JPS60100504U - radial turbine nozzle - Google Patents

radial turbine nozzle

Info

Publication number
JPS60100504U
JPS60100504U JP19149983U JP19149983U JPS60100504U JP S60100504 U JPS60100504 U JP S60100504U JP 19149983 U JP19149983 U JP 19149983U JP 19149983 U JP19149983 U JP 19149983U JP S60100504 U JPS60100504 U JP S60100504U
Authority
JP
Japan
Prior art keywords
nozzle
radial turbine
turbine nozzle
blade
walls
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
JP19149983U
Other languages
Japanese (ja)
Inventor
東作 高村
Original Assignee
日産自動車株式会社
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 日産自動車株式会社 filed Critical 日産自動車株式会社
Priority to JP19149983U priority Critical patent/JPS60100504U/en
Publication of JPS60100504U publication Critical patent/JPS60100504U/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第1図は従来のラジアルタービンノズルの構成の一例を
示す断面図、第2図は本考案ラジアルタービンノズルの
構成の一例を分解して示す断面図である。 1・・・・・・ロータの軸心、2・・・・・・ノズル翼
、2A・・・・・・前縁、2B・・・・・・後縁、3,
4・・・・・・ノズル壁、5・・・・・・嵌合溝、13
・・・・・・ノズル壁、23・・・・・・分離ノズル壁
部材、13A、23A−′・・・・・嵌合部。
FIG. 1 is a sectional view showing an example of the configuration of a conventional radial turbine nozzle, and FIG. 2 is an exploded sectional view showing an example of the configuration of the radial turbine nozzle of the present invention. 1... Rotor axis, 2... Nozzle blade, 2A... Leading edge, 2B... Trailing edge, 3.
4... Nozzle wall, 5... Fitting groove, 13
... Nozzle wall, 23 ... Separation nozzle wall member, 13A, 23A-' ... Fitting portion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ノズル翼と、該ノズル翼を挾持する2つのノズル壁とを
一体に形成したラジアルタービンノズルにおいて、前記
2つのノズル壁のうちの少なくとも一方は、前記ノズル
翼の後縁近傍の翼端部を露出可能となし、当該一方のノ
ズル壁には、前記露出部分を覆うようにしたリング部材
を分離可能に係合させたことを特徴とするラジアルター
ビンノズル。
In a radial turbine nozzle in which a nozzle blade and two nozzle walls that sandwich the nozzle blade are integrally formed, at least one of the two nozzle walls exposes a blade tip near the trailing edge of the nozzle blade. A radial turbine nozzle, characterized in that a ring member covering the exposed portion is separably engaged with one nozzle wall.
JP19149983U 1983-12-14 1983-12-14 radial turbine nozzle Pending JPS60100504U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19149983U JPS60100504U (en) 1983-12-14 1983-12-14 radial turbine nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19149983U JPS60100504U (en) 1983-12-14 1983-12-14 radial turbine nozzle

Publications (1)

Publication Number Publication Date
JPS60100504U true JPS60100504U (en) 1985-07-09

Family

ID=30412359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19149983U Pending JPS60100504U (en) 1983-12-14 1983-12-14 radial turbine nozzle

Country Status (1)

Country Link
JP (1) JPS60100504U (en)

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