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GB621329A - Improvements relating to exhaust systems for gas turbine engines in aircraft - Google Patents

Improvements relating to exhaust systems for gas turbine engines in aircraft

Info

Publication number
GB621329A
GB621329A GB4723/47A GB472347A GB621329A GB 621329 A GB621329 A GB 621329A GB 4723/47 A GB4723/47 A GB 4723/47A GB 472347 A GB472347 A GB 472347A GB 621329 A GB621329 A GB 621329A
Authority
GB
United Kingdom
Prior art keywords
aircraft
tubes
propulsion
gas turbine
turbine engines
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
GB4723/47A
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 GB4723/47A priority Critical patent/GB621329A/en
Publication of GB621329A publication Critical patent/GB621329A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

621,329. Jet propulsion of aircraft. OULIANOFF. G., and DAVIS, C. A. Feb. 18, 1947, No. 4723. Drawings to Specification. [Class 110 (iii) ] In a jet-propulsion plant, the turbine exhaust conduit is divided and connects with two or more cylindrical exhaust and propulsion tubes arranged side by side. The tubes may be quite separate, or united by stays, or the adjacent parts of the tubes may be formed by a single plane part. Each tube may be provided with a propulsion nozzle, or, the tubes may lead to a part in which the several streams are united and brought to a single nozzle.
GB4723/47A 1947-02-18 1947-02-18 Improvements relating to exhaust systems for gas turbine engines in aircraft Expired GB621329A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4723/47A GB621329A (en) 1947-02-18 1947-02-18 Improvements relating to exhaust systems for gas turbine engines in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4723/47A GB621329A (en) 1947-02-18 1947-02-18 Improvements relating to exhaust systems for gas turbine engines in aircraft

Publications (1)

Publication Number Publication Date
GB621329A true GB621329A (en) 1949-04-07

Family

ID=9782569

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4723/47A Expired GB621329A (en) 1947-02-18 1947-02-18 Improvements relating to exhaust systems for gas turbine engines in aircraft

Country Status (1)

Country Link
GB (1) GB621329A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025667A (en) * 1957-07-22 1962-03-20 Boeing Co Rotary turret reversible thrust noise suppression jet engine nozzles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025667A (en) * 1957-07-22 1962-03-20 Boeing Co Rotary turret reversible thrust noise suppression jet engine nozzles

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