JPS5268610A - Supporting device for nozzle-wing in turbo-fan engine - Google Patents

Supporting device for nozzle-wing in turbo-fan engine

Info

Publication number
JPS5268610A
JPS5268610A JP14329775A JP14329775A JPS5268610A JP S5268610 A JPS5268610 A JP S5268610A JP 14329775 A JP14329775 A JP 14329775A JP 14329775 A JP14329775 A JP 14329775A JP S5268610 A JPS5268610 A JP S5268610A
Authority
JP
Japan
Prior art keywords
wing
nozzle
turbo
supporting device
fan engine
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
JP14329775A
Other languages
Japanese (ja)
Other versions
JPS5430447B2 (en
Inventor
Ichiro Katsumata
Norimasa Sagiya
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 JP14329775A priority Critical patent/JPS5268610A/en
Publication of JPS5268610A publication Critical patent/JPS5268610A/en
Publication of JPS5430447B2 publication Critical patent/JPS5430447B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE: A nozzle-wing is so organized to be slanted axially that a nozzle-wing can be sustained by a "full cantilever" suspension system. In so doing, aimed at is to minimize the stress applied to both the nozzle-wing and the flange section when the engine is in operation, and to enhance the efficiency of the turbine by reducing the volume of lea ked air.
COPYRIGHT: (C)1977,JPO&Japio
JP14329775A 1975-12-04 1975-12-04 Supporting device for nozzle-wing in turbo-fan engine Granted JPS5268610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14329775A JPS5268610A (en) 1975-12-04 1975-12-04 Supporting device for nozzle-wing in turbo-fan engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14329775A JPS5268610A (en) 1975-12-04 1975-12-04 Supporting device for nozzle-wing in turbo-fan engine

Publications (2)

Publication Number Publication Date
JPS5268610A true JPS5268610A (en) 1977-06-07
JPS5430447B2 JPS5430447B2 (en) 1979-10-01

Family

ID=15335455

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14329775A Granted JPS5268610A (en) 1975-12-04 1975-12-04 Supporting device for nozzle-wing in turbo-fan engine

Country Status (1)

Country Link
JP (1) JPS5268610A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5549510A (en) * 1978-10-02 1980-04-10 United Technologies Corp Rotary machine
US7290983B2 (en) * 2002-12-19 2007-11-06 Siemens Aktiengesellschaft Turbine, fixing device for blades and working method for dismantling the blades of a turbine
US7625181B2 (en) 2003-10-31 2009-12-01 Kabushiki Kaisha Toshiba Turbine cascade structure

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5549510A (en) * 1978-10-02 1980-04-10 United Technologies Corp Rotary machine
JPS633122B2 (en) * 1978-10-02 1988-01-22 Yunaitetsudo Tekunorojiizu Corp
US7290983B2 (en) * 2002-12-19 2007-11-06 Siemens Aktiengesellschaft Turbine, fixing device for blades and working method for dismantling the blades of a turbine
US7625181B2 (en) 2003-10-31 2009-12-01 Kabushiki Kaisha Toshiba Turbine cascade structure

Also Published As

Publication number Publication date
JPS5430447B2 (en) 1979-10-01

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