FR1475358A - Assemblage des moteurs à turbine - Google Patents

Assemblage des moteurs à turbine

Info

Publication number
FR1475358A
FR1475358A FR57085A FR57085A FR1475358A FR 1475358 A FR1475358 A FR 1475358A FR 57085 A FR57085 A FR 57085A FR 57085 A FR57085 A FR 57085A FR 1475358 A FR1475358 A FR 1475358A
Authority
FR
France
Prior art keywords
assembly
turbine engines
engines
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
FR57085A
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.)
Continental Aviation and Engineering Corp
Original Assignee
Continental Aviation and Engineering 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 Continental Aviation and Engineering Corp filed Critical Continental Aviation and Engineering Corp
Priority to FR57085A priority Critical patent/FR1475358A/fr
Application granted granted Critical
Publication of FR1475358A publication Critical patent/FR1475358A/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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • F05B2260/301—Retaining bolts or nuts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR57085A 1966-04-08 1966-04-08 Assemblage des moteurs à turbine Expired FR1475358A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR57085A FR1475358A (fr) 1966-04-08 1966-04-08 Assemblage des moteurs à turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR57085A FR1475358A (fr) 1966-04-08 1966-04-08 Assemblage des moteurs à turbine

Publications (1)

Publication Number Publication Date
FR1475358A true FR1475358A (fr) 1967-03-31

Family

ID=8605929

Family Applications (1)

Application Number Title Priority Date Filing Date
FR57085A Expired FR1475358A (fr) 1966-04-08 1966-04-08 Assemblage des moteurs à turbine

Country Status (1)

Country Link
FR (1) FR1475358A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2515734A1 (fr) * 1981-11-05 1983-05-06 Snecma Systeme d'ajustement du centrage d'une roue de turbomachine et turbomachine munie de moyens permettant l'application dudit systeme
EP2543828A3 (fr) * 2011-07-08 2014-07-30 Rolls-Royce plc Ensemble de joint destiné à une structure annulaire

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2515734A1 (fr) * 1981-11-05 1983-05-06 Snecma Systeme d'ajustement du centrage d'une roue de turbomachine et turbomachine munie de moyens permettant l'application dudit systeme
EP0079272A1 (fr) * 1981-11-05 1983-05-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Système d'ajustement du centrage d'une roue de turbomachine
US4548546A (en) * 1981-11-05 1985-10-22 S.N.E.C.M.A. Adjustment system of centering a turbomachine wheel and mounted turbomachine by way of permitting the application of said system
EP2543828A3 (fr) * 2011-07-08 2014-07-30 Rolls-Royce plc Ensemble de joint destiné à une structure annulaire
US9222369B2 (en) 2011-07-08 2015-12-29 Rolls-Royce Plc Joint assembly for an annular structure

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