US2594689A - Fluid operated speed governor - Google Patents
Fluid operated speed governor Download PDFInfo
- Publication number
- US2594689A US2594689A US719268A US71926846A US2594689A US 2594689 A US2594689 A US 2594689A US 719268 A US719268 A US 719268A US 71926846 A US71926846 A US 71926846A US 2594689 A US2594689 A US 2594689A
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- Prior art keywords
- plunger
- spill
- bore
- valve
- diaphragm
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D13/00—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2496—Self-proportioning or correlating systems
- Y10T137/2559—Self-controlled branched flow systems
- Y10T137/2574—Bypass or relief controlled by main line fluid condition
- Y10T137/2579—Flow rate responsive
- Y10T137/2589—Pilot valve operated
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2496—Self-proportioning or correlating systems
- Y10T137/2559—Self-controlled branched flow systems
- Y10T137/2574—Bypass or relief controlled by main line fluid condition
- Y10T137/2579—Flow rate responsive
- Y10T137/2594—Choke
- Y10T137/2597—Variable choke resistance
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2496—Self-proportioning or correlating systems
- Y10T137/2559—Self-controlled branched flow systems
- Y10T137/2574—Bypass or relief controlled by main line fluid condition
- Y10T137/2605—Pressure responsive
- Y10T137/2617—Bypass or relief valve biased open
- Y10T137/262—Increasing pressure progressively closes then reopens by-pass or relief valve
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/7722—Line condition change responsive valves
- Y10T137/7758—Pilot or servo controlled
- Y10T137/7759—Responsive to change in rate of fluid flow
Definitions
- This invention relates to improvements in governors and is intended to be particularly although not exclusively applicable to governors for use in gas turbine engines, especially for aircraft.
- the kind of governor here envisaged is that known as an all-speed governor, i. e. one which automatically maintains the engine speed constant at any pre-selected value.
- the essential requirements of an all-speed governor are that at a given throttle setting it shall maintain the selected engine speed irrespective of Variations in any of the factors normally influencing engine speed, e. g. altitude and load.
- the governor is also required if possible to prevent positively any tendencies of the engine to exceed the predetermined maximum values of speed or, in the case of gas turbine aero-engines for jet propulsion, the speed corresponding to maximum permissible temperature of the gases in the jet pipe, and to allow rapid accelerations and decelerations.
- an all-speed engine governor comprises at least two fluid pressure sensitive valves, of which one is operable by the other, each being adapted to spill fuel from a fuel pressure delivery line in responseto the extent of variations of pressure of the operating fluid consequent on changes in engine speed.
- the fluid may be the fuel itself.
- the operating force for one or both valves may be the pressure drop across an orifice in the fuel delivery line, the area of said orifice being preferably adjustable.
- the delivery of a fuel pump is passed through a variable area orifice the pressure drop across which operates a spring-loaded diaphragm ofr a spill type pilot valve adapted to spill fuel from the delivery line back to the pump inlet.
- a spill type pilot valve adapted to spill fuel from the delivery line back to the pump inlet.
- rlhe latter can actuate a spill valve plunger co-operating with spill ports arranged so that an increase or decrease in engine speed (which correspond- 'ingly increases or decreases the pressure drop) causes more or less fuel respectively to be spilled from the supply line to counteract the engine Movement of this plunger also correspondingly opens or closes associated servo ports in the pilot valve body and so delivers servo liquid (which in this case is conveniently the fuel) to one side or the other of a plunger of a compensating valve moving to cause spill ports in the compensating valve to open or close respectively following the opening or closing of the pilot valve spill ports.
- Figure l is a diagrammatic representation of one form of embodiment showing the valves in longitudinal section
- Figure 2 is a view of a detail constituting a cross-section of the slot '15;
- Figure 3 is a similar representation of a second form of embodiment; and Figure 3A is a detail showing of elements in said Figure 3.
- Figure 4 is a similar representation of a third form of embodiment.
- a fuel pump delivers fuel to engine burners (not shown) through a delivery line 2 in which is a manually adjustable variable area orifice 3.
- a pilot valve 4 which spills fuel from the line 2 back through a spill return line 5 to the inlet of pump I.
- the pilot valve comprises a substantially cylindrical body 6 having an axial bore 'l in which slides a valve plunger 8, and a cap 9 is divided internally by a diaphragm I2 into two chambers Ill, II of which chamber II communicates with bore 'l and, through pipe 13, with one end of orifice 3 while chamber ID communicates through pipe 'lll with the opposite end of said tone so that chamber I0 is at higher pressure than charnber II.
- Diaphragm I2 is spring-loaded by spring I3 against movement in the direction from high pressure to low pressure and is linked to plunger 8 by rod I4 secured at opposite ends to the diaphragm and the plunger.
- the latter itself has an axial bore I5 for pressure balancing purposes and is spring-loaded by spring I6 in the saine sense as diaphragm I2.
- a lateral slot I1 in the body 6 is connected to the downstream side of orifice 3 by a spill pipe I8, and a lateral bore i9 in the opposite side of the body 6 and axially oiset from slot Il' is connected through a spill lead 2B to spill line 5.
- Plunger 8 has a recessed portion 2
- the lateral bores 22, 23 are also provided on opposite sides of the body 6 and axially offset from each other. These are intended to function as servo ports and the plunger 8 is provided with a recess 24 communicating with bore I5 and adapted to communicate with either bore 22 or 23 when the plunger is in the appropriate position.
- the pilot Valve 4 is connected through pipes 25 and 25a to a compensating valve 28 comprising a substantially cylindrical body 29 having an axial bore 38 in which slides a cylindrical plunger 3
- a spill lead 2l is taken to a lateral slot lil in the wall of body 23, and from a lateral bore 32a: opposite to and axially offset from slot i3 is taken a spill lead 33a to spill line 5.
- Plunger 3l has a recessed portion 34 which puts slot 'I into communication with bore 32a to a greater or lesser extent according to its position and also has a recess 35 which communicates through a bleed line 35a with recess 34.
- the eirect of the recesses 34, 35 is to form two lands 36, 3T on the plunger 3I which are of substantially equal dimensions.
- the slot I1 at least at its lower end 'i5 where it enters the bore l is T-shaped in horizontal section as shown in Fig. 2.
- the plunger 8 moves far enough to uncover the transverse limb a of the T there is a sudden increase in the available area of slot '.'5 and thus a sudden increase in the spill from pipe i8, which eiect tends to correct the engine speed promptly.
- the compensating valve 28 also has a light spring 44, tending to close it so as to ensure that plunger 3l shall always be returned to the correct position for starting.
- Plunger 3I is moved to the left and thus increases the extent of communication between spill lead 21 and recess 34, and between recess 24 and spill pipes 33a and 5, thereby increasing the amount of fuel spilt by valve 28 and thus causing an additional check in the engine speed.
- the diameter of the land 'l is slightly less than that of bore 3i), thus providing clearance 38 hetween the surface of land 3? and the walLoi bore 30 to permit the liquid in the bore to the left of land 31 to leak through the clearance to recess 35 and thence through recess 34 to spill pipe 5.
- a decrease in engine speed causes plunger 8 and if necessary also plunger 3i to move to the right thus decreasing the spill and increasing the fuel supply which increases the speed to the preselected value.
- the compensating valve 28 is diaphragm operated, and openings 45, 46 in the wall ii of pilot valve 4 serve as spill outlets. These openings are arranged diametrically opposite and are so shaped and disposed relative to recesses in plunger 8 that movement of the latter produces a differential pressure between iiuid in recesses 4'1 and 48 which actuates diaphragm 5I and thence plunger 3l.
- opening 45 is o quadrilateral section so as to have an effective area which varies with axial movement of plunger 8.
- the other opening is in the form of a slot.
- Plunger 8 has two recessed portions 4l, 43 of which recess 4l is adapted to communicate with openings 45, 46 and is always in communication with a lateral bore 49, While recess 43 is adapted to communicate with openings 45, 43 and is always in communication with a lateral bore 50. Opening 45 is connected through spill pipe 5a to source.
- Compensating valve 28 is provided with a diaphragm 5I connected by rod 11 to vplunger 3i; bore 49 is connected by pipe 33 to one side of the diaphragm while bore of valve 4 cornmunicates through pipe 53 and a restrictor 52 with the other side of diaphragm EI and also through pipe 54 with the left-hand end of bore rI
- the general construction of valve 28 and plunger 3l is the same as in Figure 1 except that in this case no clearance is provided between land 3l' and the wall of bore 30, the liquid in this bore located to the left of land 31 communicating through pipe 54 when plunger .3
- the restrictor 52 provides the required hydraulic damping means.
- the pressure in recess 48 is transmitted through pipe 53 and restrictor 52 to the right hand side of diaphragm 5
- all move to the left, and thus increases the spill from 21 through recess 24 to spill pipe 35.
- the invention may also be used with so called spill controlled burners i. e. wherein part o1 the fuel delivered to each burner is ejected through the burner nozzle for combustion while the remainder is returned through a spill pipe to source l, the nozzle delivery being controlled by a throttling device in the spill pipe.
- the throttling device comprises the pilot valve and compensating valve system of the invention.
- the pilot valve plunger 8 is provided with three recesses 58, 59, 68 so as to form four lands 6
- the valve body 6 is provided with two servo ports 65, 66 on one side and with two spill ports 61, 68 on the diametrically opposite side, and also with a slot 69, preferably T shaped as slot 15 of Figure 1.
- the spill port 61 when in communication through the recess 58 with the slot 69 is adapted to ensure that spill therefrom shall pass to the main spill return pipe to source l, while the spill port 68 is adapted for communication either with the recess 59 or the recess 6u according to the direction of displacement of the plunger 8 from its normal position, thereby ensuring the return of any required spill from either of said recesses back through the main spill return pipe to source
- the general arrangement is such that in the mean position of plunger 8; land 6
- the recess 59 then communicates with bore 65 and recess 60 with bore 66.
- One or more bleed lines are provided either in the valve body 6 or in plunger 8 and arranged so that movement of plunger 8 to the right causes recess 60 to be at higher pressure and recess 59 to be at lower pressure.
- a bleed line 18 is provided in the body 6 and is closed in the mean position by land 62.
- a second bleed line 19 is closed in the mean position by land 64.
- Valve 28 has a diaphragm 5
- the port 65 in pilot valve d communicates through restrictor 52 with the left hand side of diaphragm 5
- Port 66 communicates through pipe 86 with the left hand side of diaphragm 5
- the compensating valve body 29 has a spill bore 8
- the slot 69 in valve 4 and slot 80 of valve 28 are both connected to the spill pipe 1
- or compensating valve 28 is similar to that of Figure 1.
- the restrictor 52 acts in the same way as in Figure 3 as a hydraulic damping means to effect slow movement of plunger 3
- l slot 86 connected to the burner spill outlet is never completely closed of so as to provide for starting purposes.
- These means may conven- Iiently comprise light springs 82 and 84 of suitable strength to bring plunger. 3
- a fluid operated governor for a variable speed engine comprising a source of fluid and a pump connected to said source and to a fluid delivery line having a restricted orifice
- a governor in an engine, a governor according to claim l, wherein the fuel delivery line includes a variable area orifice, and the pilot valve comprises a body having an internal longitudinal bore, transverse passages communicating with said bore, a diaphragm connected across said orifice and adapted to move a plunger slidable in said longitudinal bore and adapted to control the effective area of said passages, at least one of said passages being connected to a spill return line, and at least two other of said passages communicating with said compensating valve.
- pilot valve and compensating valve each comprise a substantially cylindrical ,body having an axial bore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into two chambers each provided with an inlet, a recessed plunger slidable in said axial 7 bore and linked to said diaphragm, one of said lateral passages in the vpilot valve communicating through a restrictor with an inlet of one of said chambers of the compensating valve, a second lateral passage in the pilot valve communicating with the inlet of the other of said chambers in the compensating valve, and a third lateral passage in the pilot valve communicating with that end of the axial bore in the compensating valve remote from the diaphragm.
- pilot Valve comprises a substantially cylindrical body having an axial Ybore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into Atwo chambers each provided with an inlet, a recessed axially bored plunger slidable in saidv axial bore and linked to said diaphragm, at least two of said lateral passages communicating with the compensating valve, andat least oneof said passages being adapted to serve asa spill outlet.
- pilot valve comprises a substantially cylindrical body having kan axial bore ⁇ and a plurality valve, and at least one of said passages being adapted to serve as a spill outlet, at least one of said lateral passages being of T section, one limb of the T being axially disposed and the other limb radially disposed.
- pilot valve comprises a substantially cylindrical body having an axial bore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into two chambers each provided with an inlet, a recessed axially bored plunger idable in said axial bore and linked to said diaphragm, at least two of said lateral passages communicating with the compensating valve, and at least one of said passages being adapted to serve as a spill outlet, at least one of said lateral passages having a section such that the effective area of said passage varies with axial movement of the pilot valve plunger.
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- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Fluid-Driven Valves (AREA)
Description
April 29, 1952- J. G. SHARP ET AL 2,594,689
FLUID OPERATED SPEED GOVERNOR April 29, 1952 J. G. SHARP ET Al. 2,594,589
FLUID OPERATED SPEED GOVERNOR 5 Sheets-Sheet 2 Filed Dec. 30, 1946 a F/"g.3^.
Fig. 3
Inval fonsl By )am Man/ #M Afforneys April 29, 1952 J. G. SHARP ET AL 2,594,689
FLUID OPERATED SPEED GOVERNOR speed variations.
atented Apr. 29, 1952 ascisse FLUID OPERATED SPEED GOVERNOR Joseph Goulding Sharp, Chilwell, near Beesten;
and Robert Edward Ingham, Brandsby, England, assignors to Power Jets (Research and Development) Limited, London, England, a
British company Application December 30, 1946, Serial No. 719,268 In Great Britain January 7, 1946 (Cl. 15S-36) 6 Claims. 1
This invention relates to improvements in governors and is intended to be particularly although not exclusively applicable to governors for use in gas turbine engines, especially for aircraft. The kind of governor here envisaged is that known as an all-speed governor, i. e. one which automatically maintains the engine speed constant at any pre-selected value.
The essential requirements of an all-speed governor are that at a given throttle setting it shall maintain the selected engine speed irrespective of Variations in any of the factors normally influencing engine speed, e. g. altitude and load. The governor is also required if possible to prevent positively any tendencies of the engine to exceed the predetermined maximum values of speed or, in the case of gas turbine aero-engines for jet propulsion, the speed corresponding to maximum permissible temperature of the gases in the jet pipe, and to allow rapid accelerations and decelerations.
For fulfilling the above mentioned requirements an all-speed engine governor according to the invention comprises at least two fluid pressure sensitive valves, of which one is operable by the other, each being adapted to spill fuel from a fuel pressure delivery line in responseto the extent of variations of pressure of the operating fluid consequent on changes in engine speed. The fluid may be the fuel itself.
The operating force for one or both valves may be the pressure drop across an orifice in the fuel delivery line, the area of said orifice being preferably adjustable.
In one form of embodiment of the invention the delivery of a fuel pump is passed through a variable area orifice the pressure drop across which operates a spring-loaded diaphragm ofr a spill type pilot valve adapted to spill fuel from the delivery line back to the pump inlet. For any given orice area setting the pressure drop is dependent on the fuel flow which in turn is determined by engine speed, variations of which cause movement of the diaphragm. rlhe latter can actuate a spill valve plunger co-operating with spill ports arranged so that an increase or decrease in engine speed (which correspond- 'ingly increases or decreases the pressure drop) causes more or less fuel respectively to be spilled from the supply line to counteract the engine Movement of this plunger also correspondingly opens or closes associated servo ports in the pilot valve body and so delivers servo liquid (which in this case is conveniently the fuel) to one side or the other of a plunger of a compensating valve moving to cause spill ports in the compensating valve to open or close respectively following the opening or closing of the pilot valve spill ports.
With this arrangement a small increase in engine speed to a value above the pre-selected speed determined by the orifice setting causes the `pilot valve immediately to open and spill fuel (or more fuel) from the delivery line. If the increase is large, then due to the opening of the servo ports the compensating valve is also actuated (but relatively more slowly) and also spills fuel (or more fuel) from the delivery line. The compensating valve plunger continues to move until the engine speed returns to the pre-selected value whereupon its movement ceases. A decrease in engine speed below this value causes the valves to close and spill less fuel.
In the accompanying drawings which illustrate, by way of example, three forms of embodiment of the invention:
Figure l is a diagrammatic representation of one form of embodiment showing the valves in longitudinal section;
Figure 2 is a view of a detail constituting a cross-section of the slot '15;
Figure 3 is a similar representation of a second form of embodiment; and Figure 3A is a detail showing of elements in said Figure 3.
Figure 4 is a similar representation of a third form of embodiment.
In Figure l a fuel pump delivers fuel to engine burners (not shown) through a delivery line 2 in which is a manually adjustable variable area orifice 3. Across orice 3 is connected a pilot valve 4 which spills fuel from the line 2 back through a spill return line 5 to the inlet of pump I.
The pilot valve comprises a substantially cylindrical body 6 having an axial bore 'l in which slides a valve plunger 8, and a cap 9 is divided internally by a diaphragm I2 into two chambers Ill, II of which chamber II communicates with bore 'l and, through pipe 13, with one end of orifice 3 while chamber ID communicates through pipe 'lll with the opposite end of said orice so that chamber I0 is at higher pressure than charnber II.
Diaphragm I2 is spring-loaded by spring I3 against movement in the direction from high pressure to low pressure and is linked to plunger 8 by rod I4 secured at opposite ends to the diaphragm and the plunger. The latter itself has an axial bore I5 for pressure balancing purposes and is spring-loaded by spring I6 in the saine sense as diaphragm I2.
A lateral slot I1 in the body 6 is connected to the downstream side of orifice 3 by a spill pipe I8, and a lateral bore i9 in the opposite side of the body 6 and axially oiset from slot Il' is connected through a spill lead 2B to spill line 5. Plunger 8 has a recessed portion 2| which permits bore I3 to communicate with slot I7 to a greater or lesser extent depending on the position of the plunger.
The lateral bores 22, 23 are also provided on opposite sides of the body 6 and axially offset from each other. These are intended to function as servo ports and the plunger 8 is provided with a recess 24 communicating with bore I5 and adapted to communicate with either bore 22 or 23 when the plunger is in the appropriate position.
The pilot Valve 4 is connected through pipes 25 and 25a to a compensating valve 28 comprising a substantially cylindrical body 29 having an axial bore 38 in which slides a cylindrical plunger 3|, and unions 32, 33 at each end through which the bores 22, 23 respectively communicate with opposite ends of bore 38.
From the delivery line 2 and on the downstream side of orifice 3 a spill lead 2l is taken to a lateral slot lil in the wall of body 23, and from a lateral bore 32a: opposite to and axially offset from slot i3 is taken a spill lead 33a to spill line 5.
Plunger 3l has a recessed portion 34 which puts slot 'I into communication with bore 32a to a greater or lesser extent according to its position and also has a recess 35 which communicates through a bleed line 35a with recess 34. The eirect of the recesses 34, 35 is to form two lands 36, 3T on the plunger 3I which are of substantially equal dimensions.
The slot I1, at least at its lower end 'i5 where it enters the bore l is T-shaped in horizontal section as shown in Fig. 2. Thus, when, in rer sponse to a great increase in engine speed, the plunger 8 moves far enough to uncover the transverse limb a of the T there is a sudden increase in the available area of slot '.'5 and thus a sudden increase in the spill from pipe i8, which eiect tends to correct the engine speed promptly.
The compensating valve 28 also has a light spring 44, tending to close it so as to ensure that plunger 3l shall always be returned to the correct position for starting.
The operation of this arrangement is as follows:
At the normal pre-selected speed the pressure in chamber l0 tending to move diaphragm I2 to the left exactly balances the combined pressures of spring I3 and uid in chamber II tending to move diaphragm I2 to the right. If there is an increase in engine speed, the pressure drop across orifice 3 increases and the balance is disturbed, diaphragm I2 therefore moving to the left and moving with it rod I4 and plunger 8.
If this speed increase is small, the movement of plunger 8 will also be small and only just suicient to increase communication between slots I1 and I9 through recess 2l and thence increase the spill from pipe I8 through pipe 5 to the extent necessary in order to diminish the fuel supply and correct the speed increase.
If, however, this increase is large, movement of plunger 8 is then large enough to bring recess 24 into communication with slot 22 and thence through pipe 25 into communication with valve 28 which then comes into operation.
Plunger 3I is moved to the left and thus increases the extent of communication between spill lead 21 and recess 34, and between recess 24 and spill pipes 33a and 5, thereby increasing the amount of fuel spilt by valve 28 and thus causing an additional check in the engine speed. The diameter of the land 'l is slightly less than that of bore 3i), thus providing clearance 38 hetween the surface of land 3? and the walLoi bore 30 to permit the liquid in the bore to the left of land 31 to leak through the clearance to recess 35 and thence through recess 34 to spill pipe 5. This permits leftward movement of plunger' 3i and also provides a hydraulic damping eiiect for said plunger which consequently moves much more slowly than plunger 8 ci pilot valve. After plunger 3i has traveled leitwards to increase the spill of valve 28 sufficiently for the necessary speed correction, the value of this speed returns to the pre-selected value thus enabling plunger 8 of valve 4 to return to its original position and plunger 3i ceases to move.
A decrease in engine speed causes plunger 8 and if necessary also plunger 3i to move to the right thus decreasing the spill and increasing the fuel supply which increases the speed to the preselected value.
It will thus he,l seen that the arrangement is such that small variations in the fuel supply are quickly corrected solely or mainly by the 'pilot valve 4 while larger variations are corrected mainly by the compensating valve 23.
In Figure 3 the compensating valve 28 is diaphragm operated, and openings 45, 46 in the wall ii of pilot valve 4 serve as spill outlets. These openings are arranged diametrically opposite and are so shaped and disposed relative to recesses in plunger 8 that movement of the latter produces a differential pressure between iiuid in recesses 4'1 and 48 which actuates diaphragm 5I and thence plunger 3l. In the form shown in Fig. 3A opening 45 is o quadrilateral section so as to have an effective area which varies with axial movement of plunger 8. The other opening is in the form of a slot. Plunger 8 has two recessed portions 4l, 43 of which recess 4l is adapted to communicate with openings 45, 46 and is always in communication with a lateral bore 49, While recess 43 is adapted to communicate with openings 45, 43 and is always in communication with a lateral bore 50. Opening 45 is connected through spill pipe 5a to source.
Compensating valve 28 is provided with a diaphragm 5I connected by rod 11 to vplunger 3i; bore 49 is connected by pipe 33 to one side of the diaphragm while bore of valve 4 cornmunicates through pipe 53 and a restrictor 52 with the other side of diaphragm EI and also through pipe 54 with the left-hand end of bore rIhe general construction of valve 28 and plunger 3l is the same as in Figure 1 except that in this case no clearance is provided between land 3l' and the wall of bore 30, the liquid in this bore located to the left of land 31 communicating through pipe 54 when plunger .3| moves to the left. The restrictor 52 provides the required hydraulic damping means.
In the normal position as shown in Figure 3A the central land of plunger 6 lies across the central portions of the openings 45 and 4S. In operation if the engine speed increases and plunger 8 of valve 4 is consequently moved to vthe left, owing to the quadrilateral shape of opening 45 the portion of the opening 45 located to the Vright of the central land of plunger 8 is increasing in eiective area at a rapid rate while on the other hand the portion or the opening 45 011 the leitthe spill from opening 45 to recess 48 is being increased rapidly while the spill from opening 45 to recess 41 is decreasing less rapidly, and therefore the net spill through pipe a is increased. At the same time the pressure in recess 48 will increase relatively to the pressure in recess 41. The pressure in recess 48 is transmitted through pipe 53 and restrictor 52 to the right hand side of diaphragm 5| of valve 28, while the pressure in recess 41 is transmitted through pipe 83 to the left hand side of the diaphragm 5|. Thus the diaphragm 5| together with rod 11 and plunger 3| all move to the left, and thus increases the spill from 21 through recess 24 to spill pipe 35.
If engine speed decreases then the operation of the apparatus is the reverse of that described above and both plungers 8 and 3| move to the right to decrease the amount of fuel spilt.
The invention may also be used with so called spill controlled burners i. e. wherein part o1 the fuel delivered to each burner is ejected through the burner nozzle for combustion while the remainder is returned through a spill pipe to source l, the nozzle delivery being controlled by a throttling device in the spill pipe. In this case the throttling device comprises the pilot valve and compensating valve system of the invention.
In Figure 4 which illustrates such a system, the pilot valve plunger 8 is provided with three recesses 58, 59, 68 so as to form four lands 6|, 62, 63, 64. The valve body 6 is provided with two servo ports 65, 66 on one side and with two spill ports 61, 68 on the diametrically opposite side, and also with a slot 69, preferably T shaped as slot 15 of Figure 1. The spill port 61 when in communication through the recess 58 with the slot 69 is adapted to ensure that spill therefrom shall pass to the main spill return pipe to source l, while the spill port 68 is adapted for communication either with the recess 59 or the recess 6u according to the direction of displacement of the plunger 8 from its normal position, thereby ensuring the return of any required spill from either of said recesses back through the main spill return pipe to source The general arrangement is such that in the mean position of plunger 8; land 6| partly covers slot 69, and recess 58 communicates with bore 61. The recess 59 then communicates with bore 65 and recess 60 with bore 66.
One or more bleed lines are provided either in the valve body 6 or in plunger 8 and arranged so that movement of plunger 8 to the right causes recess 60 to be at higher pressure and recess 59 to be at lower pressure. In the present case a bleed line 18 is provided in the body 6 and is closed in the mean position by land 62. A second bleed line 19 is closed in the mean position by land 64.
The compensating valve body 29 has a spill bore 8| and a lateral spill slot 80 axially offset therefrom. The slot 69 in valve 4 and slot 80 of valve 28 are both connected to the spill pipe 1| of a spill-controlled burner 12. 'Ihe spill bore 8| and ports 61, 68 are all connected to the main spill return piping 5.
The plunger 3| or compensating valve 28 is similar to that of Figure 1.
In operation if the engine speed increases, the pressure drop across the orifice 3 increases and at the same time the actual pressure on both sides of the orifice is also increased. Plunger 8 of valve 4 is moved to the left and thus increases the amount of fuel spilt from pipe 1| through pipe 81 to vrecess 62 and thence through spill pipe 5 back to source.
At the same time the space 88 in the bore 38 located to the left of plunger 8 communicates through bleed line 18 with port 59 and thence through restricted bore 52 with diaphragm 5| to valve 58 so that any increase in ypressure in chamber of valve 4 is transmitted through the axial bore |5 to the right hand side of'diaphragm 5|. The'fpressure on the left hand side of diaphragm 5| remains unchanged so that plunger 3| move-s to the left thus increasing the spill from pipe 1| through recess 34 to slot 8| and spill return pipe 5.
For a decrease in engine speed the bleedline 19 comes into operation to effect the movement of plunger 3| to the right so as to decrease the amount of fuel spilt back to source. The restrictor 52 acts in the same way as in Figure 3 as a hydraulic damping means to effect slow movement of plunger 3|.
It may be necessary to provide means whereby l slot 86 connected to the burner spill outlet is never completely closed of so as to provide for starting purposes. These means may conven- Iiently comprise light springs 82 and 84 of suitable strength to bring plunger. 3| to the correct position for starting.
We claim:
l. In a fluid operated governor for a variable speed engine ,comprising a source of fluid and a pump connected to said source and to a fluid delivery line having a restricted orifice, the provision of at least two fluid pressure sensitive valves each having spill means affording permanently open connection to said fluid delivery line downstream of said orifice and said source, one of said valves, the pilot valve, comprising an element connected directly across the orifice whereby one side of said element is freely open to the pressure existing immediately upstream of said orifice while the opposite side of said element is freely open to the pressure existing immediately downstream of said orifice, and the other valve, the compensating valve, is hydraulically connected to and is thereby operated by the pilot valve.
2-. In an engine, a governor according to claim l, wherein the fuel delivery line includes a variable area orifice, and the pilot valve comprises a body having an internal longitudinal bore, transverse passages communicating with said bore, a diaphragm connected across said orifice and adapted to move a plunger slidable in said longitudinal bore and adapted to control the effective area of said passages, at least one of said passages being connected to a spill return line, and at least two other of said passages communicating with said compensating valve.
3. A governor according to claim l, wherein the pilot valve and compensating valve each comprise a substantially cylindrical ,body having an axial bore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into two chambers each provided with an inlet, a recessed plunger slidable in said axial 7 bore and linked to said diaphragm, one of said lateral passages in the vpilot valve communicating through a restrictor with an inlet of one of said chambers of the compensating valve, a second lateral passage in the pilot valve communicating with the inlet of the other of said chambers in the compensating valve, and a third lateral passage in the pilot valve communicating with that end of the axial bore in the compensating valve remote from the diaphragm.
4. A governor according to claim 1, wherein the pilot Valve comprises a substantially cylindrical body having an axial Ybore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into Atwo chambers each provided with an inlet, a recessed axially bored plunger slidable in saidv axial bore and linked to said diaphragm, at least two of said lateral passages communicating with the compensating valve, andat least oneof said passages being adapted to serve asa spill outlet.
5. A governor according to claim l, wherein the pilot valve comprises a substantially cylindrical body having kan axial bore `and a plurality valve, and at least one of said passages being adapted to serve as a spill outlet, at least one of said lateral passages being of T section, one limb of the T being axially disposed and the other limb radially disposed.
6. A governor according to claim 1, wherein the pilot valve comprises a substantially cylindrical body having an axial bore and a plurality of lateral passages leading into said axial bore, an end cap rigid with said body and divided internally by a diaphragm into two chambers each provided with an inlet, a recessed axially bored plunger idable in said axial bore and linked to said diaphragm, at least two of said lateral passages communicating with the compensating valve, and at least one of said passages being adapted to serve as a spill outlet, at least one of said lateral passages having a section such that the effective area of said passage varies with axial movement of the pilot valve plunger.
JOSEPH GOULDING SHARP. ROBERT EDWARD INGHAM.
REFERENCES CITED The following references are of record in the le of this patent:
UNITED STATES PATENTS Number Name Date 2,405,888 Holley Aug. 13, 1946 2,446,523 Bradbury et al. Aug. 10, 1943
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2594689X | 1946-01-07 |
Publications (1)
Publication Number | Publication Date |
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US2594689A true US2594689A (en) | 1952-04-29 |
Family
ID=10911093
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US719268A Expired - Lifetime US2594689A (en) | 1946-01-07 | 1946-12-30 | Fluid operated speed governor |
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US (1) | US2594689A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2694290A (en) * | 1951-07-25 | 1954-11-16 | United Aircraft Corp | Regulator for limiting compressor pressure rise |
US2747369A (en) * | 1952-02-13 | 1956-05-29 | Lucas Industries Ltd | Engine temperature responsive means to control fuel supply bypass and spill lines |
US2769488A (en) * | 1951-07-31 | 1956-11-06 | Lucas Industries Ltd | Liquid fuel control means |
US2802335A (en) * | 1954-12-14 | 1957-08-13 | Napier & Son Ltd | Fuel supply and associated apparatus for combustion engines |
US2824423A (en) * | 1954-10-13 | 1958-02-25 | Rolls Royce | Hydraulic speed responsive circuits |
US2849987A (en) * | 1953-04-13 | 1958-09-02 | Shafer Valve Co | Hydraulic valve operator control system |
US2874764A (en) * | 1953-03-11 | 1959-02-24 | Plessey Co Ltd | Speed control for combustion engines and turbines |
US3005463A (en) * | 1957-07-24 | 1961-10-24 | Vickers Inc | Power transmission |
US3043104A (en) * | 1959-07-24 | 1962-07-10 | Jr Alexander B Magnus | Fluid pressurizing systems with low temperature rise characteristics |
US3164202A (en) * | 1960-12-14 | 1965-01-05 | Rolls Royce | Gas turbine engine fuel system |
US3177921A (en) * | 1960-10-25 | 1965-04-13 | Plessey Co Ltd | Fuel delivery control systems, more particularly for turbojet engines |
US3427980A (en) * | 1965-03-22 | 1969-02-18 | Rolls Royce | Gear pump |
US3608575A (en) * | 1968-03-20 | 1971-09-28 | Daimler Benz Ag | Differential-pressure regulating valve assembly especially for control installations of gas turbine drive units |
US3933277A (en) * | 1973-08-13 | 1976-01-20 | Berthoud, S.A. | Method and device for controlling fluid pressure |
FR2334277A5 (en) * | 1973-08-13 | 1977-07-01 | Berthoud Sa | Agricultural sprayer discharge regulator - has double diaphragm device and pressure dependent restrictor giving speed responsive discharge |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405888A (en) * | 1945-01-01 | 1946-08-13 | George M Holley | Fuel control valve |
US2446523A (en) * | 1944-01-31 | 1948-08-10 | Westinghouse Electric Corp | Fuel control apparatus for liquid fuel burners |
-
1946
- 1946-12-30 US US719268A patent/US2594689A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2446523A (en) * | 1944-01-31 | 1948-08-10 | Westinghouse Electric Corp | Fuel control apparatus for liquid fuel burners |
US2405888A (en) * | 1945-01-01 | 1946-08-13 | George M Holley | Fuel control valve |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2694290A (en) * | 1951-07-25 | 1954-11-16 | United Aircraft Corp | Regulator for limiting compressor pressure rise |
US2769488A (en) * | 1951-07-31 | 1956-11-06 | Lucas Industries Ltd | Liquid fuel control means |
US2747369A (en) * | 1952-02-13 | 1956-05-29 | Lucas Industries Ltd | Engine temperature responsive means to control fuel supply bypass and spill lines |
US2874764A (en) * | 1953-03-11 | 1959-02-24 | Plessey Co Ltd | Speed control for combustion engines and turbines |
US2849987A (en) * | 1953-04-13 | 1958-09-02 | Shafer Valve Co | Hydraulic valve operator control system |
US2824423A (en) * | 1954-10-13 | 1958-02-25 | Rolls Royce | Hydraulic speed responsive circuits |
US2802335A (en) * | 1954-12-14 | 1957-08-13 | Napier & Son Ltd | Fuel supply and associated apparatus for combustion engines |
US3005463A (en) * | 1957-07-24 | 1961-10-24 | Vickers Inc | Power transmission |
US3043104A (en) * | 1959-07-24 | 1962-07-10 | Jr Alexander B Magnus | Fluid pressurizing systems with low temperature rise characteristics |
US3177921A (en) * | 1960-10-25 | 1965-04-13 | Plessey Co Ltd | Fuel delivery control systems, more particularly for turbojet engines |
US3164202A (en) * | 1960-12-14 | 1965-01-05 | Rolls Royce | Gas turbine engine fuel system |
US3427980A (en) * | 1965-03-22 | 1969-02-18 | Rolls Royce | Gear pump |
US3608575A (en) * | 1968-03-20 | 1971-09-28 | Daimler Benz Ag | Differential-pressure regulating valve assembly especially for control installations of gas turbine drive units |
US3933277A (en) * | 1973-08-13 | 1976-01-20 | Berthoud, S.A. | Method and device for controlling fluid pressure |
FR2334277A5 (en) * | 1973-08-13 | 1977-07-01 | Berthoud Sa | Agricultural sprayer discharge regulator - has double diaphragm device and pressure dependent restrictor giving speed responsive discharge |
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