GB454154A - Improvements in or relating to supercharged internal-combustion engines for aircraft - Google Patents

Improvements in or relating to supercharged internal-combustion engines for aircraft

Info

Publication number
GB454154A
GB454154A GB8587/35A GB858735A GB454154A GB 454154 A GB454154 A GB 454154A GB 8587/35 A GB8587/35 A GB 8587/35A GB 858735 A GB858735 A GB 858735A GB 454154 A GB454154 A GB 454154A
Authority
GB
United Kingdom
Prior art keywords
valve
subject
capsule
change
bristol
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
GB8587/35A
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.)
GEORGE OSWALD ANDERSON
Bristol Aeroplane Co Ltd
Original Assignee
GEORGE OSWALD ANDERSON
Bristol Aeroplane Co Ltd
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 GEORGE OSWALD ANDERSON, Bristol Aeroplane Co Ltd filed Critical GEORGE OSWALD ANDERSON
Priority to GB8587/35A priority Critical patent/GB454154A/en
Publication of GB454154A publication Critical patent/GB454154A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F28D19/047—Sealing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D23/00—Controlling engines characterised by their being supercharged
    • F02D23/005—Controlling engines characterised by their being supercharged with the supercharger being mechanically driven by the engine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • F02D29/04—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
    • F02D2700/02—Controlling by changing the air or fuel supply
    • F02D2700/0217—Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
    • F02D2700/0225—Control of air or mixture supply
    • F02D2700/0246—Control of air or mixture supply for engines with compressor
    • F02D2700/0256—Control of air or mixture supply for engines with compressor by changing the speed of the compressor
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Supercharger (AREA)

Abstract

454,154. Fluid-pressure servomotorcontrol systems. BRISTOL AEROPLANE CO., Ltd., FEDDEN, A. H. R., and ANDERSON, G. O., Filton House, Bristol. March 19, 1935, Nos. 8587/35 and 61/36. [Class 135] [See also Group XXVII] In a supercharged aircraft engine richness of the combustible mixture is controlled automatically in accordance with the operation of change-speed mechanism in the drive of the supercharging blower. The change-speed mechanism is connected by a link 53 to a toggle 50 in the connection between the pilots handcontrol 54 and an air-bleed valve 66, or a needle valve, in the fuel inlet to the carburettor nozzle 68. The operation is effected through a sleeve valve 44, which actuates a servomotor piston 45, a pivoted link 60 and a piston valve 43 constituting a follow-up device ; a capsule 41 subject to atmospheric pressure superposes an altitude control. Further control by a capsule subject to boost pressure in the induction pipe may also be interposed. The main throttle valve 31 is operated, subject to boost pressure control, as described in Specification 450,587.
GB8587/35A 1935-03-19 1935-03-19 Improvements in or relating to supercharged internal-combustion engines for aircraft Expired GB454154A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8587/35A GB454154A (en) 1935-03-19 1935-03-19 Improvements in or relating to supercharged internal-combustion engines for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8587/35A GB454154A (en) 1935-03-19 1935-03-19 Improvements in or relating to supercharged internal-combustion engines for aircraft

Publications (1)

Publication Number Publication Date
GB454154A true GB454154A (en) 1936-09-21

Family

ID=9855342

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8587/35A Expired GB454154A (en) 1935-03-19 1935-03-19 Improvements in or relating to supercharged internal-combustion engines for aircraft

Country Status (1)

Country Link
GB (1) GB454154A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2429423A (en) * 1941-10-17 1947-10-21 Bendix Aviat Corp Control for internal-combustion engines
US2516123A (en) * 1944-04-10 1950-07-25 Gen Motors Corp Airplane engine controller
DE754176C (en) * 1938-04-24 1953-07-20 Daimler Benz Ag Control method for aircraft engines with a supercharger

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE754176C (en) * 1938-04-24 1953-07-20 Daimler Benz Ag Control method for aircraft engines with a supercharger
US2429423A (en) * 1941-10-17 1947-10-21 Bendix Aviat Corp Control for internal-combustion engines
US2516123A (en) * 1944-04-10 1950-07-25 Gen Motors Corp Airplane engine controller

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