GB574795A - Improvement in or relating to aeroplane construction - Google Patents

Improvement in or relating to aeroplane construction

Info

Publication number
GB574795A
GB574795A GB3198/44A GB319844A GB574795A GB 574795 A GB574795 A GB 574795A GB 3198/44 A GB3198/44 A GB 3198/44A GB 319844 A GB319844 A GB 319844A GB 574795 A GB574795 A GB 574795A
Authority
GB
United Kingdom
Prior art keywords
relating
improvement
supercharger
radiators
hood
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
GB3198/44A
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 GB3198/44A priority Critical patent/GB574795A/en
Publication of GB574795A publication Critical patent/GB574795A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10Radiator arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

574,795. Aircraft fuselages ; air inlets. MAAG, G. A. Feb. 21, 1944, No. 3198. [Class 4] The cockpit hood 1 of an aeroplane is extended forwardly of the windscreen 2 to form an airscoop 3 from which air is distributed to the engine, supercharger, radiator or cabin. The rear end of the scoop is closed by a partition 5 in which is a central opening to a conduit 8 leading to the supercharger and two openings to honeycomb radiators for the engine coolant. Conduits 14 from the radiators lead to discharge openings 15 in the walls of the fuselage. The hood 1. is preferably transparent.
GB3198/44A 1944-02-21 1944-02-21 Improvement in or relating to aeroplane construction Expired GB574795A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3198/44A GB574795A (en) 1944-02-21 1944-02-21 Improvement in or relating to aeroplane construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3198/44A GB574795A (en) 1944-02-21 1944-02-21 Improvement in or relating to aeroplane construction

Publications (1)

Publication Number Publication Date
GB574795A true GB574795A (en) 1946-01-21

Family

ID=9753800

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3198/44A Expired GB574795A (en) 1944-02-21 1944-02-21 Improvement in or relating to aeroplane construction

Country Status (1)

Country Link
GB (1) GB574795A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0743247A2 (en) * 1995-05-15 1996-11-20 The Boeing Company Passive cooling device and method for cooling an auxiliary power unit on an airoplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0743247A2 (en) * 1995-05-15 1996-11-20 The Boeing Company Passive cooling device and method for cooling an auxiliary power unit on an airoplane
EP0743247A3 (en) * 1995-05-15 1998-01-07 The Boeing Company Passive cooling device and method for cooling an auxiliary power unit on an airoplane

Similar Documents

Publication Publication Date Title
GB1009269A (en) Improvements in or relating to aircraft
GB574795A (en) Improvement in or relating to aeroplane construction
US2214723A (en) Windshield air scoop
GB568667A (en) Improvements in and relating to aircraft
GB454266A (en) Improvements in or relating to aircraft and other craft or vehicles
US2340195A (en) Airplane construction
GB585317A (en) Improvements in or relating to cooling arrangements for the engines of aircraft
US1511667A (en) Cooling system for the power plants of aircraft
GB839647A (en) Improvements relating to aeroplanes
GB472555A (en) Improvements in aircraft
GB606088A (en) Improvements relating to aeroplanes
GB526461A (en) Improvements in or relating to means for cooling aircraft engines or engine radiators
GB567072A (en) Screw and jet propelled aircraft
GB521881A (en) Improvements in or relating to the construction of aeroplanes
GB571592A (en) Improvements in aeroplanes
GB574347A (en) Propulsion means for an aircraft
GB542653A (en) Improvements in or relating to aircraft
GB753657A (en) Improvements in or relating to aircraft structures
GB578176A (en) An improved intake duct for supplying air to the engines of aircraft
GB605638A (en) Aircraft
GB605641A (en) Multi-engined airplane
FR950537A (en) Aircraft cabin air conditioning unit
GB547405A (en) Improvements in or relating to multi-engined aircraft
GB494576A (en) An improved method of and means for mounting air-cooled engines on aircraft
GB480345A (en) Improvements in cowlings for aircraft engines