CA545787A - Appareil a combustion de moteurs a turbine a gaz - Google Patents

Appareil a combustion de moteurs a turbine a gaz

Info

Publication number
CA545787A
CA545787A CA545787A CA545787DA CA545787A CA 545787 A CA545787 A CA 545787A CA 545787 A CA545787 A CA 545787A CA 545787D A CA545787D A CA 545787DA CA 545787 A CA545787 A CA 545787A
Authority
CA
Canada
Prior art keywords
gas
turbine engines
combustion equipment
combustion
equipment
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
CA545787A
Other languages
English (en)
Inventor
Janes Ralph
W. Greenhough Vernon
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Publication date
Application granted granted Critical
Publication of CA545787A publication Critical patent/CA545787A/fr
Expired legal-status Critical Current

Links

CA545787A Appareil a combustion de moteurs a turbine a gaz Expired CA545787A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA545787T

Publications (1)

Publication Number Publication Date
CA545787A true CA545787A (fr) 1957-09-03

Family

ID=35702971

Family Applications (1)

Application Number Title Priority Date Filing Date
CA545787A Expired CA545787A (fr) Appareil a combustion de moteurs a turbine a gaz

Country Status (1)

Country Link
CA (1) CA545787A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US3751911A (en) * 1970-04-18 1973-08-14 Motoren Turbinen Union Air inlet arrangement for gas turbine engine combustion chamber

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US3751911A (en) * 1970-04-18 1973-08-14 Motoren Turbinen Union Air inlet arrangement for gas turbine engine combustion chamber

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