JPH027301U - - Google Patents

Info

Publication number
JPH027301U
JPH027301U JP8507988U JP8507988U JPH027301U JP H027301 U JPH027301 U JP H027301U JP 8507988 U JP8507988 U JP 8507988U JP 8507988 U JP8507988 U JP 8507988U JP H027301 U JPH027301 U JP H027301U
Authority
JP
Japan
Prior art keywords
blade
groove
root
rotor blade
protrusion
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
JP8507988U
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 JP8507988U priority Critical patent/JPH027301U/ja
Publication of JPH027301U publication Critical patent/JPH027301U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案による流体機械の翼止溝の例を
示す要部構造断面図、第2図は第1図の―線
断面図、第3図は本考案による第1溝への各動翼
及び最終翼の植込み状態を示す一部平面図、第4
図は第3図の―線断面図である。第5図は従
来の流体機械の翼止溝を示す要部斜視図、第6図
はその動翼及び最終翼の植込み状態を示す一部平
面図、第7図は第6図の―線断面図、第8図
は第7図の―線断面図である。 1…回転体、2a…第1溝、2b…第2溝、3
…切欠き部、4…動翼、4a…動翼翼根部、5…
最終翼、5a…最終翼翼根部、6…肩部、9…突
起。
Fig. 1 is a cross-sectional view of the main part structure showing an example of the blade stop groove of a fluid machine according to the present invention, Fig. 2 is a cross-sectional view taken along the line - - in Fig. 1, and Fig. 3 is a cross-sectional view of each movement to the first groove according to the present invention. Partial plan view showing the installed state of the wing and the final wing, No. 4
The figure is a sectional view taken along the line -- in FIG. Fig. 5 is a perspective view of the main part showing the blade stop groove of a conventional fluid machine, Fig. 6 is a partial plan view showing the installed state of the rotor blade and the final blade, and Fig. 7 is a cross section taken along the line - - in Fig. 6. 8 is a sectional view taken along the line -- in FIG. 7. 1... Rotating body, 2a... First groove, 2b... Second groove, 3
... Notch, 4... Moving blade, 4a... Moving blade root, 5...
Final wing, 5a...Final wing root, 6...Shoulder, 9...Protrusion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 流体機械の回転体に動翼を植込むために各動翼
翼根部を収納する周方向の第1溝を有する翼止溝
において、翼根部の遠心方向移動を抑制する肩部
を周方向に連続的に設け、最終翼を収容する第2
溝を前記第1溝底面から回転中心部方向に穿設す
ると共に、各動翼翼根部を係止する突起を第2溝
上端部に設け、該突起の適当な位置に最終翼を第
1及び第2溝間で出入れ可能な切欠き部を少なく
とも一つ以上設けたことを特徴とする流体機械の
翼止溝。
In a blade stop groove having a circumferential first groove that accommodates the blade root of each rotor blade in order to embed the rotor blade in a rotating body of a fluid machine, a shoulder part that suppresses centrifugal movement of the blade root is continuous in the circumferential direction. The second wing is installed in the
A groove is bored from the bottom surface of the first groove toward the center of rotation, and a protrusion for locking the root of each rotor blade is provided at the upper end of the second groove, and the final blade is attached to the first and second grooves at an appropriate position of the protrusion. A blade stopper groove for a fluid machine, characterized in that at least one notch portion that can be taken in and out between two grooves is provided.
JP8507988U 1988-06-29 1988-06-29 Pending JPH027301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8507988U JPH027301U (en) 1988-06-29 1988-06-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8507988U JPH027301U (en) 1988-06-29 1988-06-29

Publications (1)

Publication Number Publication Date
JPH027301U true JPH027301U (en) 1990-01-18

Family

ID=31309752

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8507988U Pending JPH027301U (en) 1988-06-29 1988-06-29

Country Status (1)

Country Link
JP (1) JPH027301U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012102730A (en) * 2010-11-10 2012-05-31 General Electric Co <Ge> Turbine assembly, and method for securing closure bucket
JP2013217252A (en) * 2012-04-06 2013-10-24 Mitsubishi Heavy Ind Ltd Rotor, axial flow fluid machine provided with the same, blade attachment of rotor, and method of manufacturing rotor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012102730A (en) * 2010-11-10 2012-05-31 General Electric Co <Ge> Turbine assembly, and method for securing closure bucket
JP2013217252A (en) * 2012-04-06 2013-10-24 Mitsubishi Heavy Ind Ltd Rotor, axial flow fluid machine provided with the same, blade attachment of rotor, and method of manufacturing rotor

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