GB348316A - Improvements in regulating means for internal combustion engines for aircraft - Google Patents

Improvements in regulating means for internal combustion engines for aircraft

Info

Publication number
GB348316A
GB348316A GB1015330A GB1015330A GB348316A GB 348316 A GB348316 A GB 348316A GB 1015330 A GB1015330 A GB 1015330A GB 1015330 A GB1015330 A GB 1015330A GB 348316 A GB348316 A GB 348316A
Authority
GB
United Kingdom
Prior art keywords
arm
piston
pilot
pressure
aircraft
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
GB1015330A
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 GB1015330A priority Critical patent/GB348316A/en
Publication of GB348316A publication Critical patent/GB348316A/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)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

348,316. Regulating. ROYCE, SiR F. H., Nightingale Road, Derby. March 31, 1930, No. 10153. [Classes 7 (iii) and 7 (vi).] In an aircraft engine having a relay device controlled by the pressure in the induction pipe for automatically adjusting the throttle valve to prevent excessive cylinder pressures at low levels, means whereby the pilot may, by exerting sufficient force, overcome the action of the relav device comprises a lever having one arm g<1> connected to the pilot's hand control f, another arm g<2> contacting with the rod el of the relay piston e, and a third arm g<3> connected to the throttle valve g<7>. The relay piston e is controlled by a valve b<4> connected to an aneroid chamber b<1> arranged in a casing b connected at a<3> to the blower outlet a<2>. The valve admits the pressure from the blower outlet to one side of the piston e, and the pressure at the blower inlet a<1> to the opposite side, according to the change of altitude. As the aircraft descends, the piston e is moved to the right, so that the rod e<1> actuates the arm g<2> to close the throttle, but the pilot can overcome this action from the control f when necessary.
GB1015330A 1930-03-31 1930-03-31 Improvements in regulating means for internal combustion engines for aircraft Expired GB348316A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1015330A GB348316A (en) 1930-03-31 1930-03-31 Improvements in regulating means for internal combustion engines for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1015330A GB348316A (en) 1930-03-31 1930-03-31 Improvements in regulating means for internal combustion engines for aircraft

Publications (1)

Publication Number Publication Date
GB348316A true GB348316A (en) 1931-05-14

Family

ID=9962501

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1015330A Expired GB348316A (en) 1930-03-31 1930-03-31 Improvements in regulating means for internal combustion engines for aircraft

Country Status (1)

Country Link
GB (1) GB348316A (en)

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