising in combination a chamber, a liquid inlet communicating with said chamber, a member arranged in said chamber and movable by liquid under pressure admitted to said chamber through said inlet, a manually operable valve movable relatively to and arranged to co-operate with said member for determining the extent of movement of said member, a second valve for controlling the rate of movement of said member, means for moving said second valve in one direction under the action of said member, and means responsive to fluid pressure for moving said second valve in the opposite direction.
- a liquid-operated servo-mechanism comprising in combination a cylinder, a liquid inlet communicating with one end of said cylinder, a piston arranged in said cylinder and movable by liquid under pressure admitted to said cylinder through said inlet, a spring acting on said piston in the direction for opposing movement thereof by liquid under pressure, a fluid outlet passage extending through said piston, a manually operable valve movable relatively to and arranged to co-operate with said piston for controlling liquid flow through said passage and thereby determining the extent of movement of said piston, a second valve for controlling the rate of movement of said piston, means for moving said second valve in one direction under the action of said piston, and means responsive to fluid pressure for moving said second valve in the opposite direction.
- a liquid-operated servo-mechanism comprising in combination a chamber, a liquid inlet communicating with said chamber, a member arranged in said chamber and movable by liquid under pressure admitted to said chamber through said inlet, a manually operable valve movable relatively to and arranged to co-operate with said member for determining the extent of movement of said member, a second valve for controlling the rate of movement of said member, a spring through the medium of which said second valve is movable in one direction by said member, and at least one diaphragm operatively connected to said second valve and responsive to fluid pressure for moving said second valve in the opposite direction.
- a liquid-operated servo-mechanism comprising in combination a cylinder, a liquid inlet communicating with one end of said cylinder, a piston arranged in said cylinder and movable by liquid under pressure admitted to said cylinder through said inlet, a spring acting on said piston in the direction for opposing movement thereof by liquid under pressure, a fluid outlet passage extending through said piston, a manually operable valve movable relatively to and arranged to co-operate with said piston for controlling liquid flow through said passage and thereby determining the extent of movement of said piston, a second valve for controlling liquid flow from said cylinder and thereby controlling the rate of movement of said piston, a spring through the medium-of which said second valve is movable in one direction by said piston, and at least one diaphragm operatively connected to said second valve and responsive to fluid pressure for moving said sec- 0nd valve in the opposite direction.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluid-Driven Valves (AREA)
Description
Dec. 16,1952 |F|ELD 2,621,632
LIQUID FUEL. CONTROL MECHANISM FOR INTERNAL-COMBUSTION PRIME MOVERS Filed Dec. 5, 1950 2 SHEETS-SHEET 1 h'vegvboz 12. JIfe e 566 CZQ Dec. 16, 1952 J, |F|E| D 2,621,632
LIQUID FUEL CONTROL MECHANISM FOR INTERNAL-COMBUSTION PRIME MOVERS Filed D80. 5, 1950 2 SHEETSSHEET 2 Patented Dec. 16, 1952 LIQUID FUEL CONTROL MECHANISM FOR INTEBNAL-CQIWBUSTION- PRIME ,MOVERS Richard Joseph "Ifield, Dura'l, New South Wales, Australia, assignor to Joseph Lucas Limited, Birmingham, England Application December .5, 1950, Serial No. 199,258 In Great Britain November '3, 1949 5' Claims. '1
' This invention relates to a liquid-fuel control mechanism for an internal combustion prime mover, and particularly a jet engine, gas turbine, or the like, the mechanism being of the kind which includes a throttle under the manual control of the driver. The object of the invention is to provide an improved mechanism adapted to prevent an excessively rapid rate of increase of supply of fuel to the prime mover in the event of an excessively rapid actuation of the manually operable throttle.
The invention comprises the combination with a throttle, of a liquid-operated servo-mechanism for v actuating the throttle, and valving means associated with the servo mechanisrn for controlling the movement of the throttle, the valving means comprising a manually operable valve for controlling the extent of movement, and a valve movable in part in response to movement of the servo mechanism and in part to fluid pres,- s'ure for controlling the rate of movement of the throttle. a
In the accompanying drawings:
Figure -1 is a sectional diagram illustrating a system which includes a fuel control means embodying the invention, and
Figure v2 is a sectional diagram'illustrating a modlfied'constructi'on of the said mechanism.
Referringto Figure 1, the fuel control mecha ni'sm shown at the left hand side of the diagram is arranged in association with a known formoi' variable delivery liquid fuel pump, and means for controlling the pump output. The pump ,com-- prises a rotary body a contained in a housing?) and provided with 'reciprocatory plungers c whicjh co-operate with an angularly adjustable swash plated. liquid fuel enters the pump along the passage {2 and is discharged along the passage 3. The swash plate is angularly ad'ju'stable by -:a servo-mechanism which comprises a piston fig slidable in a cylinder 71. and loaded by a spring 5. The two ends of the cylinder are in commnnication through .a restricted orifice a. Liquid fuel can. enter the cylinder from the passage :7, and can emerge through a passage k to a -vent m which is controlled-by a valve n. When the valven is closed, liquid acts. with equal pressures on the two sides of the piston g, and the spring 2' then moves the piston to the right for increasing thev obliquity of the swash plate, so enabling the causing it to move to the-left againsttheaction of the spring i for reducing the obliquityof the swash plate and thereby reducing the- 'pump output. I
The vent m and valve 11. are contained-in a chambered part 0 which is divided into two com-' partments by a flexible diaphragm p, and on the latter is mounted a lever q which carries the valve n. The lever 'q is loaded by a spring -r and is subject to the pressure of the liquid fuel in the-pas-' sage fwhich pressure acts on the lever through a plunger s. Also the lever is subject to atmospheric pressure admittedto the said body part at i, this pressure acting on the lever through an evacuated deformable capsule a. *By means of the valve 12 the pump output is under the automatic control of atmospheric pressure and thepressure in communication with a passage a leading from the said housing. One side of the chamber w is bounded by a flexible diaphragm y loaded by a tension spring z, and to the diaphragm is connected by a stem 3 a lever 4' carrying a valve ,5
which controls a vents in communication with a servo-cylinder it. When the liquid pressure'acting on the diaphragm yexceeds a predetermined" amount, the valve 5 is opened. Liquid can then:
escape from the cylinder '71. and the preponderating l-iquid pressure then acting on the right hand side of the piston g moves the latter to the-left for reducing the .pump output. The pump and control means above.
example of a system :to which the present invention can be applied, the invention bein concerned essentially with the additional control meansishownat the-left hand side of Figure 1 In carrying: the invention into efiect in the manner shown in Figure 1, there are provided in a hollow body part l: ,a liquid fuel inlet passage 8 and an ontletpassage 9 with an intermediate throat H), the liquid being supplied to :the
passage 3 by the pump and being zconductedlby' the. passage 9 to the prime mover. Extending through the throat L8 is arranged an axially slid'able throttle l I having at one end a conical or otherwise suitably shaped endior varying the eil'ective size of the throat. {0. The other end of I the throttle has formed on or secured to it 'a' piston 1-2 slida-ble in a cylindrical chamber 43 m described: are already known, and are described only as-an' the body part I, the side of the piston remote from the throttle being loaded by compression springs, I4, I5. The spring I 4 is supported at one end by a shoulder in the chamber I3. The other spring I5 serves to transmit motion from the piston I2 to a valve I6 to be hereinafter described.-
The cylindrical chamber I3 opens into a compartment I! which is bounded at one side by one of a pair of flexible and interconnected coaxial diaphragms I8, I9 of diiferent effective areas, these diaphragms being loaded by another spring 20. A passage 2| admits atmospheric or other related pressure from the part above described, to the region between the diaphragms, and a chamber 22 associated with the diaphragm I9 is adapted to receive liquid from the pipe 1: at a pressure related to the speed of the prime mover. The diaphragms I8, I9 are interconnected by an annulus 24.
In the compartment I1 is arranged a duct 25 terminating in a vent 26 with which co-operates the normally-closed valve I carried by the diaphragm I8. Motion is transmissible from the spring I5 to this diaphragm and valve by a thrust piece 2'! which is gapped so that it extends around the duct 25. The duct 25 communicates with a passage 28 in the part I leading to the end of the cylindrical chamber I3 below the piston, which end is also in communication with the liquid fuel inlet 8 through a restricted orifice 29. Further, an axial bore is formed in the throttle II and piston I2 and in this bore is contained a slidable valve 30 controlling ports 3| in the throttle whereby both ends of the piston chamber I3 can be put into communication through the said bore. The other end of the valve 30 extends through the throttle and the adjacent portion of the body part, and at its outer end is adapted for attachment to any convenient manually operable actuating means.
The action of the mechanism is as follows: Starting with the throttle I in any steady working position, the valve I6 is closed and the valve 30 is open. Liquid can then flow past the valve 30 and through the piston I2 to the passage 32 leading to a sump or to the inlet passage e of the pump. To obtain an increased rate of fuel supply the driver moves the valve 30 to any desired extent for closing the ports 3|. The fuel pressure acting on the piston I2 then increases and causes the extent of opening of the throttle ID to be increased. The increase of opening is, however, restricted (at least in part) by the consequent' opening of the valve I6 under the action of the spring I4, which acts in opposition to the pressures acting on the diaphragms I8, I9. But if the liquid pressure corresponding to increased engine speed should increase sufficiently to hold the valve I6 closed, the movement of the throttle is not arrested until the ports 3| are again opened'by continued movement of the throttle relatively to the valve 36. It will be seen that the rate of increase of the opening of the throttle is dependent only on the rate of movement of the piston I2, and is independent of the rate at which the driver moves the valve 30 from one position to another. The extent of movement is controlled by the valve 30.
The modification shown in Figure 2, is essentially similar in principle to the mechanism above described and differs mainly in certain details of arrangement. At one end of the body part 1 is provided a cylindrical chamber I3 which contains the piston I2 and compression spring I4. The throttle II extends from the piston through a throat I0 lying between the liquid fuel inlet passage 8' and outlet passage 9. The inlet 8 communicates with one end of the chamber I3, and liquid can pass to the other end of the chamber through a restricted orifice 29 in the piston. From the throttle extends a stem 34, and through the piston, throttle, and a part of the stem is formed an axial passage leading to ports 3|. The manually operable valve controls the inlet to this passage.
The end of the stem 34 remote from the piston I2 is connected to the diaphragm I8 by means of a tension spring 35. The two diaphragms I8, I9 (which are of different effective areas) are interconnected by an intermediate piece 24, and the diaphragm I9 is provided with a gapped yoke piece 21 which carries the normally-open valve I5. Also this diaphragm is connected to the body part by a tension spring 36. The valve I 6' co-operates with a vent 26' on a duct 25' which extends between the sides of the yoke piece 27, and this duct communicates with the ports 3| in the stem 34 by way of a passage 28' in the body part. If desired the passage 26 may be further controlled by a normally-open valve 3? which'can be actuated by any convenient means responsive to, for example, exhaust gas, or combustion chamber, temperature. In the example shown, the said means comprises a solenoid 38 operable by current derived from a thermo-couple in the hot region.
Liquid under pressure related to the speed of the pump acts on the diaphragm I8 and is led to this diaphragm from the pump through the passage :c. The region above the diaphragm I9 communicates with a sump or the pump inlet through a passage 32. Air at atmospheric or other pressure is led to the region between the diaphragm through a passage 2|.
The other parts of Figure 2 not particularly mentioned correspond substantially to those of Figure l and bear corresponding, but primed, reference numerals.
The mode of action is as follows:
With the throttle in a steady working position, the valve I6 is open (as is also the valve 31 when this is provided), and the valve 30 is closed. To obtain an increased rate of fuel supply the driver opens the valve 30 to any desired extent. Liquid can then escape from the lower part of the cylinder I3 through the ports 3| and past the valve I6, to the outlet 32, and the piston I2 will move against the spring I4 and under the pressure of the liquid at its upper side, for increasing the throttle opening. As a consequence of this movement, the spring will tend to close the valve I6, in opposition to the pressures acting on the diaphragms I8, I9, and so arrest continued movement of the piston. But if the liquid pressure related to the speed of the pump rises sufficiently rapidly to prevent closing of the valve I6, the piston will continue to move until the flow through the ports 3| is arrested by contact of the piston with the valve 30. As in the example above described the rate of movement of the throttle from one position to another is independent of the rate at which the driver moves the valve 30, the extent of movement being controlled by the valve 39.
The invention is not, however, restricted to the examples above described, as subordinate details of construction or arrangement may be varied to suit diiferent requirements. Further, it is to be understood that the term diaphragm used in the foregoing description is intended to include an equivalent "piston slidable in a cylindrical chamber.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
1. A liquid-operated servo-mechanism comprising in combination a chamber, a liquid inlet communicating with said chamber, a member arranged in said chamber and movable by liquid under pressure admitted to said chamber through said inlet, a manually operable valve movable relatively to and arranged to co-operate with said member for determining the extent of movement of said member, a second valve for controlling the rate of movement of said member, means for moving said second valve in one direction under the action of said member, and means responsive to fluid pressure for moving said second valve in the opposite direction.
2. A liquid-operated servo-mechanism comprising in combination a cylinder, a liquid inlet communicating with one end of said cylinder, a piston arranged in said cylinder and movable by liquid under pressure admitted to said cylinder through said inlet, a spring acting on said piston in the direction for opposing movement thereof by liquid under pressure, a fluid outlet passage extending through said piston, a manually operable valve movable relatively to and arranged to co-operate with said piston for controlling liquid flow through said passage and thereby determining the extent of movement of said piston, a second valve for controlling the rate of movement of said piston, means for moving said second valve in one direction under the action of said piston, and means responsive to fluid pressure for moving said second valve in the opposite direction.
3. A liquid-operated servo-mechanism comprising in combination a chamber, a liquid inlet communicating with said chamber, a member arranged in said chamber and movable by liquid under pressure admitted to said chamber through said inlet, a manually operable valve movable relatively to and arranged to co-operate with said member for determining the extent of movement of said member, a second valve for controlling the rate of movement of said member, a spring through the medium of which said second valve is movable in one direction by said member, and at least one diaphragm operatively connected to said second valve and responsive to fluid pressure for moving said second valve in the opposite direction.
4. A liquid-operated servo-mechanismcomprising in combination a cylinder, a liquid inlet communicating with one end of said cylinder, a piston arranged in said cylinder and movable by liquid under pressure admitted to said cylinder through said inlet, a spring acting on said piston in the direction for opposing movement thereof by liquid under pressure, a fluid outlet passage extending through said piston, a manually operable valve movable relatively to and arranged to co-operate with said piston for controlling liquid flow through said passage and thereby determining the extent of movement of said piston, a second valve for controlling liquid flow from said cylinder and thereby controlling the rate of movement of said piston, a spring through the medium-of which said second valve is movable in one direction by said piston, and at least one diaphragm operatively connected to said second valve and responsive to fluid pressure for moving said sec- 0nd valve in the opposite direction.
5. A liquid-operated servo-mechanism as claimed in claim 1, and having a temperatureresponsive valve arranged to control liquid flow from said chamber to said second valve.
RICHARD JOSEPH IFIELD.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,422,808 Stokes June 24, 1947 2,541,805 Berkey et a1 Feb. 13, 1951
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2621632X | 1949-11-03 |
Publications (1)
Publication Number | Publication Date |
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US2621632A true US2621632A (en) | 1952-12-16 |
Family
ID=10911947
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US199258A Expired - Lifetime US2621632A (en) | 1949-11-03 | 1950-12-05 | Liquid fuel control mechanism for internal-combustion prime movers |
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US (1) | US2621632A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2651517A (en) * | 1947-05-12 | 1953-09-08 | Rolls Royce | Hydraulic governor for gas turbine engine fuel systems |
US2691961A (en) * | 1951-04-25 | 1954-10-19 | Lucas Industries Ltd | Control means for liquid-operated servo mechanisms |
US2725040A (en) * | 1951-04-25 | 1955-11-29 | Lucas Industries Ltd | Control means for servo-mechanism of the kind having output means operable by liquid pressure and a control member therefor |
US2835228A (en) * | 1954-12-07 | 1958-05-20 | American Brake Shoe Co | Pressure compensator for variable volume pumps |
US2940429A (en) * | 1957-01-21 | 1960-06-14 | Plenty And Son Ltd | Control of variable-capacity pumps |
US2958310A (en) * | 1957-01-24 | 1960-11-01 | Plenty And Son Ltd | Pump control apparatus |
US3067693A (en) * | 1958-12-24 | 1962-12-11 | United Aircraft Corp | Control means for variable delivery pump |
US3399530A (en) * | 1967-03-17 | 1968-09-03 | Lucas Industries Ltd | Fuel flow control apparatus for gas turbine engines |
US3399529A (en) * | 1967-03-17 | 1968-09-03 | Lucas Industries Ltd | Fuel flow control apparatus for gas turbine engines |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422808A (en) * | 1943-06-22 | 1947-06-24 | Hobson Ltd H M | Regulating device for controlling the supply of fuel and other liquids to internal-combustion engines |
US2541805A (en) * | 1950-02-09 | 1951-02-13 | Gen Electric | Rate of change and maximum limit device for pressure fluid servomotor regulating systems |
-
1950
- 1950-12-05 US US199258A patent/US2621632A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422808A (en) * | 1943-06-22 | 1947-06-24 | Hobson Ltd H M | Regulating device for controlling the supply of fuel and other liquids to internal-combustion engines |
US2541805A (en) * | 1950-02-09 | 1951-02-13 | Gen Electric | Rate of change and maximum limit device for pressure fluid servomotor regulating systems |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2651517A (en) * | 1947-05-12 | 1953-09-08 | Rolls Royce | Hydraulic governor for gas turbine engine fuel systems |
US2691961A (en) * | 1951-04-25 | 1954-10-19 | Lucas Industries Ltd | Control means for liquid-operated servo mechanisms |
US2725040A (en) * | 1951-04-25 | 1955-11-29 | Lucas Industries Ltd | Control means for servo-mechanism of the kind having output means operable by liquid pressure and a control member therefor |
US2835228A (en) * | 1954-12-07 | 1958-05-20 | American Brake Shoe Co | Pressure compensator for variable volume pumps |
US2940429A (en) * | 1957-01-21 | 1960-06-14 | Plenty And Son Ltd | Control of variable-capacity pumps |
US2958310A (en) * | 1957-01-24 | 1960-11-01 | Plenty And Son Ltd | Pump control apparatus |
US3067693A (en) * | 1958-12-24 | 1962-12-11 | United Aircraft Corp | Control means for variable delivery pump |
US3399530A (en) * | 1967-03-17 | 1968-09-03 | Lucas Industries Ltd | Fuel flow control apparatus for gas turbine engines |
US3399529A (en) * | 1967-03-17 | 1968-09-03 | Lucas Industries Ltd | Fuel flow control apparatus for gas turbine engines |
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