GB521881A - Improvements in or relating to the construction of aeroplanes - Google Patents

Improvements in or relating to the construction of aeroplanes

Info

Publication number
GB521881A
GB521881A GB34917/38A GB3491738A GB521881A GB 521881 A GB521881 A GB 521881A GB 34917/38 A GB34917/38 A GB 34917/38A GB 3491738 A GB3491738 A GB 3491738A GB 521881 A GB521881 A GB 521881A
Authority
GB
United Kingdom
Prior art keywords
wing
fuselage
duct
partly
inlet
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
GB34917/38A
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.)
AVIONS KELLNER BECHEREAU
Original Assignee
AVIONS KELLNER BECHEREAU
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 AVIONS KELLNER BECHEREAU filed Critical AVIONS KELLNER BECHEREAU
Priority to GB34917/38A priority Critical patent/GB521881A/en
Publication of GB521881A publication Critical patent/GB521881A/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)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

521,881. Aircraft framework. BECHER-EAU, L., and AVIONS KELLNER-BECHEREAU SOC. ANON. Nov. 30, 1938, No. 34917. [Class 4] Structural members in the wing and between the wing and hull are hollow so as to form, partly in the wing and partly in the attaching member therefor, air ducts the inlet of which is located forwardly in the bottom or pressure side of the wing and the outlet at the near of the attaching member, the ducts accommodating the engine cooling devices. The wing 15 is connected to the fuselage 10 by a truss 16 and the radiator 18 is accommodated in the duct 17 the opening 19 of which is underneath the wing and the outlet through apertures 21. The inlet may be provided with dampers and the duct may be extended through the fuselage.
GB34917/38A 1938-11-30 1938-11-30 Improvements in or relating to the construction of aeroplanes Expired GB521881A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB34917/38A GB521881A (en) 1938-11-30 1938-11-30 Improvements in or relating to the construction of aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB34917/38A GB521881A (en) 1938-11-30 1938-11-30 Improvements in or relating to the construction of aeroplanes

Publications (1)

Publication Number Publication Date
GB521881A true GB521881A (en) 1940-06-03

Family

ID=10371513

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34917/38A Expired GB521881A (en) 1938-11-30 1938-11-30 Improvements in or relating to the construction of aeroplanes

Country Status (1)

Country Link
GB (1) GB521881A (en)

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