JP2010533815A5 - - Google Patents

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Publication number
JP2010533815A5
JP2010533815A5 JP2010517036A JP2010517036A JP2010533815A5 JP 2010533815 A5 JP2010533815 A5 JP 2010533815A5 JP 2010517036 A JP2010517036 A JP 2010517036A JP 2010517036 A JP2010517036 A JP 2010517036A JP 2010533815 A5 JP2010533815 A5 JP 2010533815A5
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JP
Japan
Prior art keywords
nozzle
chevron
flange
base
support flange
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.)
Granted
Application number
JP2010517036A
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English (en)
Japanese (ja)
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JP2010533815A (ja
JP5230736B2 (ja
Filing date
Publication date
Priority claimed from US11/779,518 external-priority patent/US7926285B2/en
Application filed filed Critical
Publication of JP2010533815A publication Critical patent/JP2010533815A/ja
Publication of JP2010533815A5 publication Critical patent/JP2010533815A5/ja
Application granted granted Critical
Publication of JP5230736B2 publication Critical patent/JP5230736B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010517036A 2007-07-18 2008-05-20 モジュール式シェブロン排気ノズル Active JP5230736B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/779,518 2007-07-18
US11/779,518 US7926285B2 (en) 2007-07-18 2007-07-18 Modular chevron exhaust nozzle
PCT/US2008/064184 WO2009025895A2 (en) 2007-07-18 2008-05-20 Modular chevron exhaust nozzle

Publications (3)

Publication Number Publication Date
JP2010533815A JP2010533815A (ja) 2010-10-28
JP2010533815A5 true JP2010533815A5 (https=) 2011-06-30
JP5230736B2 JP5230736B2 (ja) 2013-07-10

Family

ID=40263751

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010517036A Active JP5230736B2 (ja) 2007-07-18 2008-05-20 モジュール式シェブロン排気ノズル

Country Status (5)

Country Link
US (1) US7926285B2 (https=)
EP (1) EP2171244B1 (https=)
JP (1) JP5230736B2 (https=)
CA (1) CA2693844A1 (https=)
WO (1) WO2009025895A2 (https=)

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FR3082238A1 (fr) * 2018-06-11 2019-12-13 Airbus Operations Tuyere primaire d'un conduit d'ejection primaire d'une turbomachine
FR3100575B1 (fr) * 2019-09-05 2022-04-08 Safran Ceram Cone d’ejection a fixation flexible aerodynamique
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