JPS5840503U - radial turbine nozzle - Google Patents
radial turbine nozzleInfo
- Publication number
- JPS5840503U JPS5840503U JP13428381U JP13428381U JPS5840503U JP S5840503 U JPS5840503 U JP S5840503U JP 13428381 U JP13428381 U JP 13428381U JP 13428381 U JP13428381 U JP 13428381U JP S5840503 U JPS5840503 U JP S5840503U
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- block body
- radial turbine
- turbine nozzle
- pins
- 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
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) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は、従来のラジアルタービンノズルの構造を示す
断面図、第２図は、同じ（その側断面を示す断面図、第
３図は、この考案の第１実施例を示す第１図と同様な断
面図、第４図ａ、 ｂ、 ｃ。
ｄは、同じくそのＣリング、溝付ピン、頭付ピン、及び
ホルダの各形状を示す斜視図、第５図は、この考案の第
２実施例を示す一部拡大断面図、第６図は、この考案の
第３実施例を示す一部拡大断面図である。
１．２１，３１．４１・・・・・・ノズル、７・・・・
・・タービンシュラウド、１１・・・・・・ブロック体
、１６・・・・・・タービンロータ、２２．３２・・・
・・・溝付ピン、２３゜３３．４３・・・・・・Ｃリン
グ、２４・・・・・・頭付ピン、２５．３５．４５・・
・・・・ボルト、２６．４６・・・・・・連結用ホルダ
。Fig. 1 is a sectional view showing the structure of a conventional radial turbine nozzle, Fig. 2 is a sectional view showing the same side cross section, and Fig. 3 is the same as Fig. 1 showing the first embodiment of this invention. Similar sectional views, Figures 4a, b, c, and d are perspective views showing the shapes of the C-ring, grooved pin, headed pin, and holder, and Figure 5 is the second cross-sectional view of this invention. FIG. 6 is a partially enlarged sectional view showing the third embodiment of this invention. 1.21, 31.41... Nozzle, 7...・・・
...Turbine shroud, 11...Block body, 16...Turbine rotor, 22.32...
...Slotted pin, 23°33.43...C ring, 24...Pin with head, 25.35.45...
...Bolt, 26.46...Connection holder.
Claims (1)
に向けて溝付ピンを一体的に植設し、他方に夫々該ピン
と反対方向に頭付ピン番一体的に植設し、前記溝付ピン
の溝にＣリングを嵌着することによりノズルとタービン
シュラウドとを一体化すると共に、前記頭付ピンを連結
用ホルダによってブロック体に弾性支持されるボルトに
連結させることにより、ノズルとブロック体とを一体化
したことを特徴とするラジアルタービンノズル。Grooved pins are integrally implanted outward at several locations in the circumferential direction of one of the flanges that sandwich the nozzle blades, and headed pin numbers are integrally implanted in the opposite direction to the pins on the other side, respectively. The nozzle and the turbine shroud are integrated by fitting a C ring into the groove of the grooved pin, and the nozzle is connected to a bolt elastically supported by the block body by a connecting holder. A radial turbine nozzle characterized by integrating a block body and a block body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13428381U JPS5840503U (en) | 1981-09-11 | 1981-09-11 | radial turbine nozzle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13428381U JPS5840503U (en) | 1981-09-11 | 1981-09-11 | radial turbine nozzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5840503U true JPS5840503U (en) | 1983-03-17 |
Family
ID=29927712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13428381U Pending JPS5840503U (en) | 1981-09-11 | 1981-09-11 | radial turbine nozzle |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5840503U (en) |
-
1981
- 1981-09-11 JP JP13428381U patent/JPS5840503U/en active Pending
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