CH266201A - Einrichtung zum Absondern von heissem Gas aus dem Auspuffkanal eines Gasturbinentriebwerkes. - Google Patents

Einrichtung zum Absondern von heissem Gas aus dem Auspuffkanal eines Gasturbinentriebwerkes.

Info

Publication number
CH266201A
CH266201A CH266201DA CH266201A CH 266201 A CH266201 A CH 266201A CH 266201D A CH266201D A CH 266201DA CH 266201 A CH266201 A CH 266201A
Authority
CH
Switzerland
Prior art keywords
turbine engine
exhaust duct
gas
gas turbine
separating hot
Prior art date
Application number
Other languages
English (en)
Inventor
Limited Rolls-Royce
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 CH266201A publication Critical patent/CH266201A/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
CH266201D 1947-06-26 1948-06-26 Einrichtung zum Absondern von heissem Gas aus dem Auspuffkanal eines Gasturbinentriebwerkes. CH266201A (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB266201X 1947-06-26
GB250648X 1948-06-25

Publications (1)

Publication Number Publication Date
CH266201A true CH266201A (de) 1950-01-15

Family

ID=26257464

Family Applications (1)

Application Number Title Priority Date Filing Date
CH266201D CH266201A (de) 1947-06-26 1948-06-26 Einrichtung zum Absondern von heissem Gas aus dem Auspuffkanal eines Gasturbinentriebwerkes.

Country Status (3)

Country Link
US (1) US2578478A (de)
CH (1) CH266201A (de)
FR (1) FR968350A (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2648193A (en) * 1951-04-10 1953-08-11 Westinghouse Electric Corp Anti-icing apparatus having means to control temperature and pressure of the heating gases
US2906092A (en) * 1955-02-10 1959-09-29 Haltenberger Jules Gas turbine engine with exhaust heat recovery
US3009630A (en) * 1957-05-10 1961-11-21 Konink Maschinenfabriek Gebr S Axial flow fans
US10683812B2 (en) * 2018-08-17 2020-06-16 Raytheon Technologies Corporation Dual valve system with mechanical linkage

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1782072A (en) * 1928-06-19 1930-11-18 Mckinstry Frank System for preventing the formation of ice on aircraft
US2501633A (en) * 1943-06-28 1950-03-21 Lockheed Aircraft Corp Gas turbine aircraft power plant having ducted propulsive compressor means
US2402363A (en) * 1943-10-21 1946-06-18 Westinghouse Electric Corp Turbine apparatus
US2418488A (en) * 1944-07-29 1947-04-08 Westinghouse Electric Corp Power-plant apparatus

Also Published As

Publication number Publication date
FR968350A (fr) 1950-11-24
US2578478A (en) 1951-12-11

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