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FR1439798A - Means for directing hot gases against the rotor blades of a gas turbine engine - Google Patents

Means for directing hot gases against the rotor blades of a gas turbine engine

Info

Publication number
FR1439798A
FR1439798A FR25118A FR25118A FR1439798A FR 1439798 A FR1439798 A FR 1439798A FR 25118 A FR25118 A FR 25118A FR 25118 A FR25118 A FR 25118A FR 1439798 A FR1439798 A FR 1439798A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
rotor blades
hot gases
directing hot
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
FR25118A
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.)
Old Carco LLC
Original Assignee
Chrysler Corp
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 Chrysler Corp filed Critical Chrysler Corp
Priority to FR25118A priority Critical patent/FR1439798A/en
Application granted granted Critical
Publication of FR1439798A publication Critical patent/FR1439798A/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)
FR25118A 1965-07-19 1965-07-19 Means for directing hot gases against the rotor blades of a gas turbine engine Expired FR1439798A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR25118A FR1439798A (en) 1965-07-19 1965-07-19 Means for directing hot gases against the rotor blades of a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR25118A FR1439798A (en) 1965-07-19 1965-07-19 Means for directing hot gases against the rotor blades of a gas turbine engine

Publications (1)

Publication Number Publication Date
FR1439798A true FR1439798A (en) 1966-05-20

Family

ID=8584765

Family Applications (1)

Application Number Title Priority Date Filing Date
FR25118A Expired FR1439798A (en) 1965-07-19 1965-07-19 Means for directing hot gases against the rotor blades of a gas turbine engine

Country Status (1)

Country Link
FR (1) FR1439798A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751486B1 (en) * 1968-05-20 1971-06-16 Sulzer Ag BRACKET FOR THE VANE SUPPORT OF A MULTISTAGE GAS TURBINE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751486B1 (en) * 1968-05-20 1971-06-16 Sulzer Ag BRACKET FOR THE VANE SUPPORT OF A MULTISTAGE GAS TURBINE

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