US2245562A - Controlling device for internal combustion engines - Google Patents

Controlling device for internal combustion engines Download PDF

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US2245562A
US2245562A US156571A US15657137A US2245562A US 2245562 A US2245562 A US 2245562A US 156571 A US156571 A US 156571A US 15657137 A US15657137 A US 15657137A US 2245562 A US2245562 A US 2245562A
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chamber
controlling device
motor
controlling
casing
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US156571A
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Becker Ewald
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Askania Werke AG
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Askania Werke AG
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
    • F02D1/12—Transmission of control impulse to pump control, e.g. with power drive or power assistance non-mechanical, e.g. hydraulic
    • F02D1/14—Transmission of control impulse to pump control, e.g. with power drive or power assistance non-mechanical, e.g. hydraulic pneumatic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
    • F02D1/10—Transmission of control impulse to pump control, e.g. with power drive or power assistance mechanical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/13—Special devices for making an explosive mixture; Fuel pumps
    • F02M2700/1317—Fuel pumpo for internal combustion engines

Definitions

  • This invention relates to improvements in controlling devices, more particularly for fuel pumps of internal combustion engines.
  • the fuel supply depends on several factors of motor operation, on the air density within the induction pipe and on the exhaust counterpressure which naturally varies in dependence on the altitude at which the aircraft i's flying.
  • the object of the invention is to provide a simple and reliable controlling device by means of which the fuel quantity delivered by the pump is controlled automatically in dependence on the diiierent factors as functions of engine operation.
  • a further object of the invention is to facilitate the adjustment of the controlling device and to promote reliable operation.
  • Fig. 1 is a diagrammatic plan view of the controlling device
  • Fig. 2 is a sectional view of the device.
  • the controlling device comprises a casing I in which is arranged a fluid pressure relay 2, e. g. a sliding valve, as well as the servo-motor 3.
  • a chamber 5 for a capsule or bellows system 6 communicates with the induction pipe of the combustion engine (not shown) through an opening 7.
  • 'I'he capsule system 6 comprises a number of single capsules or diaphragms 6, 6', 6". Each contains a certain volume of gas of a predetermined density. If the density of air in the chamber 5, i. e. in the induction pipe of the motor decreases, then the capsules 6, B', 6", expand, thereby displacing the slide valve 2.
  • the stroke of the piston depends not only on the capsule stroke, but ⁇ also on the restoring iniiuence, i. e. on the form given to the cam-disc I6. Therefore, by the choice of the-curve it is possible to achieve a stroke of the piston I2 and the adjusting member 32 which corresponds to the fuel quantity needed by the motor for any existing air density.
  • the entire controlling device may be easily adapted to the special motor characteristic by changing the form of the cam I6. For this reason it may be advisable to arrange the cam I6 in a mannery so'that it may be exchanged. Furthermore, itis possible to arrange several cams side by side so that any cam may be set into operation by an axial displacement of the entire l cam body.
  • the form of the lcam is essential for an exact control of the fuel supply in accordance with the motor characteristic, it is desirable to have a long cam surface whichas experience has taughtmay be manufactured with greater exactness than a short one.v
  • the customary restoring cam directly fastened to the piston rod is replaced by a rotary cam disc having a long cam path which in spite of its length may be arranged within the smallest space.
  • the distance between the point of engagement of the cam It and the lever l and its pivot aids il is materially greater than the distance between the point of engagement of the capsule system 6 and lever 9 from its pivot axis Therefore, the' point of engagement of the cam iii and lever d has a greater stroke than the point oi engagement of the capsule system i3 and lever ii, thereby increasing the exactness of the controlling operation.
  • these additional controlling movements may be transmitted to the capsule system 6 in such a manner that this system is displaced as a Whole inc'iependentlyof the existing air density.
  • the capsule system 5 is not iixedly attached to seid casing l, but is supported by means of adjusting members adapted to be adjusted by the corresponding additional controlling factor and to displace the capsule system as a whole, thereby transmitting the additional controlling movement to the lever 9 and to the adjusting member 32 of the fuel pump in the manner above explained.
  • screw rings I3 and IS As adjusting members for the additional controlling movements, there are provided in the embodiment shown two screw rings I3 and IS, the outer ring i8 being screw threaded into the casing I, while the inner ring I8 is screw threaded into 'the outer ring.
  • a vsupporting member supporting the capsule system by means of a thread of a dierent or opposite pitch to the 'second screw thread.
  • Each of the screw rings may be independently rotated by means of arms itl' and i9', respectively.
  • the supporting member 2o may likewise be rotated by means of an arm 2li'. Any rotation of the ring i3 or i9 or of the supporting member 2Q results in a vertical displacement of the entire capsule system d.
  • the arms it', Iii and 2li are connected in any convenient manner with the corresponding control devices El, 25T, 231i, respectively which are responsive to various functions of engine operation.
  • the control device Zi e. g. may be responsive to the temperature of the erhaust gases (in the exhaust conduit of the motor)
  • the inner end of the supporting member 2li forms with the upper capsule 5 a chamber 24 which communicates with the atmosphere so that atmospheric pressure exists in this chamber and any change in said pressure influences the capsule system E.
  • controlling device permits controlling the fuel supply in accordance with a plurality of individual factors or functions of engine operation without the necessity of providing for each factor a special controlling device.
  • the capsule system li in said chamber is provided to control the servomotor in accordance with the air density in the induction pipe.
  • the air density is a function oi the temperature; therefore, it is important that the air in the chamber E sur rounding the capsule system 6 is caused to have the same temperature as the air in the induction pipe by permitting a small amount of air to enter the chamber 5 by any suitable means.
  • means are further provided to protect the air in the chamber 5 against any heating from'outside as e. g. from the heat radiated by the motor cylinders.
  • the casing wall of the chamber 5 is provided with a heat-insulating layer or lining 25, e. g. a rubber layer having, if desired a good reflecting coating of, i'or example, aluminum bronze.
  • a heat-insulating layer or lining 25 e. g. a rubber layer having, if desired a good reflecting coating of, i'or example, aluminum bronze.
  • another heatv1 insulating layer 26 is provided to prevent a transmission of heat from the wall of the c' ring i to the adjusting members I8, I 9, 2U of thu capsule system B.
  • the Wall 4 may be of heat insulating material such as, moulding material having a fabric insertion so as m act at the same time as a shock absorber or vibration dampen.
  • a turn buckle 21 is inserted in said controlling rod, said turn buckle having in a wellknown manner a left-hand screw and a righthand screw so that upon rotation of the buckle in one direction the connecting rod is shortened and upon rotation in opposite direction the connecting rod will be lengthened.
  • the buckle El may be rotated automatically during the controlling operation of the controlling device to vary the effective length of the connecting rod by any controlling device responsive to some additional function of engine operation which is to be taken into consideration,
  • the turn buckle 21 is provided with teeth 22 in the manner of a gear, said teeth extending axially over the entire length of the buckle.
  • (See Fig. 2.) 2! is a worm or spur gear rotatably mounted in the casing I and meshing with the teeth 28, so that, upon rotation of the Worm, the buckle 21 will also be rotated.
  • an arm 30 which may be connected in any suitable manner with an additional controlling device, schematically shown at 3l. If the piston rod I3 is displaced by the piston I2 in the manner described, the teeth 28 of the buckle 2l' slide in the worm 29 without any rotation of the buckle 21.
  • the buckle 21 may at any time be rotated by rotation of the worm 2S.
  • may be adjusted in accordance with the (B. t. u.) heat content o! the fuel per quantity unit, in accordance with the speed of the engine or of any other factor.
  • the controlling device fails to operate, it is desirable that the pilot may be able to manually actuate the adjusting member 552 of the fuel pump I1. As long as the member 32 is rigidly connected with the piston I2 of the servo-motor, the manual operation demands great exertion of strength. For this reason it is advisable to provide means by which the connec tion between the adjusting member 32 and the piston I2 may at any time be broken.
  • this means comprises a yieldable fork 33 frictionally ensuing a ball Il iixed to one end of the rod connected to the piston rod Il by' means of the above mentioned
  • the present invention is not restricted to the particular embodiment shown and described.
  • a hydraulic relay a pneumatic or electric relay may be used without departing from;
  • 1,'A controlling device for the fuel supplyf means of internal combustion engines.' comprising a casing divided into -two parts by a wally forming an insulated chamber in one part.
  • bellows system provided 'in the insulated part of the casing and forming a pressure responsive device, a pilot 'valve in the other part of the casing, a piston in the other part of the casing controlled by said pilot valve.
  • a rod connected to the piston and extending through the casing to the fuel supply means.
  • means extending from the insulated part of the casing for transferring themovementof the bellows system to the pilot valve, and a cam in the other part of the casing operatively connected to the transfer means to return the pilot valve by the transfer means to its initial position after a displacement of the piston due to a movement of the bellows system.
  • a controlling device in which' an independently adjustable device is provided in thol'rod. and means 'are provided to operate the adjustable device in dependence upon a function of the engine operation such as the temperature of the exhaust gases, the back pressure of the exhaust gases and the composition of the exhaust gases.
  • a controlling device in which means are provided in the form of a supporting member in the insulated chamber for mpending the bellows System in said insulating chamber. d in which means are provided in the casing to adjust the position of the support- 'ing memberrelative to the transfer means.
  • a controlling device for the fuel supply means of internal combustion engines comprising an element for adiusting.the fuel amount delivered to said engine, a servo-motor operatively connected to said element, a valve connected to control said servo-motor, and a pressure responsive system connected to act upon said valve, said system including a bellows responsive' to air intake pressure and temperature, and means forming a chamber connected to the atmosphere. said bellows being arranged so thatthe end thereof opposite to the valve connection constitutes a flexible end wall of said chamber. 5.
  • said chamber is provided with a rigid wail serving as a mounting for the bellows.
  • a device as claimed in claim 4 including a tube which is connected to the outer wall of said additional chamber and an external housing enclosing said bellows and said chamber, said tube being axially adjustable in said housing.
  • a device as claimed in-claim.4 including a screw-threaded tube connected to the outer wall of said chamber and an external housing enclosing said bellows and said chamber, said tube being screw threaded into said housing for adjustment thereof.
  • a device as claimed in claim 4 including a carrier for the pressure responsive system, an external housing forI enclosing said system and separately adjustable control members responsive to further functions of engine operation and disposed between the carrier and said external housing, said control members arranged to support the carrier.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)

Description

Ju'ne 17, 1941. f E. BECKER 2,245,562
CONTROLLING DEV-ICE FOR INTERNAL coMBUs'I'IoN ENGINES Filed .my so. 1957 Patented June 17, 1941 CONTROLLING DEVICE 'FOR INTERNAL CGIVEBUSTION ENGINES Ewald Becker, Berlin-Steglitz, Germany, assignor to Askania-Werke A. G. vormals Centralwerkstatt-Dessau und Carl Bamberg-Friedman, a
corporation of Germany Application July 30, 1937, Serial No. 156,571 In Germany August 1, 1936 9 Claims.
This invention relates to improvements in controlling devices, more particularly for fuel pumps of internal combustion engines.
Especially in aircraft engines the fuel supply depends on several factors of motor operation, on the air density within the induction pipe and on the exhaust counterpressure which naturally varies in dependence on the altitude at which the aircraft i's flying.
The object of the invention is to provide a simple and reliable controlling device by means of which the fuel quantity delivered by the pump is controlled automatically in dependence on the diiierent factors as functions of engine operation.
A further object of the invention is to facilitate the adjustment of the controlling device and to promote reliable operation.
The invention and its aims and objects will be readily understood from the following description of an embodiment in which reference is made to the drawing in which Fig. 1 is a diagrammatic plan view of the controlling device;
Fig. 2 is a sectional view of the device.
In the embodiment shown, the controlling device comprises a casing I in which is arranged a fluid pressure relay 2, e. g. a sliding valve, as well as the servo-motor 3. A chamber 5 for a capsule or bellows system 6 communicates with the induction pipe of the combustion engine (not shown) through an opening 7. 'I'he capsule system 6 comprises a number of single capsules or diaphragms 6, 6', 6". Each contains a certain volume of gas of a predetermined density. If the density of air in the chamber 5, i. e. in the induction pipe of the motor decreases, then the capsules 6, B', 6", expand, thereby displacing the slide valve 2. by means of a pin 8, extending through a wall 4 and a lever 9 linked at 9 to the valve 2. By a downward movement of the pin 8 the lever 9 is moved clockwise, resulting in a downward displacement of the valve 2. thereby allowing in a Well known manner the passage of a pressure iiuid, e. g. oil, to the left side of the servo-motor so that its piston I2 will be moved to the right. To the piston rod I3 is connected an adjusting member 32 in a manner hereinafter more fully explained, this adjusting member being adapted in a well known manner to vary the effective strokey of the fuel pump I'I, thereby varying the quantity of fuel fed to the motor.
When addusting the effective stroke of the fuel pump by means of the member 32, a restoring action is exerted at the same time on the valve 2. The piston rod I3 .is provided with a toothed rack I4 engaging a. pinion I5 fastened to a cam-disc I6, rotatably mounted in .the casing I. One end of the lever 9 rests on said disc as shown in Fig. 2 so that upon each rotation of the disc corresponding to the movement of the piston rod, this end of the lever 9 will be displaced upwardly or downwardly. In the case above mentioned in which the piston rod moves to the right, the disc will be rotated clockwise so that corresponding to the curve of the disc, the lever 9 will be swung counter-clockwise around a pivot-point represented by the pin 8. In this case the valve2 is Vpushed upwardly into its middle or neutral position by means of a spring II. Obviously. the valve will be restored by a downward movement in case of a left-hand movement of the servomotor piston I2.
From the foregoing explanation it follows that the stroke of the piston depends not only on the capsule stroke, but `also on the restoring iniiuence, i. e. on the form given to the cam-disc I6. Therefore, by the choice of the-curve it is possible to achieve a stroke of the piston I2 and the adjusting member 32 which corresponds to the fuel quantity needed by the motor for any existing air density.
The dependency of the quantity of fuel on the air density is differentfor each type of motor, each motor type having a certain characteristic with reference to the most favourable fuel consumption.
The entire controlling device may be easily adapted to the special motor characteristic by changing the form of the cam I6. For this reason it may be advisable to arrange the cam I6 in a mannery so'that it may be exchanged. Furthermore, itis possible to arrange several cams side by side so that any cam may be set into operation by an axial displacement of the entire l cam body.
In view of the fact that the form of the lcam is essential for an exact control of the fuel supply in accordance with the motor characteristic, it is desirable to have a long cam surface whichas experience has taughtmay be manufactured with greater exactness than a short one.v For this reason according to the invention the customary restoring cam directly fastened to the piston rod is replaced by a rotary cam disc having a long cam path which in spite of its length may be arranged within the smallest space.
With reference to the restoring operation as explalned above the advantage is to be noted that the distance between the point of engagement of the cam It and the lever l and its pivot aids il is materially greater than the distance between the point of engagement of the capsule system 6 and lever 9 from its pivot axis Therefore, the' point of engagement of the cam iii and lever d has a greater stroke than the point oi engagement of the capsule system i3 and lever ii, thereby increasing the exactness of the controlling operation.
f it is desired to control the fuel supply not only in accordance with the air density in the induction pipe, but also in accordance with the exhaust counter pressure, the temperature of the exhaust gases, the percentage of carbon-oxide of said gases any other factors or functions of engine operation, according to the invention, these additional controlling movements may be transmitted to the capsule system 6 in such a manner that this system is displaced as a Whole inc'iependentlyof the existing air density. For this purpose the capsule system 5 is not iixedly attached to seid casing l, but is supported by means of adjusting members adapted to be adjusted by the corresponding additional controlling factor and to displace the capsule system as a whole, thereby transmitting the additional controlling movement to the lever 9 and to the adjusting member 32 of the fuel pump in the manner above explained.
As adjusting members for the additional controlling movements, there are provided in the embodiment shown two screw rings I3 and IS, the outer ring i8 being screw threaded into the casing I, while the inner ring I8 is screw threaded into 'the outer ring. Into the inner ring I9 by means of a thread of a diiTer-ent or opposite pitch than the rlrst screw thread is screw threaded a vsupporting member supporting the capsule system by means of a thread of a dierent or opposite pitch to the 'second screw thread. Each of the screw rings may be independently rotated by means of arms itl' and i9', respectively. Furthermore, the supporting member 2o may likewise be rotated by means of an arm 2li'. Any rotation of the ring i3 or i9 or of the supporting member 2Q results in a vertical displacement of the entire capsule system d.
As indicated schematically in Fig. l, the arms it', Iii and 2li are connected in any convenient manner with the corresponding control devices El, 25T, 231i, respectively which are responsive to various functions of engine operation. The control device Zi, e. g. may be responsive to the temperature of the erhaust gases (in the exhaust conduit of the motor) The inner end of the supporting member 2li forms with the upper capsule 5 a chamber 24 which communicates with the atmosphere so that atmospheric pressure exists in this chamber and any change in said pressure influences the capsule system E. By reason of this additional chamber in front of the capsule system 6 being in communication with the atmosphere there is obtained a correction for the variation in exhaust back pressure with any change in altitude.
It is to be noted that the controlling device according to the invention permits controlling the fuel supply in accordance with a plurality of individual factors or functions of engine operation without the necessity of providing for each factor a special controlling device.
As explained above the chamber communi cates with the induction pipeV of the motor through an opening l. The capsule system li in said chamber is provided to control the servomotor in accordance with the air density in the induction pipe. As is well known, the air density is a function oi the temperature; therefore, it is important that the air in the chamber E sur rounding the capsule system 6 is caused to have the same temperature as the air in the induction pipe by permitting a small amount of air to enter the chamber 5 by any suitable means. For this purpose, means are further provided to protect the air in the chamber 5 against any heating from'outside as e. g. from the heat radiated by the motor cylinders.
In the embodiment shown the casing wall of the chamber 5 is provided with a heat-insulating layer or lining 25, e. g. a rubber layer having, if desired a good reflecting coating of, i'or example, aluminum bronze. Besides this another heatv1 insulating layer 26 is provided to prevent a transmission of heat from the wall of the c' ring i to the adjusting members I8, I 9, 2U of thu capsule system B. Likewise the Wall 4 may be of heat insulating material such as, moulding material having a fabric insertion so as m act at the same time as a shock absorber or vibration dampen.
In many cases it may be desired to vary the length of the connecting rod between the piston I2 of the servo-motor and the adjusting member 32 of the fuel pump I1. Therefore, according to the invention, a turn buckle 21 is inserted in said controlling rod, said turn buckle having in a wellknown manner a left-hand screw and a righthand screw so that upon rotation of the buckle in one direction the connecting rod is shortened and upon rotation in opposite direction the connecting rod will be lengthened. The buckle El may be rotated automatically during the controlling operation of the controlling device to vary the effective length of the connecting rod by any controlling device responsive to some additional function of engine operation which is to be taken into consideration,
In case of such an automatic control of the effective length of said controlling rod the turn buckle 21 is provided with teeth 22 in the manner of a gear, said teeth extending axially over the entire length of the buckle. (See Fig. 2.) 2! is a worm or spur gear rotatably mounted in the casing I and meshing with the teeth 28, so that, upon rotation of the Worm, the buckle 21 will also be rotated. To the axis of the worm 29 is fastened an arm 30 which may be connected in any suitable manner with an additional controlling device, schematically shown at 3l. If the piston rod I3 is displaced by the piston I2 in the manner described, the teeth 28 of the buckle 2l' slide in the worm 29 without any rotation of the buckle 21. On the other hand in spite of a longitudinal displacement, the buckle 21 may at any time be rotated by rotation of the worm 2S. The device 3| may be adjusted in accordance with the (B. t. u.) heat content o! the fuel per quantity unit, in accordance with the speed of the engine or of any other factor.
If for any reason the controlling device fails to operate, it is desirable that the pilot may be able to manually actuate the adjusting member 552 of the fuel pump I1. As long as the member 32 is rigidly connected with the piston I2 of the servo-motor, the manual operation demands great exertion of strength. For this reason it is advisable to provide means by which the connec tion between the adjusting member 32 and the piston I2 may at any time be broken.
In the embodiment shown this means comprises a yieldable fork 33 frictionally ensuing a ball Il iixed to one end of the rod connected to the piston rod Il by' means of the above mentioned The present invention is not restricted to the particular embodiment shown and described.
Instead of. a hydraulic relay a pneumatic or electric relay may be used without departing from;
the spirit of the invention as defined in the" aDDended; claims.
What I claim is:
1,'A controlling device for the fuel supplyf means of internal combustion engines.' comprising a casing divided into -two parts by a wally forming an insulated chamber in one part. a4
bellows system provided 'in the insulated part of the casing and forming a pressure responsive device, a pilot 'valve in the other part of the casing, a piston in the other part of the casing controlled by said pilot valve. a rod connected to the piston and extending through the casing to the fuel supply means. means extending from the insulated part of the casing for transferring themovementof the bellows system to the pilot valve, and a cam in the other part of the casing operatively connected to the transfer means to return the pilot valve by the transfer means to its initial position after a displacement of the piston due to a movement of the bellows system.
2. A controlling device according to claim l. in which' an independently adjustable device is provided in thol'rod. and means 'are provided to operate the adjustable device in dependence upon a function of the engine operation such as the temperature of the exhaust gases, the back pressure of the exhaust gases and the composition of the exhaust gases. x
3. A controlling device according to claim 1. in which means are provided in the form of a supporting member in the insulated chamber for mpending the bellows System in said insulating chamber. d in which means are provided in the casing to adjust the position of the support- 'ing memberrelative to the transfer means.
4. A controlling device for the fuel supply means of internal combustion engines, comprising an element for adiusting.the fuel amount delivered to said engine, a servo-motor operatively connected to said element, a valve connected to control said servo-motor, and a pressure responsive system connected to act upon said valve, said system including a bellows responsive' to air intake pressure and temperature, and means forming a chamber connected to the atmosphere. said bellows being arranged so thatthe end thereof opposite to the valve connection constitutes a flexible end wall of said chamber. 5. A device according to claim 4, in which said chamber is provided with a rigid wail serving as a mounting for the bellows.
6. A device as claimed in claim 4, in which means are provided for displacing said bellows and said chamber as a whole in response to any additional function of engine operation such as the temperature of the exhaust gases, the back pressure of the exhaust gases and the composition of the exhaust gases.
7. A device as claimed in claim 4, including a tube which is connected to the outer wall of said additional chamber and an external housing enclosing said bellows and said chamber, said tube being axially adjustable in said housing.
8. A device as claimed in-claim.4, including a screw-threaded tube connected to the outer wall of said chamber and an external housing enclosing said bellows and said chamber, said tube being screw threaded into said housing for adjustment thereof.
9. A device as claimed in claim 4, including a carrier for the pressure responsive system, an external housing forI enclosing said system and separately adjustable control members responsive to further functions of engine operation and disposed between the carrier and said external housing, said control members arranged to support the carrier.
EWALD BECKER.
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Cited By (51)

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US2435902A (en) * 1947-06-28 1948-02-10 Reggio Ferdinando Carlo Fuel metering device
US2466415A (en) * 1944-01-03 1949-04-05 Hobson Ltd H M Pressure sensitive capsule and mixture control device embodying the same
US2474279A (en) * 1942-05-05 1949-06-28 Gen Controls Co Follow-up servomotor
US2520115A (en) * 1946-03-30 1950-08-29 Jack & Heintz Prec Ind Inc Servomotor for aircraft controls
US2531243A (en) * 1946-09-19 1950-11-21 Texas Co Fuel-air ratio controller
US2536158A (en) * 1946-07-01 1951-01-02 Napier & Son Ltd Apparatus for metering the fuel supplied to a prime mover
US2588952A (en) * 1945-12-07 1952-03-11 Carter Carburetor Corp Fuel supply system
US2593802A (en) * 1947-04-18 1952-04-22 Const Lavalette Atel Fuel flow regulator for supercharged aircraft engines
US2596461A (en) * 1948-08-11 1952-05-13 Carter Carburetor Corp Speed presponsive valve for fuelfeeding systems
US2608051A (en) * 1947-08-25 1952-08-26 Nettel Frederick Control system for turbocharged compression-ignition internalcombustion engines
US2621475A (en) * 1946-06-13 1952-12-16 Phillips Petroleum Co Operation of multistage combustion gas turbines
US2621642A (en) * 1948-04-20 1952-12-16 Phillips Petroleum Co Fuel metering control
US2622393A (en) * 1945-07-19 1952-12-23 Gen Electric Fuel regulating apparatus for aircraft gas turbine power plants
US2643513A (en) * 1949-04-08 1953-06-30 Niles Bement Pond Co Internal-combustion engine fuel and speed control
US2649084A (en) * 1948-08-11 1953-08-18 Carter Carburetor Corp Fuel supply system
US2667743A (en) * 1946-04-23 1954-02-02 Niles Bement Pond Co Fuel control apparatus for internal-combustion engines
US2669094A (en) * 1947-02-01 1954-02-16 Niles Bement Pond Co Fuel control apparatus for jet engines
US2669093A (en) * 1947-01-10 1954-02-16 Niles Bement Pond Co Control apparatus for internal-combustion engines
US2675674A (en) * 1954-04-20 Lee he
US2694315A (en) * 1949-07-07 1954-11-16 Foxboro Co Pneumatic control device
US2697909A (en) * 1946-04-23 1954-12-28 Niles Bement Pond Co Fuel control for turbojet engines
US2698654A (en) * 1949-05-27 1955-01-04 Gen Motors Corp Jet engine controller
US2755622A (en) * 1948-01-15 1956-07-24 Chrysler Corp Apparatus for controlling combustion turbines
US2794430A (en) * 1952-02-26 1957-06-04 Curtiss Wright Corp Dual fuel engine control system
US2828728A (en) * 1954-02-17 1958-04-01 Bosch Arma Corp Fuel injection systems
US2841129A (en) * 1954-08-04 1958-07-01 Reggio Ferdinando Carlo Engine control system
US2841130A (en) * 1939-02-03 1958-07-01 Ferdinando C Reggio Variable maximum fuel limiting device
US2881705A (en) * 1954-08-04 1959-04-14 Kugelfischer G Schaefer & Co Fuel injection pump
US2891701A (en) * 1956-02-14 1959-06-23 Lucas Industries Ltd Regulating means for liquid fuel metering apparatus for internal combustion engines
US2897808A (en) * 1956-07-31 1959-08-04 Bendix Aviat Corp Fuel injection system
US2910969A (en) * 1957-11-06 1959-11-03 Reggio Ferdinando Carlo Regulating device
US2922369A (en) * 1956-02-06 1960-01-26 Bosch Arma Corp Fuel injection apparatus
US2935053A (en) * 1956-02-07 1960-05-03 Citroen Sa Andre Two stroke engines
US2963861A (en) * 1947-12-18 1960-12-13 Bendix Corp Electronic fuel control apparatus for an engine
US2965179A (en) * 1959-03-30 1960-12-20 Reggio Ferdinando Carlo Regulating device
US2965092A (en) * 1957-06-25 1960-12-20 Holley Carburetor Co Fuel metering and pumping system for fuel injection
US2971335A (en) * 1948-07-27 1961-02-14 Bendix Corp Speed and temperature responsive fuel control system for combustion engines
US2972988A (en) * 1960-02-19 1961-02-28 Panhandle Eastern Pipe Line Co Automatic control for engine mixtures and speed
US2989043A (en) * 1956-06-07 1961-06-20 Reggio Ferdinando Carlo Fuel control system
US2997037A (en) * 1958-08-07 1961-08-22 Ford Motor Co Fuel injection control system
US3033186A (en) * 1958-02-07 1962-05-08 Kugelfischer G Schaefer & Co Device for influencing the fuel delivery of an injection pump supplying the fuel for an internal combustion engine
US3036564A (en) * 1958-11-18 1962-05-29 R E T E M Rech S Et Etudes Ele Low-pressure fuel injection device
US3067581A (en) * 1943-11-04 1962-12-11 Reggio Ferdinando Carlo Fuel supply system
US3078833A (en) * 1960-02-22 1963-02-26 Whitehurst George Fuel injection control systems for internal combustion engines
US3108829A (en) * 1957-08-03 1963-10-29 Daimler Benz Ag Control arrangement, particularly for fuel injection pumps
US3120218A (en) * 1961-12-01 1964-02-04 Phillips Petroleum Co Knock suppressant
US3301245A (en) * 1964-06-25 1967-01-31 Charles R Woodburn Fuel control means
US3693501A (en) * 1969-08-28 1972-09-26 Worcester Valve Co Ltd The Servo-systems
US3906910A (en) * 1973-04-23 1975-09-23 Colt Ind Operating Corp Carburetor with feedback means and system
DE2816384A1 (en) * 1978-04-15 1979-10-25 Voegele Ag J METHOD AND DEVICE FOR THE CONTROLLED DELIVERY OF LUBRICANTS
US5190010A (en) * 1990-12-22 1993-03-02 Mercedes-Benz Ag Arrangement for regenerating a soot burn-off filter in the exhaust duct of an air-compressing fuel-injected internal-combustion engine

Cited By (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675674A (en) * 1954-04-20 Lee he
US2841130A (en) * 1939-02-03 1958-07-01 Ferdinando C Reggio Variable maximum fuel limiting device
US2474279A (en) * 1942-05-05 1949-06-28 Gen Controls Co Follow-up servomotor
US3067581A (en) * 1943-11-04 1962-12-11 Reggio Ferdinando Carlo Fuel supply system
US2466415A (en) * 1944-01-03 1949-04-05 Hobson Ltd H M Pressure sensitive capsule and mixture control device embodying the same
US2622393A (en) * 1945-07-19 1952-12-23 Gen Electric Fuel regulating apparatus for aircraft gas turbine power plants
US2588952A (en) * 1945-12-07 1952-03-11 Carter Carburetor Corp Fuel supply system
US2520115A (en) * 1946-03-30 1950-08-29 Jack & Heintz Prec Ind Inc Servomotor for aircraft controls
US2697909A (en) * 1946-04-23 1954-12-28 Niles Bement Pond Co Fuel control for turbojet engines
US2667743A (en) * 1946-04-23 1954-02-02 Niles Bement Pond Co Fuel control apparatus for internal-combustion engines
US2621475A (en) * 1946-06-13 1952-12-16 Phillips Petroleum Co Operation of multistage combustion gas turbines
US2536158A (en) * 1946-07-01 1951-01-02 Napier & Son Ltd Apparatus for metering the fuel supplied to a prime mover
US2531243A (en) * 1946-09-19 1950-11-21 Texas Co Fuel-air ratio controller
US2669093A (en) * 1947-01-10 1954-02-16 Niles Bement Pond Co Control apparatus for internal-combustion engines
US2669094A (en) * 1947-02-01 1954-02-16 Niles Bement Pond Co Fuel control apparatus for jet engines
US2593802A (en) * 1947-04-18 1952-04-22 Const Lavalette Atel Fuel flow regulator for supercharged aircraft engines
US2435902A (en) * 1947-06-28 1948-02-10 Reggio Ferdinando Carlo Fuel metering device
US2608051A (en) * 1947-08-25 1952-08-26 Nettel Frederick Control system for turbocharged compression-ignition internalcombustion engines
US2963861A (en) * 1947-12-18 1960-12-13 Bendix Corp Electronic fuel control apparatus for an engine
US2755622A (en) * 1948-01-15 1956-07-24 Chrysler Corp Apparatus for controlling combustion turbines
US2621642A (en) * 1948-04-20 1952-12-16 Phillips Petroleum Co Fuel metering control
US2971335A (en) * 1948-07-27 1961-02-14 Bendix Corp Speed and temperature responsive fuel control system for combustion engines
US2649084A (en) * 1948-08-11 1953-08-18 Carter Carburetor Corp Fuel supply system
US2596461A (en) * 1948-08-11 1952-05-13 Carter Carburetor Corp Speed presponsive valve for fuelfeeding systems
US2643513A (en) * 1949-04-08 1953-06-30 Niles Bement Pond Co Internal-combustion engine fuel and speed control
US2698654A (en) * 1949-05-27 1955-01-04 Gen Motors Corp Jet engine controller
US2694315A (en) * 1949-07-07 1954-11-16 Foxboro Co Pneumatic control device
US2794430A (en) * 1952-02-26 1957-06-04 Curtiss Wright Corp Dual fuel engine control system
US2828728A (en) * 1954-02-17 1958-04-01 Bosch Arma Corp Fuel injection systems
US2881705A (en) * 1954-08-04 1959-04-14 Kugelfischer G Schaefer & Co Fuel injection pump
US2841129A (en) * 1954-08-04 1958-07-01 Reggio Ferdinando Carlo Engine control system
US2922369A (en) * 1956-02-06 1960-01-26 Bosch Arma Corp Fuel injection apparatus
US2935053A (en) * 1956-02-07 1960-05-03 Citroen Sa Andre Two stroke engines
US2891701A (en) * 1956-02-14 1959-06-23 Lucas Industries Ltd Regulating means for liquid fuel metering apparatus for internal combustion engines
US2989043A (en) * 1956-06-07 1961-06-20 Reggio Ferdinando Carlo Fuel control system
US2897808A (en) * 1956-07-31 1959-08-04 Bendix Aviat Corp Fuel injection system
US2965092A (en) * 1957-06-25 1960-12-20 Holley Carburetor Co Fuel metering and pumping system for fuel injection
US3108829A (en) * 1957-08-03 1963-10-29 Daimler Benz Ag Control arrangement, particularly for fuel injection pumps
US2910969A (en) * 1957-11-06 1959-11-03 Reggio Ferdinando Carlo Regulating device
US3033186A (en) * 1958-02-07 1962-05-08 Kugelfischer G Schaefer & Co Device for influencing the fuel delivery of an injection pump supplying the fuel for an internal combustion engine
US2997037A (en) * 1958-08-07 1961-08-22 Ford Motor Co Fuel injection control system
US3036564A (en) * 1958-11-18 1962-05-29 R E T E M Rech S Et Etudes Ele Low-pressure fuel injection device
US2965179A (en) * 1959-03-30 1960-12-20 Reggio Ferdinando Carlo Regulating device
US2972988A (en) * 1960-02-19 1961-02-28 Panhandle Eastern Pipe Line Co Automatic control for engine mixtures and speed
US3078833A (en) * 1960-02-22 1963-02-26 Whitehurst George Fuel injection control systems for internal combustion engines
US3120218A (en) * 1961-12-01 1964-02-04 Phillips Petroleum Co Knock suppressant
US3301245A (en) * 1964-06-25 1967-01-31 Charles R Woodburn Fuel control means
US3693501A (en) * 1969-08-28 1972-09-26 Worcester Valve Co Ltd The Servo-systems
US3906910A (en) * 1973-04-23 1975-09-23 Colt Ind Operating Corp Carburetor with feedback means and system
DE2816384A1 (en) * 1978-04-15 1979-10-25 Voegele Ag J METHOD AND DEVICE FOR THE CONTROLLED DELIVERY OF LUBRICANTS
US5190010A (en) * 1990-12-22 1993-03-02 Mercedes-Benz Ag Arrangement for regenerating a soot burn-off filter in the exhaust duct of an air-compressing fuel-injected internal-combustion engine

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