JPS5177405U - - Google Patents

Info

Publication number
JPS5177405U
JPS5177405U JP15228374U JP15228374U JPS5177405U JP S5177405 U JPS5177405 U JP S5177405U JP 15228374 U JP15228374 U JP 15228374U JP 15228374 U JP15228374 U JP 15228374U JP S5177405 U JPS5177405 U JP S5177405U
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
JP15228374U
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 JP15228374U priority Critical patent/JPS5177405U/ja
Publication of JPS5177405U publication Critical patent/JPS5177405U/ja
Pending legal-status Critical Current

Links

JP15228374U 1974-12-16 1974-12-16 Pending JPS5177405U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15228374U JPS5177405U (en) 1974-12-16 1974-12-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15228374U JPS5177405U (en) 1974-12-16 1974-12-16

Publications (1)

Publication Number Publication Date
JPS5177405U true JPS5177405U (en) 1976-06-18

Family

ID=28443839

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15228374U Pending JPS5177405U (en) 1974-12-16 1974-12-16

Country Status (1)

Country Link
JP (1) JPS5177405U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010085405A (en) * 2008-09-29 2010-04-15 Rosemount Aerospace Inc Blade tip clearance measurement sensor and method for gas turbine engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010085405A (en) * 2008-09-29 2010-04-15 Rosemount Aerospace Inc Blade tip clearance measurement sensor and method for gas turbine engines

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