CH320078A - Exhaust pipe of a gas turbine system - Google Patents

Exhaust pipe of a gas turbine system

Info

Publication number
CH320078A
CH320078A CH320078DA CH320078A CH 320078 A CH320078 A CH 320078A CH 320078D A CH320078D A CH 320078DA CH 320078 A CH320078 A CH 320078A
Authority
CH
Switzerland
Prior art keywords
gas turbine
exhaust pipe
turbine system
exhaust
pipe
Prior art date
Application number
Other languages
German (de)
Inventor
Henry Kerry Thomas
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH320078A publication Critical patent/CH320078A/en

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
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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)
  • Supercharger (AREA)
CH320078D 1953-02-10 1954-02-10 Exhaust pipe of a gas turbine system CH320078A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB320078X 1953-02-10

Publications (1)

Publication Number Publication Date
CH320078A true CH320078A (en) 1957-03-15

Family

ID=10331638

Family Applications (1)

Application Number Title Priority Date Filing Date
CH320078D CH320078A (en) 1953-02-10 1954-02-10 Exhaust pipe of a gas turbine system

Country Status (2)

Country Link
CH (1) CH320078A (en)
GB (1) GB746832A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19541890A1 (en) * 1995-11-10 1997-05-15 Asea Brown Boveri Gas turbine group

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3802187A (en) * 1972-06-01 1974-04-09 Avco Corp Exhaust system for rear drive engine
EP2423450A1 (en) * 2010-08-27 2012-02-29 Siemens Aktiengesellschaft Flow separator device for a condensation steam turbine with multiple outputs

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19541890A1 (en) * 1995-11-10 1997-05-15 Asea Brown Boveri Gas turbine group

Also Published As

Publication number Publication date
GB746832A (en) 1956-03-21

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