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
Authority: CH; Switzerland
Prior art keywords: turbine engine; exhaust duct; gas; gas turbine; separating hot
Prior art date: 1947-06-26

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.)

1947-06-26

Filing date

1948-06-26

Publication date

1950-01-15

1948-06-26 Application filed by Rolls Royce filed Critical Rolls Royce

1950-01-15 Publication of CH266201A publication Critical patent/CH266201A/de

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

1948
- 1948-06-21 US US34310A patent/US2578478A/en not_active Expired - Lifetime
- 1948-06-25 FR FR968350D patent/FR968350A/fr not_active Expired
- 1948-06-26 CH CH266201D patent/CH266201A/de unknown

Also Published As

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

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