FR1295745A - Conduit annulaire de transition pour turbo-réacteur - Google Patents

Conduit annulaire de transition pour turbo-réacteur

Info

Publication number
FR1295745A
FR1295745A FR868524A FR868524A FR1295745A FR 1295745 A FR1295745 A FR 1295745A FR 868524 A FR868524 A FR 868524A FR 868524 A FR868524 A FR 868524A FR 1295745 A FR1295745 A FR 1295745A
Authority
FR
France
Prior art keywords
turbo
reactor
transition duct
annular transition
annular
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
FR868524A
Other languages
English (en)
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft 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
Priority claimed from US44586A external-priority patent/US3086363A/en
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Priority to FR868524A priority Critical patent/FR1295745A/fr
Application granted granted Critical
Publication of FR1295745A publication Critical patent/FR1295745A/fr
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
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR868524A 1960-07-22 1961-07-20 Conduit annulaire de transition pour turbo-réacteur Expired FR1295745A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR868524A FR1295745A (fr) 1960-07-22 1961-07-20 Conduit annulaire de transition pour turbo-réacteur

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US44586A US3086363A (en) 1960-07-22 1960-07-22 Annular transition duct
FR868524A FR1295745A (fr) 1960-07-22 1961-07-20 Conduit annulaire de transition pour turbo-réacteur

Publications (1)

Publication Number Publication Date
FR1295745A true FR1295745A (fr) 1962-06-08

Family

ID=26191531

Family Applications (1)

Application Number Title Priority Date Filing Date
FR868524A Expired FR1295745A (fr) 1960-07-22 1961-07-20 Conduit annulaire de transition pour turbo-réacteur

Country Status (1)

Country Link
FR (1) FR1295745A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115163559A (zh) * 2022-06-24 2022-10-11 中国船舶重工集团公司第七0三研究所 一种低损失的压气机过渡段结构

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115163559A (zh) * 2022-06-24 2022-10-11 中国船舶重工集团公司第七0三研究所 一种低损失的压气机过渡段结构
CN115163559B (zh) * 2022-06-24 2024-05-17 中国船舶重工集团公司第七0三研究所 一种低损失的压气机过渡段结构

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