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HEYERMAN JEFFREY BERNARD, FIELDING BRUCE, OLVER BRYAN W, SMYTHE CARL: [fr] Système dassemblage de réacteur à double flux, [de] Montagesystem für Zweistromtriebwerk, [en] Turbofan mounting system. PRATT & WHITNEY CANADA, November 17, 2010: EP2251540-A2 (5 worldwide citation)

[en] A gas turbine engine has a rear mounting assembly (40) incorporating a mounting apparatus attached to a bypass duct wall (10) with a link device (46) for transferring core portion related inertia-induced loads, from an MTF (28) of the core portion (13) in a short circuit across an annular bypas ...


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HEYERMAN JEFFREY BERNARD, OLVER BRYAN, CAULFEILD STEPHEN: DISPOSITIF DINSTALLATION DE TURBINE, TURBOFAN MOUNTING ARRANGEMENT. PRATT & WHITNEY CANADA, PRATT & WHITNEY CANADA, NORTON ROSE FULBRIGHT CANADA S E N C R L S R L, January 22, 2019: CA2756914 (2 worldwide citation)

A gas turbine engine has a rear mounting structure incorporating a mounting apparatus attached to a bypass duct wall with a link device of six rods for transferring core portion related inertia-induced loads, from an inner case of the core portion in a short circuit across an annular bypass air pass ...


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Heyerman Jeffrey Bernard: Gas turbine rotor containment element with frangible connections. Pratt & Whitney Canada, October 31, 2007: EP1849964-A2

A containment system (22) for containing fragments of a burst rotor including first and second means (52, 54) for frangibly connecting a containment element (36) to first and second walls (46, 48), the first and second means (52, 54) rupturing upon being subjected to a load mainly produced by a tran ...


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Heyerman Jeffrey Bernard: Rotor containment element with frangible connections. Pratt & Whitney Canada, Heyerman Jeffrey Bernard, OGILVY RENAULT SENCRL, November 8, 2007: WO/2007/124559

A containment system (22) for containing fragments of a burst rotor (20) including first and second means (52, 54) for frangibly connecting a containment element (36) to first and second walls (46, 48), the first and second means (52, 54) rupturing upon being subjected to a load mainly produced by a ...


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HEYERMAN JEFFREY BERNARD, OLVER BRYAN W: SUPPORTS DE LIAISON AVEC DISPOSITIF DE REGLAGE VERROUILLABLE, SUPPORT LINKS WITH LOCKABLE ADJUSTMENT FEATURE. PRATT & WHITNEY CANADA, PRATT & WHITNEY CANADA, NORTON ROSE FULBRIGHT CANADA S E N C R L S R L, October 18, 2016: CA2702901

A cam-type apparatus is included in a support link between outer and inner cases of gas turbine engines for centering the cases one to another. The cam- type apparatus is lockable to allow locking an adjusted position of the cam-type apparatus.


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HEYERMAN JEFFREY BERNARD, OLVER BRYAN W, FIELDING BRUCE, SMYTHE CARL: SYSTEME DE MONTAGE POUR REACTEUR A DOUBLE FLUX, TURBOFAN MOUNTING SYSTEM. PRATT & WHITNEY CANADA, PRATT & WHITNEY CANADA, NORTON ROSE FULBRIGHT CANADA S E N C R L S R L, February 21, 2017: CA2702501

A gas turbine engine has a rear mounting assembly incorporating a mounting apparatus attached to a bypass duct wall with a link device for transferring core portion related inertia-induced loads, from an MTF of the core portion in a short circuit across an annular bypass air passage to the bypass du ...