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CA557096A - Gas turbine power plant installations - Google Patents

Gas turbine power plant installations

Info

Publication number
CA557096A
CA557096A CA557096A CA557096DA CA557096A CA 557096 A CA557096 A CA 557096A CA 557096 A CA557096 A CA 557096A CA 557096D A CA557096D A CA 557096DA CA 557096 A CA557096 A CA 557096A
Authority
CA
Canada
Prior art keywords
gas turbine
power plant
turbine power
plant installations
installations
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
CA557096A
Other languages
French (fr)
Inventor
L. Johnson Christopher
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 CA557096A publication Critical patent/CA557096A/en
Expired legal-status Critical Current

Links

CA557096A Gas turbine power plant installations Expired CA557096A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA557096T

Publications (1)

Publication Number Publication Date
CA557096A true CA557096A (en) 1958-05-06

Family

ID=35723502

Family Applications (1)

Application Number Title Priority Date Filing Date
CA557096A Expired CA557096A (en) Gas turbine power plant installations

Country Status (1)

Country Link
CA (1) CA557096A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3137408A1 (en) * 2022-06-29 2024-01-05 Safran Helicopter Engines Drained assembly of an aircraft turbomachine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3137408A1 (en) * 2022-06-29 2024-01-05 Safran Helicopter Engines Drained assembly of an aircraft turbomachine

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