GB530544A - Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes - Google Patents

Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes

Info

Publication number
GB530544A
GB530544A GB18664/39A GB1866439A GB530544A GB 530544 A GB530544 A GB 530544A GB 18664/39 A GB18664/39 A GB 18664/39A GB 1866439 A GB1866439 A GB 1866439A GB 530544 A GB530544 A GB 530544A
Authority
GB
United Kingdom
Prior art keywords
air
fairing
utilisation
relating
pipes
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
GB18664/39A
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 GB530544A publication Critical patent/GB530544A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof

Landscapes

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

Abstract

530,544. Propelling aircraft. JUNKERS FLUGZEUG - UND - MOTORENWERKE AKT.-GES. June 27, 1939, No. 18664. Convention date, July 9, 1938. Addition to 506,699. [Class 4] Aero-engine exhaust pipes constructed and arranged in the manner described in the parent Specification are surrounded by a fairing having air inlets adapted to direct air into the pipes. As shown, a single fairing 6 'having flanged inlets 9 is provided. A further air-inlet 7 is provided and air escapes to the atmosphere in the region of the outlet cross-sections of the pipes 2. In a modification the fairing 6 is surrounded by a further fairing having an airinlet at its leading edge. The air may be directed by inturned flanges or nozzles and a reflux propulsive effect may be obtained from the cooling air.
GB18664/39A 1938-07-09 1939-06-27 Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes Expired GB530544A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE530544X 1938-07-09

Publications (1)

Publication Number Publication Date
GB530544A true GB530544A (en) 1940-12-13

Family

ID=6554565

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18664/39A Expired GB530544A (en) 1938-07-09 1939-06-27 Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes

Country Status (1)

Country Link
GB (1) GB530544A (en)

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