FR1326037A - Turbine - Google Patents

Turbine

Info

Publication number
FR1326037A
FR1326037A FR900093A FR900093A FR1326037A FR 1326037 A FR1326037 A FR 1326037A FR 900093 A FR900093 A FR 900093A FR 900093 A FR900093 A FR 900093A FR 1326037 A FR1326037 A FR 1326037A
Authority
FR
France
Prior art keywords
turbine
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
FR900093A
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.)
NAPIER AERO ENGINES Ltd
Original Assignee
NAPIER AERO ENGINES 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
Application filed by NAPIER AERO ENGINES Ltd filed Critical NAPIER AERO ENGINES Ltd
Priority to FR900093A priority Critical patent/FR1326037A/en
Application granted granted Critical
Publication of FR1326037A publication Critical patent/FR1326037A/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
    • F01D9/04—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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR900093A 1962-06-07 1962-06-07 Turbine Expired FR1326037A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR900093A FR1326037A (en) 1962-06-07 1962-06-07 Turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR900093A FR1326037A (en) 1962-06-07 1962-06-07 Turbine

Publications (1)

Publication Number Publication Date
FR1326037A true FR1326037A (en) 1963-05-03

Family

ID=8780607

Family Applications (1)

Application Number Title Priority Date Filing Date
FR900093A Expired FR1326037A (en) 1962-06-07 1962-06-07 Turbine

Country Status (1)

Country Link
FR (1) FR1326037A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3314653A (en) * 1964-04-10 1967-04-18 Chrysler Corp Unitary nozzles and shroud sections
US4511306A (en) * 1982-02-02 1985-04-16 Westinghouse Electric Corp. Combustion turbine single airfoil stator vane structure
US4830571A (en) * 1986-02-24 1989-05-16 Tech Development Inc. Pneumatic starters
US5295787A (en) * 1991-10-09 1994-03-22 Rolls-Royce Plc Turbine engines
FR2846997A1 (en) * 2002-11-07 2004-05-14 Snecma Moteurs Mounting for aircraft gas turbine flow guides has flow guide sectors bolted directly in place on carrier and with sealing sectors to cover impingement surfaces
FR2922588A1 (en) * 2007-10-22 2009-04-24 Snecma Sa Rotor disk or drum i.e. booster drum, for e.g. turbojet engine of airplane, has flange including orifice for mounting bolt, where rim of bolt cooperates with edges of reinforcement of flange for immobilizing bolt in orifice
FR2978798A1 (en) * 2011-08-03 2013-02-08 Snecma Angular sector for rectifier of compressor in turbine of turboshaft engine e.g. turbojet, of aircraft, has hook projecting toward from suction face of blade, and recess receiving thinned part of external ring of sector of adjacent rectifier

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3314653A (en) * 1964-04-10 1967-04-18 Chrysler Corp Unitary nozzles and shroud sections
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US4511306A (en) * 1982-02-02 1985-04-16 Westinghouse Electric Corp. Combustion turbine single airfoil stator vane structure
US4830571A (en) * 1986-02-24 1989-05-16 Tech Development Inc. Pneumatic starters
US5295787A (en) * 1991-10-09 1994-03-22 Rolls-Royce Plc Turbine engines
FR2846997A1 (en) * 2002-11-07 2004-05-14 Snecma Moteurs Mounting for aircraft gas turbine flow guides has flow guide sectors bolted directly in place on carrier and with sealing sectors to cover impingement surfaces
FR2922588A1 (en) * 2007-10-22 2009-04-24 Snecma Sa Rotor disk or drum i.e. booster drum, for e.g. turbojet engine of airplane, has flange including orifice for mounting bolt, where rim of bolt cooperates with edges of reinforcement of flange for immobilizing bolt in orifice
FR2978798A1 (en) * 2011-08-03 2013-02-08 Snecma Angular sector for rectifier of compressor in turbine of turboshaft engine e.g. turbojet, of aircraft, has hook projecting toward from suction face of blade, and recess receiving thinned part of external ring of sector of adjacent rectifier

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