GB535253A - Improvements relating to aircraft engine cooling systems - Google Patents

Improvements relating to aircraft engine cooling systems

Info

Publication number
GB535253A
GB535253A GB2242939A GB2242939A GB535253A GB 535253 A GB535253 A GB 535253A GB 2242939 A GB2242939 A GB 2242939A GB 2242939 A GB2242939 A GB 2242939A GB 535253 A GB535253 A GB 535253A
Authority
GB
United Kingdom
Prior art keywords
duct
gap
spinner
radiator
aircraft engine
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
GB2242939A
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.)
JOHN VIVIAN STANBURY
Hawker Aircraft Ltd
Original Assignee
JOHN VIVIAN STANBURY
Hawker Aircraft 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 JOHN VIVIAN STANBURY, Hawker Aircraft Ltd filed Critical JOHN VIVIAN STANBURY
Priority to GB2242939A priority Critical patent/GB535253A/en
Publication of GB535253A publication Critical patent/GB535253A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P3/00—Liquid cooling
    • F01P3/18—Arrangements or mounting of liquid-to-air heat-exchangers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

535,253. Aircraft engine accessories. HAWKER AIRCRAFT, Ltd., and STANBURY, J. V. Aug. 2, 1939, No. 22429. [Class 4] A radiator 10 for engine cooling liquid or lubricant and designed to reduce aero-dynamic drag is arranged around the propeller shaft 4 in the tubular portion 7 of a cooling duct extending from the leading edge 5 of the aeroplane wing. The forward part 7a of the duct is reduced to form with a troughed ring 9 behind the spinner 6 a gap 8. Air enters slots in the leading edge of the wing and passes through passages 11, 12 to the duct 7, where it issues in a rearward direction through the annular gap 8 with a reaction effect. The gap may be varied in diameter by forming the tapered end 7a of the duct of a number of pivoted overlapping flaps or gills. The spinner may be made doublewalled for the passage of air from the radiator to prevent undue cooling of the mechanism for controlling the pitch of the airscrew.
GB2242939A 1939-08-02 1939-08-02 Improvements relating to aircraft engine cooling systems Expired GB535253A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2242939A GB535253A (en) 1939-08-02 1939-08-02 Improvements relating to aircraft engine cooling systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2242939A GB535253A (en) 1939-08-02 1939-08-02 Improvements relating to aircraft engine cooling systems

Publications (1)

Publication Number Publication Date
GB535253A true GB535253A (en) 1941-04-03

Family

ID=10179224

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2242939A Expired GB535253A (en) 1939-08-02 1939-08-02 Improvements relating to aircraft engine cooling systems

Country Status (1)

Country Link
GB (1) GB535253A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2824301A1 (en) * 2013-07-10 2015-01-14 Uav Engines Ltd Cooling of internal combustion engines
CN114194403A (en) * 2022-01-25 2022-03-18 广东汇天航空航天科技有限公司 Heat radiation structure of driving device and aircraft

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2824301A1 (en) * 2013-07-10 2015-01-14 Uav Engines Ltd Cooling of internal combustion engines
WO2015003853A1 (en) * 2013-07-10 2015-01-15 Uav Engines Ltd Cooling of internal combustion engines
EP2949900A1 (en) * 2013-07-10 2015-12-02 Uav Engines Ltd Cooling of internal combustion engines
CN105593487A (en) * 2013-07-10 2016-05-18 Uav发动机有限公司 Cooling of internal combustion engines
RU2665843C2 (en) * 2013-07-10 2018-09-04 Юав Энджинз Лтд Cooling of internal combustion engines
US10253677B2 (en) 2013-07-10 2019-04-09 Uav Engines Ltd. Cooling of internal combustion engines
CN105593487B (en) * 2013-07-10 2019-08-13 Uav发动机有限公司 The cooling of internal combustion engine
US10513965B2 (en) 2013-07-10 2019-12-24 Uav Engines Ltd. Cooling of internal combustion engines
KR20210037008A (en) * 2013-07-10 2021-04-05 유에이브이 엔진스 엘티디. Cooling of internal combustion engines
RU2750471C2 (en) * 2013-07-10 2021-06-28 Юав Энджинз Лтд Cooling of internal combustion engines
CN114194403A (en) * 2022-01-25 2022-03-18 广东汇天航空航天科技有限公司 Heat radiation structure of driving device and aircraft
CN114194403B (en) * 2022-01-25 2023-06-02 广东汇天航空航天科技有限公司 Heat radiation structure of driving device and aircraft

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