JPS6445903A - Jig for inserting turbine blade - Google Patents

Jig for inserting turbine blade

Info

Publication number
JPS6445903A
JPS6445903A JP20317487A JP20317487A JPS6445903A JP S6445903 A JPS6445903 A JP S6445903A JP 20317487 A JP20317487 A JP 20317487A JP 20317487 A JP20317487 A JP 20317487A JP S6445903 A JPS6445903 A JP S6445903A
Authority
JP
Japan
Prior art keywords
blade
disc
rack
turbine
turbine blade
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
JP20317487A
Other languages
Japanese (ja)
Inventor
Toru Yoshida
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.)
Sumitomo Heavy Industries Ltd
Original Assignee
Sumitomo Heavy Industries 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 Sumitomo Heavy Industries Ltd filed Critical Sumitomo Heavy Industries Ltd
Priority to JP20317487A priority Critical patent/JPS6445903A/en
Publication of JPS6445903A publication Critical patent/JPS6445903A/en
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE:To perform automatic insertion of a blade into a disc, by a method wherein a turbine disc is placed on a base bed, meanwhile, a turbine blade temporarily assembled with a blade rack is lowered as it is rotated. CONSTITUTION:When a turbine blade (a) is assembled in a way to insert it into a turbine disc (b), the blade (a) is inserted in a female recessed part 1a of a blade rack 1 for temporary assembly. An engaging recessed part 1b of the blade rack 1 is engaged with a claw 2b of a suspension tool 2 for lifting, and the temporary assembly is moved to a given position. Consecutively, a press plate 4 is pressed by means of a cylinder 5, and is guided by means of a guide rail 7. The blade rack 1 is lowered as it is rotated, and the blade (a) is inserted in the disc (b). Thereafter, the claw 2b is released from engagement to lift up the suspension tool 2, an assembly of the blade (a) and the disc (b) is removed from the blade rack 1, and is moved to a given position.
JP20317487A 1987-08-17 1987-08-17 Jig for inserting turbine blade Pending JPS6445903A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20317487A JPS6445903A (en) 1987-08-17 1987-08-17 Jig for inserting turbine blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20317487A JPS6445903A (en) 1987-08-17 1987-08-17 Jig for inserting turbine blade

Publications (1)

Publication Number Publication Date
JPS6445903A true JPS6445903A (en) 1989-02-20

Family

ID=16469682

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20317487A Pending JPS6445903A (en) 1987-08-17 1987-08-17 Jig for inserting turbine blade

Country Status (1)

Country Link
JP (1) JPS6445903A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111203603A (en) * 2018-11-21 2020-05-29 中国航发商用航空发动机有限责任公司 Interchange clamping device for turbine disc
JP2021527180A (en) * 2018-06-12 2021-10-11 サフラン エアークラフト エンジンズ Retention system for blade wheel dismantling

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021527180A (en) * 2018-06-12 2021-10-11 サフラン エアークラフト エンジンズ Retention system for blade wheel dismantling
CN111203603A (en) * 2018-11-21 2020-05-29 中国航发商用航空发动机有限责任公司 Interchange clamping device for turbine disc

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