JPS57168023A - Gas turbine for high temperature - Google Patents

Gas turbine for high temperature

Info

Publication number
JPS57168023A
JPS57168023A JP56051744A JP5174481A JPS57168023A JP S57168023 A JPS57168023 A JP S57168023A JP 56051744 A JP56051744 A JP 56051744A JP 5174481 A JP5174481 A JP 5174481A JP S57168023 A JPS57168023 A JP S57168023A
Authority
JP
Japan
Prior art keywords
stator
rotor
turbine
gas turbine
blades
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.)
Pending
Application number
JP56051744A
Other languages
Japanese (ja)
Inventor
Shiro Takahashi
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.)
AGC Inc
Original Assignee
Asahi Glass Co 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 Asahi Glass Co Ltd filed Critical Asahi Glass Co Ltd
Priority to JP56051744A priority Critical patent/JPS57168023A/en
Publication of JPS57168023A publication Critical patent/JPS57168023A/en
Pending 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/18—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means
    • F01D1/20—Non-positive-displacement machines or engines, e.g. steam turbines without stationary working-fluid guiding means traversed by the working-fluid substantially axially

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To reduce the tensile stress in a captioned turbine greatly by providing a rotor outside a stator and burying moving blades made of ceramic material on the inside of the rotor for using the centrifugal force for the compressive force to the moving blades made of ceramics. CONSTITUTION:A gas turbine is constructed of a stator 1 in the center of the turbine and a stator 2 provided round the said stator 1. On the ouside of the stator blades 3 are planted. Meanwhile, the rotor 2 is supported by shafts 15 provided on its both ends in bearings 7 to be rotatable round the stator 1, and on its inside, ceramic gas turbine rotor blades 4 are provided toward the side of the stator 1 for constructing a turbine drive part together with the above-said stator blades 3.
JP56051744A 1981-04-08 1981-04-08 Gas turbine for high temperature Pending JPS57168023A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP56051744A JPS57168023A (en) 1981-04-08 1981-04-08 Gas turbine for high temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP56051744A JPS57168023A (en) 1981-04-08 1981-04-08 Gas turbine for high temperature

Publications (1)

Publication Number Publication Date
JPS57168023A true JPS57168023A (en) 1982-10-16

Family

ID=12895426

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56051744A Pending JPS57168023A (en) 1981-04-08 1981-04-08 Gas turbine for high temperature

Country Status (1)

Country Link
JP (1) JPS57168023A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6575699B1 (en) * 1999-03-27 2003-06-10 Rolls-Royce Plc Gas turbine engine and a rotor for a gas turbine engine
WO2019186144A1 (en) * 2018-03-27 2019-10-03 Intelligent Power Generation Limited Axial out-runner turbine and method for manufacturing a rotor section for that turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6575699B1 (en) * 1999-03-27 2003-06-10 Rolls-Royce Plc Gas turbine engine and a rotor for a gas turbine engine
WO2019186144A1 (en) * 2018-03-27 2019-10-03 Intelligent Power Generation Limited Axial out-runner turbine and method for manufacturing a rotor section for that turbine
CN112313393A (en) * 2018-03-27 2021-02-02 智能发电有限公司 Axial flow external rotor turbine and method for manufacturing rotor part of the turbine

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