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US2182933A - Regulation of internal combustion engines - Google Patents

Regulation of internal combustion engines Download PDF

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Publication number
US2182933A
US2182933A US106773A US10677336A US2182933A US 2182933 A US2182933 A US 2182933A US 106773 A US106773 A US 106773A US 10677336 A US10677336 A US 10677336A US 2182933 A US2182933 A US 2182933A
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pressure
piston
constant
ratio
space
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US106773A
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Schimanek Emil
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2700/00Mechanical control of speed or power of a single cylinder piston engine
    • F02D2700/02Controlling by changing the air or fuel supply
    • F02D2700/0217Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
    • F02D2700/0225Control of air or mixture supply
    • F02D2700/0228Engines without compressor
    • F02D2700/023Engines without compressor by means of one throttle device
    • F02D2700/0235Engines without compressor by means of one throttle device depending on the pressure of a gaseous or liquid medium
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7748Combustion engine induction type
    • Y10T137/7749Valve in auxiliary inlet to induction line
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7748Combustion engine induction type
    • Y10T137/7752With separate reactor surface
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7758Pilot or servo controlled
    • Y10T137/7759Responsive to change in rate of fluid flow
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7781With separate connected fluid reactor surface
    • Y10T137/7784Responsive to change in rate of fluid flow
    • Y10T137/7787Expansible chamber subject to differential pressures
    • Y10T137/7789With Venturi tube having a connection to throat

Definitions

  • This invention relates to a method of producing and maintaining a constant liquid or gas pressure in a space independently of the surrounding atmospheric pressure for purposes of regulation in connection with internal combustion engines.
  • 'I'he invention is based on the recognitionA of the fact that the pressure acting on one of the two smaller effective pressure surfaces of a dif-4 ferential piston or of a dilerential diaphragm or the like ycan be kept independent of the pressures acting on the two other pressure surfaces of the piston or the like, ⁇ if these latter pressures which may themselves be variable remain in a 15, constant ratio to one another and the pressure surfaces acted on by them are so dimensioned that they are to one another in the same, but inverse ratio.
  • F1, Fz'and F3 be for example the effective 20 pressure surfaces and In, p2 and p3 the pressures acting on them, the ratio 25 is to be constant but the ratio El vF2 is to be equal to- 30 g I P1 In this cas'e the products from pressure and surface for these two pressure surfaces F1. p1 or F2, p2 will be equal to one another and, if the pres- .5 sures act in opposition to one another, the two forces acting on the two pressure surfaces will balance one another.
  • the pressure p3 acting on the remaining third pressure ysurface F3 of the differential piston or the like can then be suit- 0 ably adjusted or kept constant by theforce of a spring or the like.
  • Fig. 1 shows one form. of the differential pres-v sure member by means of which a delivery of aliquid to an internal combustion engine is main- 5 tained at constant pressure.
  • Fig. 2 shows an arrangement in the induction pipe of the internal combustion Aengine which may be used in connection with a differential pressure member.
  • Fig. 3 is another form of the diierential pressure member using diaphragms in place of the differential piston construction of Fig. l..
  • Fig. 1 of the drawing I is a dierential piston which is capable of moving upwards and downwards a few millimetres in the cylinder 2.
  • a gas or liquid pressure Into the space 3 above the piston I and into the space 5 below the piston there is transmitted through the connections 4 and 6 respectively a gas or liquid pressure, the magnitudes of which pressures are in a constant ratio to one another, which is inversely equal to the ratio of the pressure surfaces I4 and I5.
  • the forces acting on the piston surfaces I4 and I5 will always balance one another, even when the pressures in the spaces 3 and. 5 change.
  • a spring 9 which may consequently be made relatively long or with a suitably large number of convolutions, so that its eiect may in view of the small motion of the piston be regarded as practically constant.
  • a gas or a liquid is enclosed, the pressure of which is dependent (without being dependent on the pressures acting on the two other piston surfaces) only on the pressure of the spring 9.
  • the piston I 40 When the gas or liquid pressure in the spacel I is smaller than the spring pressure, the piston I 40 will move downwards and gas or liquid will ow under pressure through the connectin I2 and the ring-shaped space II through the holes I0, until thepressure of the pressure medium contained in the space 'I has correspondingly risen, 45 so that it balances the pressure of the spring. Should the pressure in the space 'I become ltoo high, the piston I is moved upwards and the pressure medium will flow out of the space I through the connection into the open, until equilibrium is reestablished.
  • Fig. 2 shows how, for instance, the two gas or liquid pressures which are in themselves variable, but always maintain the same ratio to one another, for the two spaces 3 and 5 of the differential piston or the like may be produced.
  • the double Venturi tube shown in the drawing may for instance be interposed either in the induction pipe of the engine after the throttle valve, that is between the latter and the engine, :1r-:1: and y-y indicating the limits of the element, or it may be provided at the compressor of an engine, so that the outer tube I6.
  • the admission to an aero'- plane engine can be regulated, the constant pressure being brought into suitable relation to the gas pressure determining ⁇ the admission to the engine.
  • Fig. -3 an arrangement is shown, in which a differential 'diaphragm is used in place of a differential piston.
  • the spaces and connections aisaass of this arrangement bear reference numerals corresponding to those of Figure 1.
  • an induction pipe having means therein providing pressure differences of a constant ratio when a gaseous medium of varying density iiows through the induction pipe, a housing, movable means subject to the action of said pressure dilerences arranged within said housing and having two surfaces with the area of one surfacerdiiering with respect to the area of the other surface in a ratio corresponding to the ratio of the pressure differences so that the forces acting on said movable means balance each other, yieldable means urging said movable means in one direction, said housing having a chamber therein, means carried by the movable means adjacent the chamber and having a surface subjected to the pressure of the iiuid medium which is to be rendered constant so as to urge the movable means in a direction opposite to the force of said yieldable means, valve means carried by saidy movable means for admitting the fluid medium to said chamber when the pressure therein permits the movable means to be moved by the action of the
  • an induction pipe having means therein providing pressure differences of a constant ratio when a gaseous medium of varying density flows through the induction pipe, a housing, a piston subject to the action fof said pressure differences arranged within said housing and having two surfaces with the area of one surface differing with respect to the area of the other surface in a ratio corresponding to the ratio of the pressure differences so that the forces acting, on said piston balance each other, a spring urging said piston in one direction, said housing having a chamber therein, a shoulder carried by the piston adjacent the chamber and having a surface subjected to the pressure of the fluid medium which is to be rendered constant so as to urge the piston in a direction opposite to the force of said spring, valve'means carried by said piston for admitting the uid medium to said chamber when the pressure therein permits the piston to be moved by the action of the spring, and said chamber having an opening therein for permitting the uid medium to escape under constant pressure.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Description

Dec. 12, 1939. E. scHlMANEK REGULATION oF INTERNAL coMBsTIoN ENGINES Filed oct. 21, 1935VA .Jagd
511i/ Sci Patented Dec.` 12, 1939 PATENT OFFICE REGULATION oF INTERNAL coMBUsTIoN ENGINES Emil Schimanek, Budapest, Hungary Application October 21, 1936, Serial No. 106,773 In Austria October 26, 1935 2 Claims.
This invention relates to a method of producing and maintaining a constant liquid or gas pressure in a space independently of the surrounding atmospheric pressure for purposes of regulation in connection with internal combustion engines.
'I'he invention is based on the recognitionA of the fact that the pressure acting on one of the two smaller effective pressure surfaces of a dif-4 ferential piston or of a dilerential diaphragm or the like ycan be kept independent of the pressures acting on the two other pressure surfaces of the piston or the like,` if these latter pressures which may themselves be variable remain in a 15, constant ratio to one another and the pressure surfaces acted on by them are so dimensioned that they are to one another in the same, but inverse ratio.
If F1, Fz'and F3 be for example the effective 20 pressure surfaces and In, p2 and p3 the pressures acting on them, the ratio 25 is to be constant but the ratio El vF2 is to be equal to- 30 g I P1 In this cas'e the products from pressure and surface for these two pressure surfaces F1. p1 or F2, p2 will be equal to one another and, if the pres- .5 sures act in opposition to one another, the two forces acting on the two pressure surfaces will balance one another. The pressure p3 acting on the remaining third pressure ysurface F3 of the differential piston or the like can then be suit- 0 ably adjusted or kept constant by theforce of a spring or the like.
In a preferred form of the method according to the invention there are brought to bear on the pressure surfaces of the differential piston or v(Cl. 123-136) diagrammatically illustrated by constructional examples.
Fig. 1 shows one form. of the differential pres-v sure member by means of which a delivery of aliquid to an internal combustion engine is main- 5 tained at constant pressure.
Fig. 2 shows an arrangement in the induction pipe of the internal combustion Aengine which may be used in connection with a differential pressure member.
Fig. 3 is another form of the diierential pressure member using diaphragms in place of the differential piston construction of Fig. l..
In Fig. 1 of the drawing I is a dierential piston which is capable of moving upwards and downwards a few millimetres in the cylinder 2. Into the space 3 above the piston I and into the space 5 below the piston there is transmitted through the connections 4 and 6 respectively a gas or liquid pressure, the magnitudes of which pressures are in a constant ratio to one another, which is inversely equal to the ratio of the pressure surfaces I4 and I5. Thus the forces acting on the piston surfaces I4 and I5 will always balance one another, even when the pressures in the spaces 3 and. 5 change.
In the interior of the suitably hollow piston I is disposed a spring 9 which may consequently be made relatively long or with a suitably large number of convolutions, so that its eiect may in view of the small motion of the piston be regarded as practically constant. In the space 'I which is controlled by the third pressure surface of the differential piston a gas or a liquid is enclosed, the pressure of which is dependent (without being dependent on the pressures acting on the two other piston surfaces) only on the pressure of the spring 9.
When the gas or liquid pressure in the spacel I is smaller than the spring pressure, the piston I 40 will move downwards and gas or liquid will ow under pressure through the connectin I2 and the ring-shaped space II through the holes I0, until thepressure of the pressure medium contained in the space 'I has correspondingly risen, 45 so that it balances the pressure of the spring. Should the pressure in the space 'I become ltoo high, the piston I is moved upwards and the pressure medium will flow out of the space I through the connection into the open, until equilibrium is reestablished.
The arrangement of Fig. 2 shows how, for instance, the two gas or liquid pressures which are in themselves variable, but always maintain the same ratio to one another, for the two spaces 3 and 5 of the differential piston or the like may be produced. The double Venturi tube shown in the drawing may for instance be interposed either in the induction pipe of the engine after the throttle valve, that is between the latter and the engine, :1r-:1: and y-y indicating the limits of the element, or it may be provided at the compressor of an engine, so that the outer tube I6.
connects the compression space of the compressor with the suction space or with the atmosphere or with some other space in which a lower pressure prevails than in the compression space of the compressor. In b oth cases gas flows in the direction of the arrow II through the tube I6 forming one Venturi tube and through the second Venturi tube I9. Under the normal operative conditions of the engine, from idle running to full load, the critical velocity always occurs in the narrowest cross-section I8 of the latter Venturi tube, so that the pressure prevailing in the cross-section I8 will theoretically always amount to 0.53 times the pressure prevailing in the tube I6 for instance at the place -az-rc. Actually this` proportional number will assume a somewhat greater, but always constant value. This ratio is therefore independent of the specific gravity of the air and of the velocity of flow, consequently of the load on thel engine. of its speed of revolution and of all other factors (for instance the extent to which the throttle valve is opened and so on) Thus, when the pressure at the place :v -:v is conveyed through the connection 20 into the space below the dierential piston of Fig. l and the pressure at the place I8 through the connection 2| into the space 3 above the differential piston, then, if the ratio of the surfaces I5 and Il be so selected that it also amounts to a fraction of the pressure ratio, theoretically equal to 0.53, but actually in practice a constant slightly higher than this, 'equilibrium will prevail between the forces acting on the surfaces I4 and I5 and the pressure in the space I will only be dependent on the force of the spring 9. 'I'his constant pressure can be conveyed away through the connection 22 and be made use of for regulating purposes in all those cases in which the regulation is to be based on such a constant factor.
Thus, for instance, the admission to an aero'- plane engine can be regulated, the constant pressure being brought into suitable relation to the gas pressure determining `the admission to the engine.
In Fig. -3 an arrangement is shown, in which a differential 'diaphragm is used in place of a differential piston. The spaces and connections aisaass of this arrangement bear reference numerals corresponding to those of Figure 1.
What I claim is:
l. In apparatus for controlling the pressure of a fluid fuel medium supplied to an engine, an induction pipe having means therein providing pressure differences of a constant ratio when a gaseous medium of varying density iiows through the induction pipe, a housing, movable means subject to the action of said pressure dilerences arranged within said housing and having two surfaces with the area of one surfacerdiiering with respect to the area of the other surface in a ratio corresponding to the ratio of the pressure differences so that the forces acting on said movable means balance each other, yieldable means urging said movable means in one direction, said housing having a chamber therein, means carried by the movable means adjacent the chamber and having a surface subjected to the pressure of the iiuid medium which is to be rendered constant so as to urge the movable means in a direction opposite to the force of said yieldable means, valve means carried by saidy movable means for admitting the fluid medium to said chamber when the pressure therein permits the movable means to be moved by the action of the yieldable means, and said chamber having an opening therein for permitting the fluid medium to escape under constant pressure.
-2. In apparatus for controlling the pressure of a fluid fuel medium supplied to an engine, an induction pipe having means therein providing pressure differences of a constant ratio when a gaseous medium of varying density flows through the induction pipe, a housing, a piston subject to the action fof said pressure differences arranged within said housing and having two surfaces with the area of one surface differing with respect to the area of the other surface in a ratio corresponding to the ratio of the pressure differences so that the forces acting, on said piston balance each other, a spring urging said piston in one direction, said housing having a chamber therein, a shoulder carried by the piston adjacent the chamber and having a surface subjected to the pressure of the fluid medium which is to be rendered constant so as to urge the piston in a direction opposite to the force of said spring, valve'means carried by said piston for admitting the uid medium to said chamber when the pressure therein permits the piston to be moved by the action of the spring, and said chamber having an opening therein for permitting the uid medium to escape under constant pressure.
EMIL SCHIMANEK.
Cil
US106773A 1935-10-26 1936-10-21 Regulation of internal combustion engines Expired - Lifetime US2182933A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3169513A (en) * 1962-05-10 1965-02-16 Applic Ind Et Immobilieres Int Device for reguating the supply of fuel injected into an internal combustion engine
US3940928A (en) * 1974-02-11 1976-03-02 General Motors Corporation Air diverter valve
US4176641A (en) * 1976-12-30 1979-12-04 Cummins Engine Company, Inc. Aneroid for a turbocharged engine
US4237849A (en) * 1978-03-27 1980-12-09 Roberts Albert S Fuel pressure regulator
US4556490A (en) * 1983-03-19 1985-12-03 Robert Bosch Gmbh Arrangement for feeding of fuel

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3169513A (en) * 1962-05-10 1965-02-16 Applic Ind Et Immobilieres Int Device for reguating the supply of fuel injected into an internal combustion engine
US3940928A (en) * 1974-02-11 1976-03-02 General Motors Corporation Air diverter valve
US4176641A (en) * 1976-12-30 1979-12-04 Cummins Engine Company, Inc. Aneroid for a turbocharged engine
US4237849A (en) * 1978-03-27 1980-12-09 Roberts Albert S Fuel pressure regulator
US4556490A (en) * 1983-03-19 1985-12-03 Robert Bosch Gmbh Arrangement for feeding of fuel

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