GB1048872A - Method of cooling the outer skin of aircraft and the like flying devices - Google Patents

Method of cooling the outer skin of aircraft and the like flying devices

Info

Publication number
GB1048872A
GB1048872A GB59964A GB59964A GB1048872A GB 1048872 A GB1048872 A GB 1048872A GB 59964 A GB59964 A GB 59964A GB 59964 A GB59964 A GB 59964A GB 1048872 A GB1048872 A GB 1048872A
Authority
GB
United Kingdom
Prior art keywords
aircraft
cooling
fuel
outer skin
jan
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
GB59964A
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.)
Airbus Defence and Space GmbH
Junkers Flugzeug und Motorenwerke AG
Original Assignee
Messerschmitt Bolkow Blohm AG
Junkers Flugzeug und Motorenwerke AG
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 Messerschmitt Bolkow Blohm AG, Junkers Flugzeug und Motorenwerke AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1048872A publication Critical patent/GB1048872A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/36—Structures adapted to reduce effects of aerodynamic or other external heating

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)

Abstract

1,048,872. Cooling aircraft. JUNKERSFLUGZEUGUND MOTORENWERKE A.G. Jan. 6, 1964 [Jan. 30, 1963], No. 599/64. Headings B7G and B7W. Fuel, e.g. liquid hydrogen, oxygen, fluorine, or ammonia, is led to a heated region of the outer skin of an aircraft or spacecraft, to absorb heat. Fuel is led through cooling ducts in passages on the inside of the wing leading edge skin and thence discharged through orientatable attitude-control nozzles at the wing tips. After use as a coolant, the fuel may alternatively be used to power auxiliary services.
GB59964A 1963-01-30 1964-01-06 Method of cooling the outer skin of aircraft and the like flying devices Expired GB1048872A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEJ0023082 1963-01-30

Publications (1)

Publication Number Publication Date
GB1048872A true GB1048872A (en) 1966-11-23

Family

ID=7201258

Family Applications (1)

Application Number Title Priority Date Filing Date
GB59964A Expired GB1048872A (en) 1963-01-30 1964-01-06 Method of cooling the outer skin of aircraft and the like flying devices

Country Status (1)

Country Link
GB (1) GB1048872A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4817855A (en) * 1984-10-11 1989-04-04 Allied-Signal Inc. Pressure vessel
US4986495A (en) * 1988-06-15 1991-01-22 Rockwell International Corporation Cooling structure
US5042565A (en) * 1990-01-30 1991-08-27 Rockwell International Corporation Fiber reinforced composite leading edge heat exchanger and method for producing same

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4817855A (en) * 1984-10-11 1989-04-04 Allied-Signal Inc. Pressure vessel
US4986495A (en) * 1988-06-15 1991-01-22 Rockwell International Corporation Cooling structure
US5042565A (en) * 1990-01-30 1991-08-27 Rockwell International Corporation Fiber reinforced composite leading edge heat exchanger and method for producing same

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