GB469615A - Improvements in or relating to power plants for aircraft - Google Patents

Improvements in or relating to power plants for aircraft

Info

Publication number
GB469615A
GB469615A GB3004/36A GB300436A GB469615A GB 469615 A GB469615 A GB 469615A GB 3004/36 A GB3004/36 A GB 3004/36A GB 300436 A GB300436 A GB 300436A GB 469615 A GB469615 A GB 469615A
Authority
GB
United Kingdom
Prior art keywords
engine
oil
radiator
cooler
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
GB3004/36A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB3004/36A priority Critical patent/GB469615A/en
Publication of GB469615A publication Critical patent/GB469615A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

469,615. Cooling cylinders ; crank cases. FAIREY AVIATION CO., Ltd., and FORSYTH, A. G. Jan. 31, 1936, No. 3004. [Class 7 (ii)] [Also in Groups XXXIII and XIII] A power plant for aircraft includes an enginecooling system, an oil-cooling system, a supercharging system, and means for preheating the air supply to the engine some of which parts are formed integrally with, and others being attached to, the engine crank-case which alone is adapted for attachment to the aircraft. As shown, a header tank n for the engine cooling system is connected by a pipe o to a radiator r disposed in a tunnel or recess of the engine cowling. The radiator r is connected to a pump u which delivers water to a water-jacket w from whence it passes by pipes x to the tank n. Air passing through an oil cooler 11 is led to the carburetter air-intake 13. Only a part of the air flowing through the radiator r may pass through the cooler 11. An oil suction pump 15 draws oil from the cooler in known manner. Superchargers b are provided.
GB3004/36A 1936-01-31 1936-01-31 Improvements in or relating to power plants for aircraft Expired GB469615A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3004/36A GB469615A (en) 1936-01-31 1936-01-31 Improvements in or relating to power plants for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3004/36A GB469615A (en) 1936-01-31 1936-01-31 Improvements in or relating to power plants for aircraft

Publications (1)

Publication Number Publication Date
GB469615A true GB469615A (en) 1937-07-29

Family

ID=9750123

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3004/36A Expired GB469615A (en) 1936-01-31 1936-01-31 Improvements in or relating to power plants for aircraft

Country Status (1)

Country Link
GB (1) GB469615A (en)

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