-
公开(公告)号：US11655731B2
公开(公告)日：2023-05-23
申请号：US16791375
申请日：2020-02-14
CPC分类号： F01D25/20 , F01M1/02 , F01M1/10 , F01M11/0004 , F16H57/0402 , F16H57/0436 , F16H57/0452 , F16H57/0457 , F01M2001/105 , F01M2001/1035
摘要： An oil supply system for supplying oil to a lubricating cavity of a gas turbine engine, the oil supply system has: a de-oiler having a de-oiler air-oil inlet, a de-oiler oil outlet hydraulically connected to the lubricating cavity, and a de-oiler air outlet in fluid flow communication with an environment outside of the oil supply system; and a closed-loop oil circuit including a main pump having a main pump inlet and a main pump outlet, the main pump outlet hydraulically connected to the lubricating cavity, a de-aerator having a de-aerator inlet hydraulically connected to a scavenge outlet of the lubricating cavity, a de-aerator air-oil outlet in fluid flow communication with the de-oiler inlet, and a de-aerator oil outlet hydraulically connected to the main pump inlet.
-
公开(公告)号：US10533487B2
公开(公告)日：2020-01-14
申请号：US15849991
申请日：2017-12-21
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Andre Julien , Mark Cunningham , Serge LaFortune , Pierre-Yves Legare
IPC分类号： F02B29/04 , F02C6/12 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F01C11/00 , F02B33/40 , F02B39/04 , F01C21/18 , F02M31/04 , F02M31/10 , F02B37/12 , F02B53/08 , F02B53/14 , F01C1/22
摘要： An engine assembly including an engine core including at least one internal combustion engine each including a rotor sealingly and rotationally received within a respective internal cavity to provide rotating chambers of variable volume in the respective internal cavity, a compressor having an outlet in fluid communication with an inlet of the engine core, a first intake conduit in fluid communication with an inlet of the compressor and with a first source of air, a second intake conduit in fluid communication with the inlet of the compressor and with a second source of air warmer than the first source of air, and a selector valve configurable to selectively open and close at least the fluid communication between the inlet of the compressor and the first intake conduit. A method of supplying air to a compressor is also discussed.
-
公开(公告)号：US10100730B2
公开(公告)日：2018-10-16
申请号：US14644503
申请日：2015-03-11
发明人： Roger Huppe , Pierre-Yves Legare
摘要： A gas turbine engine including a secondary air system with interconnected fluid passages defining at least one flow path between a common source of pressurized air and a common outlet. Some of the fluid passages deliver the pressurized air to components of the gas turbine engine. The fluid passages include a common fluid passage through which all circulation of the pressurized air to the common outlet passes. The common fluid passage has a section including a venturi configured for controlling a flow of the pressurized air from the source to the outlet. In one embodiment, the venturi is provided in a common inlet or common outlet passage. A method of pressurizing a secondary air system is also discussed.
-
公开(公告)号：US09932892B2
公开(公告)日：2018-04-03
申请号：US14806880
申请日：2015-07-23
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Jade Bilodeau , Andre Julien , Pierre-Yves Legare , Jason Nichols
IPC分类号： F02B53/14 , F02C3/04 , F02C6/12 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F01C11/00 , F02B29/04 , F02B33/40 , F02B39/04 , F02B41/10 , F02C3/107 , F02C6/00 , F02C6/20 , F01C21/18 , F02M31/04 , F02M31/10 , F01C1/22 , F02B53/00
CPC分类号： F02B53/14 , F01C1/22 , F01C11/008 , F01C21/18 , F02B29/0418 , F02B33/40 , F02B39/04 , F02B41/10 , F02B2053/005 , F02C3/04 , F02C3/107 , F02C6/00 , F02C6/12 , F02C6/20 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F02M31/042 , F02M31/10 , F02M31/107 , F05D2250/312 , F05D2260/40311 , F05D2260/98 , Y02T10/126 , Y02T10/146 , Y02T10/163 , Y02T10/17 , Y02T50/675
摘要： A compound engine assembly having an engine core including at least one internal combustion engine in driving engagement with an engine shaft, a compressor having an outlet in fluid communication with an inlet of the engine core and including at least one rotor rotatable about an axis coaxial with the engine shaft, the engine shaft in driving engagement with the compressor rotor, and a turbine section having an inlet in fluid communication with an outlet of the engine core and including at least one rotor engaged on a rotatable turbine shaft, the turbine shaft configured to compound power with the engine shaft. The turbine and engine shafts are parallel to and radially offset from one another, and the turbine shaft and the axis of the compressor rotor are parallel to and radially offset from one another. A method of driving a rotatable load of an aircraft is also discussed.
-
公开(公告)号：US09896998B2
公开(公告)日：2018-02-20
申请号：US14806902
申请日：2015-07-23
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Andre Julien , Mark Cunningham , Serge Lafortune , Pierre-Yves Legare
IPC分类号： F02G3/00 , F02G1/00 , F02C7/06 , F02C7/10 , B64D33/10 , B64D41/00 , F02B33/00 , F04C18/00 , F01C1/063 , F02B41/00 , F02C7/04 , F02C7/042 , F02C7/14 , F01C1/22 , F01C11/00 , F01C21/06 , F01C21/18 , F02C3/04 , F02C6/18
CPC分类号： F02B41/00 , B64D33/10 , F01C1/22 , F01C11/008 , F01C21/06 , F01C21/18 , F02C3/04 , F02C6/18 , F02C7/04 , F02C7/042 , F02C7/14 , Y02T50/675
摘要： A compound engine assembly including a compressor, an engine core including at least one rotary internal combustion engine and having an inlet in fluid communication with an outlet of the compressor, a turbine section having an inlet in fluid communication with an outlet of the engine core and configured to compound power with the engine core, and an air conduit having at least one heat exchanger extending thereacross. An outer wall of the air conduit has a plurality of openings defined therethrough downstream of the heat exchanger(s), each selectively closable by a pivotable flap movable between a retracted position where the opening is obstructed and an extended position away from the opening. Each opening defines a fluid communication between the air conduit and the ambient air when the respective flap is in the extended position. A method of directing flow through a compound engine assembly is also discussed.
-
公开(公告)号：US09797297B2
公开(公告)日：2017-10-24
申请号：US14806918
申请日：2015-07-23
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Andre Julien , Mark Cunningham , Serge Lafortune , Pierre-Yves Legare
IPC分类号： F02B29/04 , F01C1/22 , F01C11/00 , F02B33/34 , F02B41/10 , F02B61/04 , F01D13/00 , F02K5/00 , F02C6/12 , F02B53/00
CPC分类号： F02B29/0493 , F01C1/22 , F01C11/002 , F01C11/008 , F01D13/003 , F02B29/0412 , F02B29/0418 , F02B33/34 , F02B41/10 , F02B53/00 , F02B61/04 , F02B2053/005 , F02C6/12 , F02K5/00 , F05D2220/40 , Y02T10/146 , Y02T10/163 , Y02T10/17
摘要： A compound engine assembly including an air conduit having an inlet in fluid communication with ambient air around the compound engine assembly, a compressor having an inlet in fluid communication with the air conduit, an engine core including at least one rotary internal combustion engine and having an inlet in fluid communication with an outlet of the compressor, a turbine section having an inlet in fluid communication with an outlet of the engine core and configured to compound power with the engine core; and at least one heat exchanger in fluid communication with the air conduit, each heat exchanger configured to circulate a fluid of the engine assembly in heat exchange relationship with an airflow from the air conduit circulating therethrough. A method of supplying air to a compound engine assembly is also discussed.
-
公开(公告)号：US09879591B2
公开(公告)日：2018-01-30
申请号：US14806883
申请日：2015-07-23
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Andre Julien , Mark Cunningham , Serge Lafortune , Pierre-Yves Legare
IPC分类号： F02B29/04 , F02C6/12 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F02B37/12 , F02B53/08 , F02B53/14 , F01C11/00 , F02B39/04 , F01C21/18 , F02M31/04 , F02M31/10 , F01C1/22
CPC分类号： F02B29/0406 , F01C1/22 , F01C11/008 , F01C21/18 , F02B29/0412 , F02B33/40 , F02B37/12 , F02B39/04 , F02B53/08 , F02B53/14 , F02C6/12 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F02M31/042 , F02M31/10 , F02M31/107 , F05D2250/312 , F05D2260/40311 , F05D2260/98 , Y02T10/126 , Y02T10/17 , Y02T50/675
摘要： An intake assembly for a compressor providing compressed air to an internal combustion engine core, including an air conduit having at least one heat exchanger extending thereacross, an intake plenum for the compressor, a first intake conduit connected to the air conduit upstream of the heat exchanger(s), a second intake conduit connected to the air conduit downstream of the heat exchanger(s), and a selector valve configurable between a first configuration to allow a fluid communication between the intake plenum and the air conduit through the first intake conduit and a second configuration to prevent the fluid communication through the first intake conduit. Fluid communication between the intake plenum and the air conduit through the second intake conduit is allowed at least when the selector valve is in the second configuration. An engine assembly and method of supplying air to a compressor are also discussed.
-
公开(公告)号：US11371436B2
公开(公告)日：2022-06-28
申请号：US16744289
申请日：2020-01-16
发明人： Pierre-Yves Legare , Eric Langevin , Alain Martel
摘要： Systems and methods for regulating oil flow to an engine are described herein. An oil pressure target for the engine is determined based on one or more engine operating parameters. Oil flow to the engine is controlled based on the oil pressure target. Closed-loop feedback of oil pressure of the engine is obtained from at least one sensor during the controlling of the oil flow to the engine. A pressure difference between the oil pressure target and the closed-loop feedback of the oil pressure of the engine is determined. The oil flow to the engine is adjusted based on the pressure difference.
-
公开(公告)号：US11293295B2
公开(公告)日：2022-04-05
申请号：US16570066
申请日：2019-09-13
IPC分类号： F01D11/02 , F01D11/00 , F04D29/10 , F16J15/447
摘要： An aircraft engine having a shaft, an engine casing, at least one bearing located between the shaft and the engine casing, the engine casing defining a bearing cavity containing the at least one bearing, an air distribution system configured to inject compressed air to the bearing cavity to in use provide a sealing air flow entering the bearing cavity, and a labyrinth seal having a seal rotor and a seal stator, fins extending from one of the seal rotor and the seal stator toward the other of the seal rotor and the seal stator, at least one of the fins extending in an angled upstream direction relative to a direction of the sealing air flow.
-
公开(公告)号：US10883414B2
公开(公告)日：2021-01-05
申请号：US16707362
申请日：2019-12-09
发明人： Jean Thomassin , Sebastien Bolduc , Bruno Villeneuve , Stephane Berube , Mike Fontaine , David Gagnon-Martin , Andre Julien , Mark Cunningham , Serge Lafortune , Pierre-Yves Legare
IPC分类号： F02B29/04 , F02C6/12 , F02C7/047 , F02C7/052 , F02C7/055 , F02C7/14 , F02C7/36 , F01C11/00 , F02B33/40 , F02B39/04 , F01C21/18 , F02M31/04 , F02M31/10 , F02B37/12 , F02B53/08 , F02B53/14 , F01C1/22
摘要： An engine assembly including an engine core including at least one internal combustion engine each including a rotor sealingly and rotationally received within a respective internal cavity to provide rotating chambers of variable volume in the respective internal cavity, a compressor having an outlet in fluid communication with an inlet of the engine core, a first intake conduit in fluid communication with an inlet of the compressor and with a first source of air, a second intake conduit in fluid communication with the inlet of the compressor and with a second source of air warmer than the first source of air, and a selector valve configurable to selectively open and close at least the fluid communication between the inlet of the compressor and the first intake conduit. A method of supplying air to a compressor is also discussed.
-
-
-
-
-
-
-
-
-
搜索结果
13 条记录 (耗时 0.02 秒)
