GB734307A - Improvements in or relating to pumps and control systems therefor - Google Patents

Improvements in or relating to pumps and control systems therefor

Info

Publication number
GB734307A
GB734307A GB2057/53A GB205753A GB734307A GB 734307 A GB734307 A GB 734307A GB 2057/53 A GB2057/53 A GB 2057/53A GB 205753 A GB205753 A GB 205753A GB 734307 A GB734307 A GB 734307A
Authority
GB
United Kingdom
Prior art keywords
pump
valve
valves
ports
pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB2057/53A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB734307A publication Critical patent/GB734307A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M41/00Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/08Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/12Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F04B1/14Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/13Special devices for making an explosive mixture; Fuel pumps
    • F02M2700/1317Fuel pumpo for internal combustion engines
    • F02M2700/1329Controlled rotary fuel pump with parallel pistons or with a single piston in the extension of the driving shaft

Landscapes

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

Abstract

734,307. Fluid-pressure servomotor-control systems. BENDIX AVIATION CORPORATION. Jan. 23, 1953 [March 22, 1952], No. 2057/53. Class 135. [Also in Groups XXVI and XXVIII] The delivery of a constant stroke fluid pump is controlled by variably regulating the fluid pressure differential established across the check valves 28 controlling the pump discharge ports 33 so as to vary the period of time the check valves are seated during the suction-stroke of the pump. Fig. 1 shows a swash-plate pump 10 for supplying liquid fuel to the burners of a gas turbine or jet propulsion engine past a throttle or control device 58. The pump 10 (see Group XXVIII) comprises a swash-plate 471 driven from the engine through a shaft 48 and adapted to reciprocate pump plungers 18 in pumping chambers 23 having inlet ports 24 and discharge ports 33. The fuel passing the valves 28 flows through ports 34<SP>1</SP>, 36 to a common chamber 37 connected to the pump delivery pipe 39. The valves 28 are loaded in the closing direction by springs 41 and the chambers 40 at the rear of the valves communicate with the pump delivery pressure by restricted orifices 42 in the valves themselves or by a bleed between the chamber 37 and an annular manifold 44 connected to the chambers 40 by ports 43. The manifold 44 is connected by conduit 45 to a regulating device comprising a valve 60 actuated by a spring-loaded diaphragm 61 subject to the pressure drop across the throttle 58. The valve 60 is adapted to connect the conduit 45 to the low-pressure side of the pump through a further conduit 71. The pressure drop across the valve 60 is regulated by a further valve 72 actuated by a spring-loaded diaphragm 73 and having ports 70 in a hollow sliding valve member. The passage 45 is connected to a chamber 74 on one side of the diaphragm 73 by a passage 75 with a calibrated restriction 75<SP>1</SP>. This arrangement limits the rate of response of the valve 72 and serves to prevent surges in the main delivery pipe 39.
GB2057/53A 1952-03-22 1953-01-23 Improvements in or relating to pumps and control systems therefor Expired GB734307A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US734307XA 1952-03-22 1952-03-22

Publications (1)

Publication Number Publication Date
GB734307A true GB734307A (en) 1955-07-27

Family

ID=22113629

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2057/53A Expired GB734307A (en) 1952-03-22 1953-01-23 Improvements in or relating to pumps and control systems therefor

Country Status (1)

Country Link
GB (1) GB734307A (en)

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