JP2009063166A5 - - Google Patents

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Publication number
JP2009063166A5
JP2009063166A5 JP2008213978A JP2008213978A JP2009063166A5 JP 2009063166 A5 JP2009063166 A5 JP 2009063166A5 JP 2008213978 A JP2008213978 A JP 2008213978A JP 2008213978 A JP2008213978 A JP 2008213978A JP 2009063166 A5 JP2009063166 A5 JP 2009063166A5
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JP
Japan
Prior art keywords
frame
fastener
ring
thermal
ribs
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
JP2008213978A
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English (en)
Japanese (ja)
Other versions
JP5317581B2 (ja
JP2009063166A (ja
Filing date
Publication date
Priority claimed from US11/851,622 external-priority patent/US20090067917A1/en
Application filed filed Critical
Publication of JP2009063166A publication Critical patent/JP2009063166A/ja
Publication of JP2009063166A5 publication Critical patent/JP2009063166A5/ja
Application granted granted Critical
Publication of JP5317581B2 publication Critical patent/JP5317581B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2008213978A 2007-09-07 2008-08-22 熱継手 Active JP5317581B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/851,622 2007-09-07
US11/851,622 US20090067917A1 (en) 2007-09-07 2007-09-07 Bipod Flexure Ring

Publications (3)

Publication Number Publication Date
JP2009063166A JP2009063166A (ja) 2009-03-26
JP2009063166A5 true JP2009063166A5 (enExample) 2011-10-06
JP5317581B2 JP5317581B2 (ja) 2013-10-16

Family

ID=40111025

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008213978A Active JP5317581B2 (ja) 2007-09-07 2008-08-22 熱継手

Country Status (4)

Country Link
US (3) US20090067917A1 (enExample)
EP (1) EP2034135B1 (enExample)
JP (1) JP5317581B2 (enExample)
CA (1) CA2638187C (enExample)

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US20090067917A1 (en) 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
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US9290261B2 (en) 2011-06-09 2016-03-22 United Technologies Corporation Method and assembly for attaching components
US10059431B2 (en) 2011-06-09 2018-08-28 United Technologies Corporation Method and apparatus for attaching components having dissimilar rates of thermal expansion
US9417422B2 (en) * 2011-08-23 2016-08-16 Bae Systems Information And Electronic Systems Integration Inc. Rigid adaptor ring for CTE mismatched optical device components
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US9856011B2 (en) * 2015-08-06 2018-01-02 The Boeing Company Method for the joining of wings or control surfaces to an airplane fuselage
US11149646B2 (en) 2015-09-02 2021-10-19 General Electric Company Piston ring assembly for a turbine engine
US9976746B2 (en) 2015-09-02 2018-05-22 General Electric Company Combustor assembly for a turbine engine
US10168051B2 (en) 2015-09-02 2019-01-01 General Electric Company Combustor assembly for a turbine engine
US10197278B2 (en) 2015-09-02 2019-02-05 General Electric Company Combustor assembly for a turbine engine
US10837640B2 (en) 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
US11402097B2 (en) 2018-01-03 2022-08-02 General Electric Company Combustor assembly for a turbine engine
FR3084916B1 (fr) * 2018-08-10 2020-07-17 Safran Ceramics Cone d'ejection a fixation flexible
US11767770B2 (en) 2021-08-10 2023-09-26 The Boeing Company Double bipod fitting to mitigate thermal loading of engine exhaust structures
US11901619B2 (en) 2021-12-16 2024-02-13 The Boeing Company Radome with ceramic matrix composite

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US8726675B2 (en) * 2007-09-07 2014-05-20 The Boeing Company Scalloped flexure ring
US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
US8459941B2 (en) * 2009-06-15 2013-06-11 General Electric Company Mechanical joint for a gas turbine engine
US9284969B2 (en) * 2012-02-24 2016-03-15 Pratt & Whitney Canada Corp. Thermal expansion joint connection for sheet metal assembly

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