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GB406485A - Improvements in or relating to means for use in cooling aircraft motors - Google Patents

Improvements in or relating to means for use in cooling aircraft motors

Info

Publication number
GB406485A
GB406485A GB6933/33A GB693333A GB406485A GB 406485 A GB406485 A GB 406485A GB 6933/33 A GB6933/33 A GB 6933/33A GB 693333 A GB693333 A GB 693333A GB 406485 A GB406485 A GB 406485A
Authority
GB
United Kingdom
Prior art keywords
wing
air
blower
orifices
radiator
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
GB6933/33A
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.)
Dornier Metallbauten GmbH
Original Assignee
Dornier Metallbauten GmbH
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 Dornier Metallbauten GmbH filed Critical Dornier Metallbauten GmbH
Publication of GB406485A publication Critical patent/GB406485A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • F01P11/10Guiding or ducting cooling-air, to, or from, liquid-to-air heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Cleaning Of Streets, Tracks, Or Beaches (AREA)

Abstract

406,485. Aircraft motor accessories. DORNIER METALLBAUTEN GES., and DORNIER, C., Friedrichshafen, Lake Constance. Germany. March 7, 1933, No. 6933. Convention date, May 20, 1932. [Class 4.] For cooling aircraft motors and for removing the boundary layer of air from the upper surface of the wings, a blower draws air through orifices in the surface and discharges it through a radiator or radiators which may be arranged in the wing. A blower d driven from the engine b draws air from a chamber f communicating with pipes h having branches i leading to orifices k in the upper surface of the wing. The air is discharged through a radiator e and through openings l in the fuselage just beneath the wing. Modifications are described in which both the blower and the radiator are arranged within the wing, the blower in one case being driven round by peripheral blades acted upon by jets of exhaust gases. In another case two blowers on a common transverse axis aspirate air through two radiators from the interior of the wing which has holes in its upper rear surface and the air is discharged through two orifices in the lower surface.
GB6933/33A 1932-05-20 1933-03-07 Improvements in or relating to means for use in cooling aircraft motors Expired GB406485A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE406485X 1932-05-20

Publications (1)

Publication Number Publication Date
GB406485A true GB406485A (en) 1934-03-01

Family

ID=6422071

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6933/33A Expired GB406485A (en) 1932-05-20 1933-03-07 Improvements in or relating to means for use in cooling aircraft motors

Country Status (1)

Country Link
GB (1) GB406485A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2285669A (en) * 1994-01-13 1995-07-19 Short Brothers Plc Boundary layer control in aerodynamic structures

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2285669A (en) * 1994-01-13 1995-07-19 Short Brothers Plc Boundary layer control in aerodynamic structures
US5743493A (en) * 1994-01-13 1998-04-28 Short Brothers Plc Boundary layer control in aerodynamic low drag structures
GB2285669B (en) * 1994-01-13 1998-06-10 Short Brothers Plc Boundary layer control in aerodynamic low drag structures

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