JPS5268609A - Fixing device for static wing in turbo-fan engine - Google Patents

Fixing device for static wing in turbo-fan engine

Info

Publication number
JPS5268609A
JPS5268609A JP14329675A JP14329675A JPS5268609A JP S5268609 A JPS5268609 A JP S5268609A JP 14329675 A JP14329675 A JP 14329675A JP 14329675 A JP14329675 A JP 14329675A JP S5268609 A JPS5268609 A JP S5268609A
Authority
JP
Japan
Prior art keywords
static wing
fixing device
turbo
fan engine
static
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.)
Granted
Application number
JP14329675A
Other languages
Japanese (ja)
Other versions
JPS5430446B2 (en
Inventor
Takaharu Ono
Takao Furuhashi
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.)
National Institute of Advanced Industrial Science and Technology AIST
Original Assignee
Agency of Industrial Science and Technology
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 Agency of Industrial Science and Technology filed Critical Agency of Industrial Science and Technology
Priority to JP14329675A priority Critical patent/JPS5268609A/en
Publication of JPS5268609A publication Critical patent/JPS5268609A/en
Publication of JPS5430446B2 publication Critical patent/JPS5430446B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE: In order to fix a static wing simply and with a high precision, devised is to set up a fixing device in which a groove is provided under the static wing fitting which is fixed to the static wing casing, and the convex which is provided on the upper-end of the static wing are used as a guide fo assemblying the static wing.
COPYRIGHT: (C)1977,JPO&Japio
JP14329675A 1975-12-04 1975-12-04 Fixing device for static wing in turbo-fan engine Granted JPS5268609A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14329675A JPS5268609A (en) 1975-12-04 1975-12-04 Fixing device for static wing in turbo-fan engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14329675A JPS5268609A (en) 1975-12-04 1975-12-04 Fixing device for static wing in turbo-fan engine

Publications (2)

Publication Number Publication Date
JPS5268609A true JPS5268609A (en) 1977-06-07
JPS5430446B2 JPS5430446B2 (en) 1979-10-01

Family

ID=15335428

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14329675A Granted JPS5268609A (en) 1975-12-04 1975-12-04 Fixing device for static wing in turbo-fan engine

Country Status (1)

Country Link
JP (1) JPS5268609A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4695225A (en) * 1983-08-30 1987-09-22 Bbc Brown, Boveri & Company, Limited Axial swirl body for generating rotary flows
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
JPH03141829A (en) * 1989-09-07 1991-06-17 General Electric Co <Ge> Fan/caul integrated superhigh bypass ratio engine and transportation and detachment thereof
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
US5312227A (en) * 1991-12-18 1994-05-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Turbine casing delimiting an annular gas flow stream divided by radial arms
US6884024B2 (en) * 2002-03-26 2005-04-26 Mtu Aero Engines Gmbh Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine
JP2016510377A (en) * 2012-12-31 2016-04-07 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ Multi-piece frame for turbine exhaust case
JP2016133106A (en) * 2015-01-22 2016-07-25 中電プラント株式会社 Stator block mounting jig

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
US4695225A (en) * 1983-08-30 1987-09-22 Bbc Brown, Boveri & Company, Limited Axial swirl body for generating rotary flows
JPH03141829A (en) * 1989-09-07 1991-06-17 General Electric Co <Ge> Fan/caul integrated superhigh bypass ratio engine and transportation and detachment thereof
US5312227A (en) * 1991-12-18 1994-05-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Turbine casing delimiting an annular gas flow stream divided by radial arms
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
US6884024B2 (en) * 2002-03-26 2005-04-26 Mtu Aero Engines Gmbh Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine
JP2016510377A (en) * 2012-12-31 2016-04-07 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ Multi-piece frame for turbine exhaust case
US10329957B2 (en) 2012-12-31 2019-06-25 United Technologies Corporation Turbine exhaust case multi-piece framed
JP2016133106A (en) * 2015-01-22 2016-07-25 中電プラント株式会社 Stator block mounting jig

Also Published As

Publication number Publication date
JPS5430446B2 (en) 1979-10-01

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