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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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OLVER BRYAN W: [fr] Un moteur à turbine à gaz comprenant un ensemble refroidisseur, [de] Ein Gasturbinentriebwerk mit einer Kühleranordnung, [en] A gas turbine engine with a bleed air cooler assembly. PRATT & WHITNEY CANADA, December 2, 2009: EP2128023-A1 (4 worldwide citation)

[en] A bleed air cooler assembly (36) of a gas turbine engine (10) comprises a cooler body (44) defining a fluid passage therein and a connector (52) detachably affixed with the cooler body (44) installed in an annular bypass air passage (28).


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Olver Bryan, Ciampa Alessandro, Marrano Roberto, Trepanier Richard, Lamarre Sylvain, Bernard Martin, Germain Patrick: Turbofan bypass duct air cooled fluid cooler installation. Pratt & Whitney Canada, March 12, 2008: EP1898069-A2 (3 worldwide citation)

A cooling apparatus for cooling a fluid in a bypass gas turbine engine comprises a heat exchanger (34) disposed within a bypass duct (30) and accommodated by a sub-passage defined by a flow divider (48) affixed to an annular wall (32) of the bypass_duct. The sub-passage defines an open upstream end ...


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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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Bruno Vittorio, Olver Bryan: An improved mounting system for installing a starter-generator to an accessory housing on a gas turbine engine. Pratt & Whitney Canada, Bruno Vittorio, Olver Bryan, BAILEY Todd D, July 1, 2004: WO/2004/055339 (1 worldwide citation)

A mounting system, for installing a starter-generator (13) to an accessory housing, (12) where the starter-generator (13) has a mounting end with a connecting flange (15) and a cooling air outlet radially inward of a peripheral starter-generator housing edge,(19) and where the accessory housing (18) ...


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Olver Bryan William: Enveloppe protectrice pour montage de cables, Protective saddle mount for cable tie. Pratt & Whitney Canada, Pratt & Whitney Canada, Ogilvy Renault Sencrl, April 19, 2011: CA2665890 (1 worldwide citation)

A method and apparatus for providing a mounting system for an elongated item such as a cable, tube or wire, or an assembly of multiple cables, tube and/or wires. The mounting system includes an apparatus for mounting to a supporting structure, and an apparatus for receiving the elongated item. Also ...


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Morenko Oleg, Olver Bryan: Tubulure de carburant interne et interface de carenage carburant, Internal fuel manifold and fuel fairing interface. Pratt & Whitney Canada, Pratt & Whitney Canada, Norton Rose Or Sencrl, July 26, 2011: CA2603370

A mounting system for an annular internal fuel manifold disposed within a gas turbine engine includes a fuel inlet assembly having a heat shield extending about at least a portion of an inner fuel inlet tube. The heat shield has a distal end engaged with the fuel manifold and has a radially outwardl ...


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