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51. 发明申请

US20190203620A1 TURBOPROP ENGINE ASSEMBLY WITH COMBINED ENGINE AND COOLING EXHAUST 审中-公开
公开(公告)号：US20190203620A1
公开(公告)日：2019-07-04
申请号：US16292846
申请日：2019-03-05
申请人： PRATT & WHITNEY CANADA CORP.
发明人： Andre JULIEN , Serge DUSSAULT , Jean THOMASSIN
IPC分类号： F01N3/05 , B64D27/08 , B64D33/04 , F02B61/04 , F02B53/14 , F01N13/08 , B64D27/02 , F02C7/18 , F02C6/20 , F02C5/00 , F02K1/38 , B64D33/10 , B64D27/10
CPC分类号： F01N3/055 , B64D27/02 , B64D27/08 , B64D27/10 , B64D33/04 , B64D33/10 , F01N13/082 , F01N2260/022 , F01N2270/02 , F02B53/14 , F02B61/04 , F02B2053/005 , F02C5/00 , F02C6/206 , F02C7/18 , F02K1/386 , F05D2260/213 , Y02T50/672 , Y02T50/676
摘要： A turboprop engine assembly for an aircraft, including an internal combustion engine having a liquid coolant system, an air duct in fluid communication with an environment of the aircraft, a heat exchanger received within the air duct having coolant passages in fluid communication with the liquid coolant system and air passages air passages in fluid communication with the air duct, and an exhaust duct in fluid communication with an exhaust of the internal combustion engine. The exhaust duct has an outlet positioned within the air duct downstream of the heat exchanger and upstream of an outlet of the air duct, the outlet of the exhaust duct spaced inwardly from a peripheral wall of the air duct. In use, a flow of cooling air surrounds a flow of exhaust gases. A method of discharging air and exhaust gases in an turboprop engine assembly having an internal combustion engine is also discussed.

52. 发明授权

US10006360B2 Rotary directional pressure engine 有权
公开(公告)号：US10006360B2
公开(公告)日：2018-06-26
申请号：US14705210
申请日：2015-05-06
申请人： Brian Schmidt
发明人： Brian Schmidt
IPC分类号： F02B55/02 , F02B53/10 , F02B55/14 , F02B53/14 , F01D1/22 , F01D1/28 , F01D1/34 , F01C1/00
CPC分类号： F02B55/02 , F01C1/00 , F01D1/22 , F01D1/28 , F01D1/34 , F02B53/10 , F02B53/14 , F02B55/14 , Y02T10/17
摘要： A rotary directional pressure engine having a case within which a plurality of rotors rotate in parallel. The rotors include asymmetrical cavities on the circumferential faces thereof, which cavities function to move air and/or other gases into a combustion chamber area during an intake phase, to cooperatively form a combustion chamber during an ignition and combustion phase, and to move exhaust gases to the area of one or more exhaust ports for removal from the engine during an exhaust phase. Continued rotation of the rotors is accomplished by harnessing and properly directing the forces of combustion against the asymmetrical cavities of the rotors.

53. 发明申请

US20180003106A1 Pivoting Piston Machine 审中-公开
公开(公告)号：US20180003106A1
公开(公告)日：2018-01-04
申请号：US15702365
申请日：2017-09-12
申请人： Innowatt GmbH
发明人： Herbert Huettlin
IPC分类号： F02B53/06 , F01L1/04 , F01L1/344 , F02B53/14
CPC分类号： F02B53/06 , F01C9/002 , F01C21/002 , F01C21/18 , F01L1/02 , F01L1/026 , F01L1/04 , F01L1/12 , F01L1/344 , F01L3/00 , F01L3/20 , F02B53/14
摘要： A pivoting piston machine includes a housing, a first piston and a second piston arranged in the housing, the first and second pistons being pivotable away from one another and toward one another about a pivot axis. The machine has a working chamber arranged between first and second piston. The working chamber increases and decreases in size in alternating fashion during pivoting of the first piston and of the second piston. The machine also has a inlet mouth for admission and discharge of the working medium. A closing element for closing and opening the inlet or the outlet has a valve disk interacting with a valve seat. Either the inlet mouth or the outlet mouth is arranged within the working chamber between the first end surface and the second end surface, and the valve seat and the valve disk are arranged at either the inlet mouth or the outlet mouth.

54. 发明申请

US20170058673A1 ROTARY MACHINE 有权
标题翻译：旋转机
公开(公告)号：US20170058673A1
公开(公告)日：2017-03-02
申请号：US15060355
申请日：2016-03-03
申请人： Lumenium LLC
发明人： William Anderson , Trent Lukaczyk , William Lukaczyk , Riccardo Meldolesi , Clive B. Lacy
IPC分类号： F01C1/04 , B64D27/16 , F01D5/12 , F01C21/10 , F04D29/38
CPC分类号： F01C1/04 , B64D27/16 , F01C21/001 , F01C21/008 , F01C21/02 , F01C21/06 , F01C21/08 , F01C21/0809 , F01C21/104 , F01D5/12 , F02B53/06 , F02B53/12 , F02B53/14 , F02B55/14 , F04C2/04 , F04D29/38 , Y02T10/17
摘要： The disclosure provides rotary machines that include, in one embodiment, a rotatable shaft defining a central axis A, the shaft having a first end and a second end. The shaft can have an elongate first island disposed thereon. The first island can have a body with a volume generally defined between front and rear surfaces that are spaced apart. The front and rear surfaces can lie in a plane parallel to a radial axis R. The perimeters of the front and rear surfaces can define a curved perimeter surface therebetween. The disclosure further provides embodiments having stationary islands and casings that rotate about the island.
摘要翻译：本公开提供了旋转机器，在一个实施例中包括限定中心轴线A的可旋转轴，该轴具有第一端和第二端。轴可以具有设置在其上的细长的第一岛。第一岛可以具有通常在间隔开的前表面和后表面之间限定的体积的主体。前表面和后表面可以位于平行于径向轴线R的平面中。前表面和后表面的周边可以在其间限定弯曲的周边表面。本公开进一步提供具有围绕岛旋转的固定岛和壳体的实施例。

55. 发明申请

US20170037776A1 AUXILIARY POWER UNIT WITH COMBINED COOLING OF GENERATOR 审中-公开
标题翻译：辅助发电机组合式发电机组
公开(公告)号：US20170037776A1
公开(公告)日：2017-02-09
申请号：US15227483
申请日：2016-08-03
申请人： PRATT & WHITNEY CANADA CORP.
发明人： Anthony JONES , Andre JULIEN , David MENHEERE , Jean THOMASSIN , Richard ULLYOTT
IPC分类号： F02B63/04 , F02B53/14 , B64D41/00 , F01P5/04 , F01P5/06 , F02B37/00 , F02B63/06 , F01P1/06
CPC分类号： F02B63/04 , B64D33/08 , B64D41/00 , F01C1/22 , F01C21/18 , F01P1/06 , F01P5/04 , F01P5/06 , F02B37/00 , F02B53/02 , F02B53/14 , F02B63/06 , F02B67/04 , F02B2053/005 , F02C5/00 , F02C7/14 , F02C7/18 , F02K5/00 , F05D2220/50 , F05D2260/213 , Y02T10/144 , Y02T10/17 , Y02T50/53 , Y02T50/672 , Y02T50/676
摘要： An auxiliary power unit for an aircraft, including an internal combustion engine having a liquid coolant system, a generator drivingly engaged to the internal combustion engine and having a liquid coolant system distinct from the liquid coolant system of the internal combustion engine, a first heat exchanger in fluid communication with the liquid coolant system of the internal combustion engine, a second heat exchanger in fluid communication with the liquid coolant system of the generator, an exhaust duct in fluid communication with air passages of the heat exchangers, and a fan received in the exhaust duct and rotatable by the internal combustion engine for driving a cooling air flow through the air passages. The liquid coolant system of the engine may be distinct from fuel and lubricating systems of the auxiliary power unit. A method of cooling a generator and an internal combustion engine is also discussed.
摘要翻译：一种用于飞行器的辅助动力单元，包括具有液体冷却剂系统的内燃机，与内燃机驱动接合并具有与内燃机的液体冷却剂系统不同的液体冷却剂系统的发电机，第一热交换器与所述内燃机的液体冷却剂系统流体连通的第二热交换器与所述发电机的液体冷却剂系统流体连通，与所述热交换器的空气通道流体连通的排气管道，排气管道，并且可由内燃机旋转，用于驱动通过空气通道的冷却空气流。发动机的液体冷却剂系统可以不同于辅助动力单元的燃料和润滑系统。还讨论了一种冷却发电机和内燃机的方法。

56. 发明申请

US20160245166A1 COMPOUND ENGINE ASSEMBLY WITH COAXIAL COMPRESSOR AND OFFSET TURBINE SECTION 有权
标题翻译：复合发动机组件与同轴压缩机和偏心涡轮机部分
公开(公告)号：US20160245166A1
公开(公告)日：2016-08-25
申请号：US14806880
申请日：2015-07-23
申请人： Pratt & Whitney Canada Corp.
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
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.
摘要翻译：一种复合发动机组件，其具有包括与发动机轴驱动接合的至少一个内燃机的发动机机芯，具有与发动机机芯的入口流体连通的出口的压缩机，并且包括至少一个转子，发动机轴，与压缩机转子驱动接合的发动机轴，以及涡轮部，其具有与发动机芯的出口流体连通的入口，并且包括接合在可旋转的涡轮轴上的至少一个转子，所述涡轮轴被配置为与发动机轴组合动力。涡轮机和发动机轴彼此平行并径向偏移，并且涡轮轴和压缩机转子的轴线彼此平行并径向偏移。还讨论了驱动飞行器的可旋转载荷的方法。

57. 发明申请

US20150337725A1 Combined driving system of an electric energy generator with the utilization of the pressure potential of a high-energy medium generated in the form of a mixture of exhaust gases and compressed air with the aid of a motor with rocking pistons with an integrated compressor section 审中-公开
公开(公告)号：US20150337725A1
公开(公告)日：2015-11-26
申请号：US14120131
申请日：2012-10-26
申请人： Jiri Frolik , Ceské vysoké ucení technické v Praze
发明人： Jiri Frolik , Jiri Nozicka , Renata Hruba
IPC分类号： F02B53/14 , F02B63/04 , F01C9/00
CPC分类号： F02B53/14 , F01C9/00 , F01C9/002 , F02B63/042 , Y02T10/17
摘要： The essence of the solution resides in that an internal combustion engine with rocking pistons is constituted by a shared working space in a shared housing (1) of the motor and a compressor in the central portion of which there are formed in a mirrored fashion combustion chambers (2, 2.1) containing rocking blades (3, 3.1) of the motor that are rigidly radially supported on a turnable central shaft (4) and in a carrier ring (4.1) and wherein the rocking blades (3, 3.1) are to advantage mutually angled with respect to each other and wherein the combustion chambers (2, 2.1) are delimited on the one side by delimiting partitions (5, 5.1) radially disposed at the inner circumferential surface of the shared housing (1) of the motor and the compressor and separating the combustion chambers (2, 2.1) from primary compressor chambers (6, 6.1) of the primary compressor part, and on the opposite side by a pair of rocking blades (3, 3.1) at the locations of their lower dead centers, and wherein on the opposite side of the pair of rocking blades (3, 3.1) there are formed secondary compressor chambers (7, 7.1) of a secondary compressor part delimited by end parts of a guiding segment (18) provided with secondary suction and outlet channels (19, 19.1) of a secondary compressor and wherein the turnable central shaft (4) extends with its end portions into external housings (1.1, 1.2) of a crankshaft mechanism that are connected in a mirror fashion to the shared housing (1) of the motor and the compressor, where the turnable central shaft (4) is provided with an oscillating yoke (8) having arms that are connected by means of a pair of piston rods (9, 9.1) with a pair of crankshafts (10, 10.1) on the outer ends of which there is supported a pair of flywheels (11, 11.1) that are provided on their peripheries with coils (12, 12.1) of a stator winding. A pressurized mixing chamber (17) that is connected to the outlet (28) of the exhaust gases from the rocking motor and to the outlet (29) of the pressurized air from the compressor part is provided with a main outlet (22) for the energy medium that is connected to the working expansion machine (23) that is connected with a working generator (25) of electric current, and the collection mixing chamber (17) is connected by a relief outlet (18) for the energy medium to an inlet (19) of a relief expansion machine (20) that is connected to a relief generator (21) of electric current that is electrically connected with coils (12, 12.1) of a stator winding. The combined driving system can be used primarily for the driving of generators of electric current, but its use is not limited to the driving of mobile machines and other apparatuses requiring rotary motion for their operation.

58. 发明申请

US20150273997A1 POWERTRAIN FOR INTERNAL-COMBUSTION ENGINE VEHICLE WITH COMBINATION OF PISTON ENGINE AND ROTARY ENGINE 审中-公开
标题翻译：内燃机动力传动系统与发动机和旋转发动机的组合
公开(公告)号：US20150273997A1
公开(公告)日：2015-10-01
申请号：US14674116
申请日：2015-03-31
申请人： Myungkoo KANG , Hyo Jeong Jeon
发明人： Myungkoo KANG , Hyo Jeong Jeon
IPC分类号： B60K5/08 , F16H3/00 , B60K17/02 , F02B73/00 , F02B53/14
CPC分类号： B60K5/08 , B60K6/387 , B60K6/48 , B60K2006/4816 , B60K2006/4825 , F02B53/14 , F02B73/00 , F02B75/22 , Y02T10/6221 , Y02T10/6252 , Y02T10/6256
摘要： Disclosed herein is a powertrain for an internal-combustion engine vehicle with a combination of a piston engine and a rotary engine. The powertrain includes a piston engine (10), a transmission (20), and a rotary engine (30). The piston engine (10) is provided as a primary power source. The transmission (20) is configured such that power produced from the piston engine (10) is transmitted to the transmission (20) through an output shaft (1). The rotary engine (30) is provided as a secondary power source and shares the output shaft (1) with the piston engine (10) and transmits produced power to the transmission (20). Power produced from the piston engine and power produced from the rotary engine are simultaneously or selectively transmitted to the transmission. Therefore, the present invention can have the advantages of the respective engines, whereby the performance and fuel efficiency per a unit engine displacement can be maximized.
摘要翻译：本文公开了一种具有活塞式发动机和旋转式发动机的组合的内燃机车辆的动力传动系。动力系包括活塞发动机（10），变速器（20）和旋转发动机（30）。活塞式发动机（10）设置为主动力源。变速器（20）构造成使得从活塞发动机（10）产生的动力通过输出轴（1）传递到变速器（20）。旋转发动机（30）被设置为二次动力源，并与活塞发动机（10）共用输出轴（1），并且将所产生的动力传递到变速器（20）。从活塞发动机产生的动力和从旋转发动机产生的动力同时或选择性地传递到变速器。因此，本发明可以具有各发动机的优点，由此能够使每单位发动机排量的性能和燃料效率最大化。

59. 发明申请

US20120139260A1 POWER SUPPLY SYSTEMS 失效
标题翻译：电源系统
公开(公告)号：US20120139260A1
公开(公告)日：2012-06-07
申请号：US13318100
申请日：2010-04-30
申请人： Julian Francis Dunne
发明人： Julian Francis Dunne
IPC分类号： H02K7/18 , H02P9/04
CPC分类号： B60K6/24 , B60K1/02 , B60K6/32 , B60K6/46 , B60L1/006 , B60L11/123 , B60L11/14 , B60L11/1816 , B60L11/1842 , B60L11/1844 , B60L11/1861 , B60L11/1887 , B60L2240/423 , B60L2240/441 , B60L2240/443 , F01C1/063 , F01C9/002 , F01C21/007 , F01C21/008 , F01C21/08 , F01C21/10 , F02B53/00 , F02B53/14 , F02B63/04 , F04C2240/30 , Y02E60/721 , Y02T10/17 , Y02T10/6217 , Y02T10/6269 , Y02T10/6295 , Y02T10/642 , Y02T10/7044 , Y02T10/705 , Y02T10/7072 , Y02T10/7077 , Y02T90/121 , Y02T90/128 , Y02T90/14 , Y02T90/163 , Y02T90/34 , Y04S10/126
摘要： A power supply system comprises an internal combustion engine (20) having a pair of opposed pistons (28, 30) and cylinder (32) within which the pistons move in use, the pistons (28, 30) and cylinder together forming a combustion chamber. The pair of opposed pistons (28, 30) and the cylinder (32) are each arranged to rotate, in use, about a common axis of rotation A with respect to an associated electric generator arrangement (22) so as to generate an electric output. The pair of opposed pistons (28, 30) are also arranged to together form a mass-elastic system that is capable of resonance and further arranged such that combustion in the combustion chamber causes the pistons (28, 30) to oscillate relative to each other about the common rotational axis (A).
摘要翻译：电源系统包括内燃机（20），其具有一对相对的活塞（28,30）和气缸（32），其中活塞在使用中移动，活塞（28,30）和气缸在一起形成燃烧室。一对相对的活塞（28,30）和气缸（32）各自布置成在使用中围绕相关联的发电机装置（22）绕共同的旋转轴线A旋转，以便产生电输出。一对相对的活塞（28,30）也布置成一起形成能够共振的质量弹性系统，并进一步布置成使得燃烧室中的燃烧使得活塞（28,30）相对于彼此振荡围绕公共旋转轴线（A）。

60. 发明申请

US20120031369A1 SEPARATE-TYPE ROTARY ENGINE 审中-公开
公开(公告)号：US20120031369A1
公开(公告)日：2012-02-09
申请号：US13264157
申请日：2010-05-01
申请人： Dockjong Ki
发明人： Dockjong Ki
IPC分类号： F02B55/14 , F02B53/00
CPC分类号： F02B53/14 , F01C1/46 , F01C11/004 , F02B53/08 , Y02T10/17
摘要： The aim of the present invention is to provide a separate-type rotary engine which significantly reduces vibrations and weight as compared to conventional cylinder-type internal combustion engines, which is simple in configuration and thus reduces manufacturing costs, which directly generates rotary force rather than through a crankshaft to increase mechanical efficiency, and in which a compressor and a force generator are separated from each other to enable the simple design of an engine suitable for a variety of uses. The engine of the present invention shown in FIG. 1 comprises: said compressor and force generator including housings 1 and 1′, each of which has a circular inner cross-sectional surface; rotors 3 and 3′,each of which has a circular or elliptical shape or a combination of a circular and elliptical shape, and rotates with one side thereof contacting the housing and the other side thereof spaced apart from the housing using the center of the circular inner space of the housing as an axis' and hinged vanes 9 and 9′, each of which has one end hinged to an upper portion of each of the housing 1 and 1′ and the other end contacting each of outer surfaces 4 and 4′ of the rotating rotors 3 and 3′ to prevent a drop in the pressure of the compressed air and combustion gas during compression and expansion. The thus-configured compressor and the force generator are further provided with a compressed air tank 12 interposed between a one-way check valve 11 and a compressed air valve 13 to store high-pressure compressed air, wherein the open/shut operation of the compressed air valve 13 is controlled in accordance with the rotation position of the rotor 3′ of the force generator, so as to store high-pressure compressed air; a fuel nozzle 15 for injecting fuel into the compressed air discharged at a high speed from the compressed air tank 12; an ignition device 16 for burning fuel in a combustion chamber 7; a gas exhaust port 18 formed at an end of an exhaust space 6-4 to discharge combustion gas to the outside of the engine; and an air intake port 17 formed at a front end of an air intake space 6-1 of the compressor to serve as a passage for introducing air from the outside of the compressor. The engine of the present invention is advantageous in that one combustion is performed per one rotation of each of the rotors, each of the rotors is located dead center in each of the housings rather than being eccentric, the expansion stroke of combustion gas is significantly longer to reduce vibrations and to improve engine efficiency as compared to a rotary engine (Wankel engine), and the compressor and the force generator are arranged independently from each other on a same rotary axis to enable easy changes in the sizes thereof and the simple design of an engine suitable for a variety of purposes.

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