GB471926A - Improvements in cooling systems for aircraft engines - Google Patents

Improvements in cooling systems for aircraft engines

Info

Publication number
GB471926A
GB471926A GB7663/36A GB766336A GB471926A GB 471926 A GB471926 A GB 471926A GB 7663/36 A GB7663/36 A GB 7663/36A GB 766336 A GB766336 A GB 766336A GB 471926 A GB471926 A GB 471926A
Authority
GB
United Kingdom
Prior art keywords
wing
radiators
aircraft
tunnels
channels
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
GB7663/36A
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.)
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 GB7663/36A priority Critical patent/GB471926A/en
Publication of GB471926A publication Critical patent/GB471926A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)

Abstract

471,926. Propelling aircraft. ELLOR, J. E. March 13, 1936, No. 7663. [Class 4] A liquid-cooled aircraft-engine is mounted outside of the aircraft wings and has radiators arranged in convergent - divergent tunnels accommodated in the wing and forward of the front or main wing-spar ; the inlet to the tunnel is disposed in the leading edge and the outlet beneath the wing such that air passes through the radiator with a downward inclination. As shown, an engine is situated in a fuselage A and is cooled by a liquid medium which is passed through radiators B<1> housed one in each wing. The radiators are inclined as shown and the area of the exit C<2> may be under the pilot's control. Heat may be added to the escaping air stream as described in Specification 454,266, either by leading the exhaust manifolds D through the channels or allowing the exhaust to discharge into the channels. The manifolds are led through tunnels D<1> having open front ends so that air can pass therethrough.
GB7663/36A 1936-03-13 1936-03-13 Improvements in cooling systems for aircraft engines Expired GB471926A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7663/36A GB471926A (en) 1936-03-13 1936-03-13 Improvements in cooling systems for aircraft engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7663/36A GB471926A (en) 1936-03-13 1936-03-13 Improvements in cooling systems for aircraft engines

Publications (1)

Publication Number Publication Date
GB471926A true GB471926A (en) 1937-09-13

Family

ID=9837418

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7663/36A Expired GB471926A (en) 1936-03-13 1936-03-13 Improvements in cooling systems for aircraft engines

Country Status (1)

Country Link
GB (1) GB471926A (en)

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