GB516099A - Improvements in and relating to engine-driven vehicles, especially aircraft, having radiators for cooling the engines thereof - Google Patents

Improvements in and relating to engine-driven vehicles, especially aircraft, having radiators for cooling the engines thereof

Info

Publication number
GB516099A
GB516099A GB23455/38A GB2345538A GB516099A GB 516099 A GB516099 A GB 516099A GB 23455/38 A GB23455/38 A GB 23455/38A GB 2345538 A GB2345538 A GB 2345538A GB 516099 A GB516099 A GB 516099A
Authority
GB
United Kingdom
Prior art keywords
cowling
casing
radiator
engine
radiators
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
GB23455/38A
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.)
Safran Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Publication of GB516099A publication Critical patent/GB516099A/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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10—Radiator arrangement
    • B64D33/12—Radiator arrangement of retractable type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

516,099. Engine radiators for aircraft &c. SOC. FRANCAISE HISPANO-SUIZA. Aug. 9, 1938, No. 23455. Convention date, Feb. 14. [Class- 64 (iii)] [Also in Group XXXIII] One or more aircraft engine cooling radiators R, Fig. 1, are mounted within a cowling C connected to the engine casing F, so that each radiator moves with the cowling when the inlet and outlet openings of the latter are adjusted by its movement relatively to the casing F. The cowling C is connected to the casing F by rods 5 which with the radiator make a deformable parallelogram. A recess 6 is provided in the casing F into which the radiator R and cowling C may be completely retracted, In a modfication, Fig. 4, the radiator R is connected to the casing F through a movable partition 7, and the cowling C is moved by a toothed rack and pinion 8, 9. In a further modification, Fig. 5, the radiator R may move parallel to itself, and is mounted on a rod 8 connected to the walls F by extensible partitions 7, 7<1>.
GB23455/38A 1938-02-14 1938-08-09 Improvements in and relating to engine-driven vehicles, especially aircraft, having radiators for cooling the engines thereof Expired GB516099A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE516099X 1938-02-14

Publications (1)

Publication Number Publication Date
GB516099A true GB516099A (en) 1939-12-21

Family

ID=3871192

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23455/38A Expired GB516099A (en) 1938-02-14 1938-08-09 Improvements in and relating to engine-driven vehicles, especially aircraft, having radiators for cooling the engines thereof

Country Status (1)

Country Link
GB (1) GB516099A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2234805A (en) * 1989-08-04 1991-02-13 Rolls Royce Plc A heat exchanger arrangement for a gas turbine engine
JP2011525452A (en) * 2008-06-26 2011-09-22 エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング Air path for supplying outside air into the aircraft
EP2497713A3 (en) * 2011-03-11 2012-11-21 Raytheon Company Heat exchanger in a free air stream
FR3022019A1 (en) * 2014-06-06 2015-12-11 Dassault Aviat PLATFORM THERMAL EXCHANGE DEVICE, PLATFORM AND ASSOCIATED METHOD
EP2557039A3 (en) * 2011-08-08 2016-05-11 The Boeing Company Aircraft supplemental liquid cooler and method

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2234805A (en) * 1989-08-04 1991-02-13 Rolls Royce Plc A heat exchanger arrangement for a gas turbine engine
JP2011525452A (en) * 2008-06-26 2011-09-22 エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング Air path for supplying outside air into the aircraft
EP2497713A3 (en) * 2011-03-11 2012-11-21 Raytheon Company Heat exchanger in a free air stream
AU2012200764B2 (en) * 2011-03-11 2013-12-19 Raytheon Company Free air stream heat exchanger design
US8636051B2 (en) 2011-03-11 2014-01-28 Raytheon Company Free air stream heat exchanger design
EP2557039A3 (en) * 2011-08-08 2016-05-11 The Boeing Company Aircraft supplemental liquid cooler and method
FR3022019A1 (en) * 2014-06-06 2015-12-11 Dassault Aviat PLATFORM THERMAL EXCHANGE DEVICE, PLATFORM AND ASSOCIATED METHOD

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