GB346503A - Improvements in means for regulating internal combustion engines for aircraft - Google Patents

Improvements in means for regulating internal combustion engines for aircraft

Info

Publication number
GB346503A
GB346503A GB387830A GB387830A GB346503A GB 346503 A GB346503 A GB 346503A GB 387830 A GB387830 A GB 387830A GB 387830 A GB387830 A GB 387830A GB 346503 A GB346503 A GB 346503A
Authority
GB
United Kingdom
Prior art keywords
aneroid
throttle
prevented
backfires
idling
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
GB387830A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB387830A priority Critical patent/GB346503A/en
Publication of GB346503A publication Critical patent/GB346503A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02D2700/0248—Control of air or mixture supply for engines with compressor by means of throttle devices
    • F02D2700/0251—Control of air or mixture supply for engines with compressor by means of throttle devices in the intake conduit

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Abstract

346,503. Regulating; spray carburetters. ELLOR, J. E., 149, Burton Road, Derby. Feb. 5, 1930, No. 3878. [Classes 7 (iii) and 7 (vi).] In altitude controls for aircraft engines provided with supercharging-blowers, in which full opening of the throttle at ground level is prevented by an aneroid device acting through relay mechanism, for example as described in Specification 346,892, means are provided for preventing damage to the aneroid device by backfires, or by excessive vacuum, as when the engine is idling. An aneroid device b<2> subjected to the pressure in the inlet manifold a4 actuates a valve d which connects one side of a relay piston b<7> to the blower intake a<1>, and the other side to the blower outlet a<4>, thereby actuating a cam c acting on the pilot's throttle control h, h<1>. Damage due to backfires is prevented by the provision of small holes d<3>, d<4> in the communication between the aneroid chamber bl and the pipe g connected to the inlet manifold. Damage due to excessive vacuum when the engine is idling is prevented by a valve j<1> connected to the throttle by a rod j<3>, so as to open the aneroid chamber to atmosphere at j when the throttle approaches the closed position. The opening j also serves to drain away liquid fuel.
GB387830A 1930-02-05 1930-02-05 Improvements in means for regulating internal combustion engines for aircraft Expired GB346503A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB387830A GB346503A (en) 1930-02-05 1930-02-05 Improvements in means for regulating internal combustion engines for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB387830A GB346503A (en) 1930-02-05 1930-02-05 Improvements in means for regulating internal combustion engines for aircraft

Publications (1)

Publication Number Publication Date
GB346503A true GB346503A (en) 1931-04-16

Family

ID=9766572

Family Applications (1)

Application Number Title Priority Date Filing Date
GB387830A Expired GB346503A (en) 1930-02-05 1930-02-05 Improvements in means for regulating internal combustion engines for aircraft

Country Status (1)

Country Link
GB (1) GB346503A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2466441A (en) * 1943-09-01 1949-04-05 Bendix Aviat Corp Pressure responsive selector valve
DE763961C (en) * 1938-08-17 1955-04-28 Bosch Gmbh Robert Fuel supply device for diesel aircraft engines working with supercharging
US2746427A (en) * 1951-01-31 1956-05-22 Gen Motors Corp Pressure sensing apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE763961C (en) * 1938-08-17 1955-04-28 Bosch Gmbh Robert Fuel supply device for diesel aircraft engines working with supercharging
US2466441A (en) * 1943-09-01 1949-04-05 Bendix Aviat Corp Pressure responsive selector valve
US2746427A (en) * 1951-01-31 1956-05-22 Gen Motors Corp Pressure sensing apparatus

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