JPS63198433U - - Google Patents

Info

Publication number
JPS63198433U
JPS63198433U JP9052387U JP9052387U JPS63198433U JP S63198433 U JPS63198433 U JP S63198433U JP 9052387 U JP9052387 U JP 9052387U JP 9052387 U JP9052387 U JP 9052387U JP S63198433 U JPS63198433 U JP S63198433U
Authority
JP
Japan
Prior art keywords
hole
turbine
vane device
gas passage
gas 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.)
Pending
Application number
JP9052387U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP9052387U priority Critical patent/JPS63198433U/ja
Publication of JPS63198433U publication Critical patent/JPS63198433U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Turbines (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の一実施例を示す断面図、第2
図は他の実施例を示す断面図、第3図は従来例を
示す断面図である。 2……静翼、3……タービンハウジング、4…
…インナーシユラウド、5……ピニオンギア、7
……デイフユーザ部、8……孔、15……ピン、
15a……ネジ部、15b……先端、17……凹
部。
Fig. 1 is a sectional view showing one embodiment of the present invention;
The figure is a sectional view showing another embodiment, and FIG. 3 is a sectional view showing a conventional example. 2... Stationary blade, 3... Turbine housing, 4...
...Inner shroud, 5...Pinion gear, 7
...Diff user section, 8...hole, 15...pin,
15a...screw part, 15b...tip, 17...recessed part.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンの上流側の環状のガス流路を画成する
外周部材と内周部材を備え、この環状ガス流路に
複数枚の静翼が回転可能に設けられるガスタービ
ン用可変静翼装置において、前記静翼の回転中心
軸上を貫通する孔を形成し、この孔に挿通した棒
状部材を介して前記内周部材を前記外周部材に支
持したことを特徴とするガスタービン用可変静翼
装置。
A variable stator vane device for a gas turbine, comprising an outer peripheral member and an inner peripheral member defining an annular gas passage on the upstream side of the turbine, and a plurality of stator blades rotatably provided in the annular gas passage. A variable stator vane device for a gas turbine, characterized in that a hole is formed passing through the rotation center axis of the stator blade, and the inner circumferential member is supported by the outer circumferential member via a rod-shaped member inserted through the hole.
JP9052387U 1987-06-12 1987-06-12 Pending JPS63198433U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9052387U JPS63198433U (en) 1987-06-12 1987-06-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9052387U JPS63198433U (en) 1987-06-12 1987-06-12

Publications (1)

Publication Number Publication Date
JPS63198433U true JPS63198433U (en) 1988-12-21

Family

ID=30950470

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9052387U Pending JPS63198433U (en) 1987-06-12 1987-06-12

Country Status (1)

Country Link
JP (1) JPS63198433U (en)

Similar Documents

Publication Publication Date Title
JPS63198433U (en)
JPS62108501U (en)
JPS62138834U (en)
JPS6271339U (en)
JPH02145603U (en)
JPH01166727U (en)
JPS6369733U (en)
JPS61193230U (en)
JPS61144775U (en)
JPS63186973U (en)
JPS61149741U (en)
JPS63115532U (en)
JPS61126054U (en)
JPH03110102U (en)
JPH038631U (en)
JPS6222001U (en)
JPS61123801U (en)
JPH01173301U (en)
JPS62204166U (en)
JPS628393U (en)
JPS61194404U (en)
JPS61128342U (en)
JPS61204999U (en)
JPS62105336U (en)
JPS6133901U (en) Turbocharger variable nozzle