JPS5666089U - - Google Patents

Info

Publication number
JPS5666089U
JPS5666089U JP14883079U JP14883079U JPS5666089U JP S5666089 U JPS5666089 U JP S5666089U JP 14883079 U JP14883079 U JP 14883079U JP 14883079 U JP14883079 U JP 14883079U JP S5666089 U JPS5666089 U JP S5666089U
Authority
JP
Japan
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
JP14883079U
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 JP14883079U priority Critical patent/JPS5666089U/ja
Publication of JPS5666089U publication Critical patent/JPS5666089U/ja
Pending legal-status Critical Current

Links

JP14883079U 1979-10-29 1979-10-29 Pending JPS5666089U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14883079U JPS5666089U (en) 1979-10-29 1979-10-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14883079U JPS5666089U (en) 1979-10-29 1979-10-29

Publications (1)

Publication Number Publication Date
JPS5666089U true JPS5666089U (en) 1981-06-02

Family

ID=29379948

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14883079U Pending JPS5666089U (en) 1979-10-29 1979-10-29

Country Status (1)

Country Link
JP (1) JPS5666089U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016509650A (en) * 2013-01-23 2016-03-31 コンセプツ・イーティーアイ・インコーポレーテッド Structure and method for forcibly coupling flow fields of adjacent wing elements of a turbomachine, and turbomachine incorporating the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016509650A (en) * 2013-01-23 2016-03-31 コンセプツ・イーティーアイ・インコーポレーテッド Structure and method for forcibly coupling flow fields of adjacent wing elements of a turbomachine, and turbomachine incorporating the same

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