FR1368570A - Support of the downstream end of the combustion chamber of a gas turbo-engine - Google Patents

Support of the downstream end of the combustion chamber of a gas turbo-engine

Info

Publication number
FR1368570A
FR1368570A FR946926A FR946926A FR1368570A FR 1368570 A FR1368570 A FR 1368570A FR 946926 A FR946926 A FR 946926A FR 946926 A FR946926 A FR 946926A FR 1368570 A FR1368570 A FR 1368570A
Authority
FR
France
Prior art keywords
engine
support
combustion chamber
downstream end
gas turbo
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
FR946926A
Other languages
French (fr)
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries 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
Priority claimed from GB34650/62A external-priority patent/GB1010338A/en
Application filed by Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to FR946926A priority Critical patent/FR1368570A/en
Application granted granted Critical
Publication of FR1368570A publication Critical patent/FR1368570A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR946926A 1962-09-11 1963-09-09 Support of the downstream end of the combustion chamber of a gas turbo-engine Expired FR1368570A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR946926A FR1368570A (en) 1962-09-11 1963-09-09 Support of the downstream end of the combustion chamber of a gas turbo-engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB34650/62A GB1010338A (en) 1962-09-11 1962-09-11 Means for supporting the downstream end of a combustion chamber in a gas turbine engine
FR946926A FR1368570A (en) 1962-09-11 1963-09-09 Support of the downstream end of the combustion chamber of a gas turbo-engine

Publications (1)

Publication Number Publication Date
FR1368570A true FR1368570A (en) 1964-07-31

Family

ID=26203276

Family Applications (1)

Application Number Title Priority Date Filing Date
FR946926A Expired FR1368570A (en) 1962-09-11 1963-09-09 Support of the downstream end of the combustion chamber of a gas turbo-engine

Country Status (1)

Country Link
FR (1) FR1368570A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2356000A1 (en) * 1976-06-21 1978-01-20 Gen Electric TURBOMACHINE COMBUSTION CHAMBER SUPPORT DEVICE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2356000A1 (en) * 1976-06-21 1978-01-20 Gen Electric TURBOMACHINE COMBUSTION CHAMBER SUPPORT DEVICE

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