JPS51151400U - - Google Patents

Info

Publication number
JPS51151400U
JPS51151400U JP7166075U JP7166075U JPS51151400U JP S51151400 U JPS51151400 U JP S51151400U JP 7166075 U JP7166075 U JP 7166075U JP 7166075 U JP7166075 U JP 7166075U JP S51151400 U JPS51151400 U JP S51151400U
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
JP7166075U
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 JP7166075U priority Critical patent/JPS51151400U/ja
Publication of JPS51151400U publication Critical patent/JPS51151400U/ja
Pending legal-status Critical Current

Links

JP7166075U 1975-05-28 1975-05-28 Pending JPS51151400U (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7166075U JPS51151400U (ja) 1975-05-28 1975-05-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7166075U JPS51151400U (ja) 1975-05-28 1975-05-28

Publications (1)

Publication Number Publication Date
JPS51151400U true JPS51151400U (ja) 1976-12-03

Family

ID=28542272

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7166075U Pending JPS51151400U (ja) 1975-05-28 1975-05-28

Country Status (1)

Country Link
JP (1) JPS51151400U (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016185740A (ja) * 2015-03-27 2016-10-27 富士重工業株式会社 航空機の推力偏向装置及び航空機の推力偏向方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123321A (en) * 1964-03-03 Aircraft channel wing propeller combination
US3565208A (en) * 1970-02-02 1971-02-23 Rohr Corp Retractable silencing shield for jet engine nozzle
US3844375A (en) * 1973-04-30 1974-10-29 Boeing Co Noise shield for jet engine exhaust
US3844376A (en) * 1973-04-30 1974-10-29 Boeing Co Clamshell noise shield for engine exhaust

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123321A (en) * 1964-03-03 Aircraft channel wing propeller combination
US3565208A (en) * 1970-02-02 1971-02-23 Rohr Corp Retractable silencing shield for jet engine nozzle
US3844375A (en) * 1973-04-30 1974-10-29 Boeing Co Noise shield for jet engine exhaust
US3844376A (en) * 1973-04-30 1974-10-29 Boeing Co Clamshell noise shield for engine exhaust

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016185740A (ja) * 2015-03-27 2016-10-27 富士重工業株式会社 航空機の推力偏向装置及び航空機の推力偏向方法

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