CH367662A - Gas turbine group - Google Patents

Gas turbine group

Info

Publication number
CH367662A
CH367662A CH7542059A CH7542059A CH367662A CH 367662 A CH367662 A CH 367662A CH 7542059 A CH7542059 A CH 7542059A CH 7542059 A CH7542059 A CH 7542059A CH 367662 A CH367662 A CH 367662A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine group
group
gas
turbine
Prior art date
Application number
CH7542059A
Other languages
French (fr)
Inventor
Noel Penny Robert
Spencer King Charles
Original Assignee
Rover Co Ltd
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 Rover Co Ltd filed Critical Rover Co Ltd
Priority to CH7542059A priority Critical patent/CH367662A/en
Publication of CH367662A publication Critical patent/CH367662A/en

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
    • F02C7/22—Fuel supply systems
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel
CH7542059A 1959-07-07 1959-07-07 Gas turbine group CH367662A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CH7542059A CH367662A (en) 1959-07-07 1959-07-07 Gas turbine group

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH7542059A CH367662A (en) 1959-07-07 1959-07-07 Gas turbine group

Publications (1)

Publication Number Publication Date
CH367662A true CH367662A (en) 1963-02-28

Family

ID=4534127

Family Applications (1)

Application Number Title Priority Date Filing Date
CH7542059A CH367662A (en) 1959-07-07 1959-07-07 Gas turbine group

Country Status (1)

Country Link
CH (1) CH367662A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991010054A1 (en) * 1989-12-21 1991-07-11 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5117636A (en) * 1990-02-05 1992-06-02 General Electric Company Low nox emission in gas turbine system
US5160069A (en) * 1989-09-21 1992-11-03 Allied-Signal Inc. Integrated power unit combustion apparatus and method
US5161363A (en) * 1989-09-21 1992-11-10 Allied-Signal Inc. Integrated power unit
US5214911A (en) * 1989-12-21 1993-06-01 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5317864A (en) * 1992-09-30 1994-06-07 Sundstrand Corporation Tangentially directed air assisted fuel injection and small annular combustors for turbines

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5160069A (en) * 1989-09-21 1992-11-03 Allied-Signal Inc. Integrated power unit combustion apparatus and method
US5161363A (en) * 1989-09-21 1992-11-10 Allied-Signal Inc. Integrated power unit
WO1991010054A1 (en) * 1989-12-21 1991-07-11 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5214911A (en) * 1989-12-21 1993-06-01 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5117636A (en) * 1990-02-05 1992-06-02 General Electric Company Low nox emission in gas turbine system
US5317864A (en) * 1992-09-30 1994-06-07 Sundstrand Corporation Tangentially directed air assisted fuel injection and small annular combustors for turbines

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