| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | 带有转子间歇运动的旋转马达 | CN200680051198.X | 2006-11-27 | CN101360886A | 2009-02-04 | 本·科尼利厄斯 |
| 本发明提供了一种旋转马达，其包括可围绕第一轴线旋转的第一转子部件；可围绕第二轴线旋转的第二转子部件；以及传动系统，用于旋转第一转子部件和第二转子部件；其特征在于第一转子部件和第二转子部件适于以可变的角速度旋转。 | ||||||
| 42 | 旋转活塞的固定轴结构 | CN200610152193.8 | 2006-09-18 | CN101149017A | 2008-03-26 | 谭波 |
| 本发明是一种用于行星型旋转活塞发动机的旋转活塞的固定轴结构，属于旋转活塞发动机领域，解决了以前旋转活塞的冷却、活塞与其配合轴的润滑、冷却和进、排气口道狭窄的问题。它具有带偏心轴孔的主轴，主轴在端盖上的轴套中转动；与偏心轴孔转动配合的固定轴；旋转活塞与固定轴固定连接，固定轴固定在旋转活塞的中心轴线上或与旋转活塞是一体；实现主轴和固定轴运动关系的在缸体外的齿轮组件。 | ||||||
| 43 | 环面几何形状电动机系统 | CN200680003111.1 | 2006-01-09 | CN101116237A | 2008-01-30 | R·卡德尔 |
| 一种环面电动机系统包括中空定子和转子，转子由磁体组件沿着在中空定子中形成的转子路径驱动。转子作为转子路径中的活塞运行，以将流体吸入转子路径以及将流体从转子路径排出。转子上的力均趋向于将转子置于转子路径的中心。将转子加速而离开磁体系统上的入口端，并在转子接近于出口端时将转子减速。 | ||||||
| 44 | 利用内燃机的废热的系统 | CN200510062436.4 | 2005-03-28 | CN100340826C | 2007-10-03 | 宇野庆一; 麻弘知; 稻叶淳; 山中隆; 吉田秀治; 小川博史 |
| 一种废热能量回收系统具有制冷剂循环(10A)和兰金循环(30A)。当循环操作从制冷剂循环(10A)变为兰金循环(30A)时，膨胀装置(100)在泵(32)被起动之后起动。当循环操作从兰金循环(30A)变为制冷剂循环(10A)时，膨胀装置(100)在泵(32)被停止之后停止。 | ||||||
| 45 | 利用内燃机的废热的系统 | CN200510062436.4 | 2005-03-28 | CN1677022A | 2005-10-05 | 宇野庆一; 麻弘知; 稻叶淳; 山中隆; 吉田秀治; 小川博史 |
| 一种废热能量回收系统具有制冷剂循环(10A)和兰金循环(30A)。当循环操作从制冷剂循环(10A)变为兰金循环(30A)时，膨胀装置(100)在泵(32)被起动之后起动。当循环操作从兰金循环(30A)变为制冷剂循环(10A)时，膨胀装置(100)在泵(32)被停止之后停止。 | ||||||
| 46 | ACTUATOR OF LINK MECHANISM FOR INTERNAL COMBUSTION ENGINE | US15748265 | 2016-07-13 | US20180223730A1 | 2018-08-09 | Yoshihiro SUDA; Kotofumi YANAI; Kishiro NAGAI |
| Provided is an actuator of a link mechanism for an internal combustion engine, in which a speed reducer is sufficiently lubricated. The actuator includes an oil passage formed in a control shaft for changing the posture of a control link and configured to feed lubricant oil to the speed reducer; and an open portion which opens to face the speed reducer in one end side located on the speed reducer side, and which is in communication with the oil passage in the other end side. An inner diameter of the one end side of the open portion is larger than an outer diameter of one end side of the oil passage. | ||||||
| 47 | Multi-vane impeller device | US15264823 | 2016-09-14 | US10012081B2 | 2018-07-03 | Gregory T. Kemp; Joseph S. Orosz; John L. Montgomery |
| A device usable as an impeller has a plurality of vanes rotating eccentrically about a shaft. Eccentric rotation is enabled by a cam mounted on the shaft. The vanes are received within slots in a rotor which surrounds the shaft and rotates about an axis coaxial with the shaft. The rotor rotates within a housing having a cylindrical surface facing the rotor. The surface is eccentric to the shaft. The vanes execute reciprocal motion upon rotation of the rotor. The vane motion is constrained so that the edges of the vanes remain proximate to the cylindrical surface during rotation. | ||||||
| 48 | COMPOUND ENGINE ASSEMBLY WITH CANTILEVERED COMPRESSOR AND TURBINE | US15849977 | 2017-12-21 | US20180179948A1 | 2018-06-28 | Sylvain LAMARRE; Mike FONTAINE; Andre JULIEN; Michael GAUL; Jean THOMASSIN; Lazar MITROVIC |
| A compound engine assembly with an engine core including at least one internal combustion engine, a compressor, and a turbine section where the turbine shaft is configured to compound power with the engine shaft. The turbine section may include a first stage turbine and a second stage turbine. The turbine shaft is rotationally supported by a plurality of bearings all located on a same side of the compressor rotor(s) and all located on a same side of the turbine rotor(s), for example all located between the compressor rotor(s) and the turbine rotor(s), such that the compressor rotor(s) and the turbine rotor(s) are cantilevered. A method of driving a rotatable load of an aircraft is also discussed. | ||||||
| 49 | Electromagnetic only vane coordination of a cat and mouse engine | US15544029 | 2016-06-17 | US20180106151A1 | 2018-04-19 | Anatoli GALIN; Oleksandr GALIN; Natalia GALIN; Volodymyr GALIN |
| A rotary-vane internal combustion engine of the cat and mouse or scissor type with coordinated rotation of two co-axial shafts with position sensors creating chambers of variable volume for intake, compression, power and exhaust strokes. A reversible electric generator motor on at least one of the shafts with an electronic control system for current, an energy storage unit and electrical load. The total work done and angular speed is calculated or empirically determined while an alternating accelerating or decelerating torque is applied for a continuous, uniform rotation cycle. | ||||||
| 50 | Rotary Engine | US15804666 | 2017-11-06 | US20180066520A1 | 2018-03-08 | Alexander Shkolnik; Nikolay Shkolnik |
| A rotary engine includes an intake port, an exhaust port, a rotor having an intake channel and/or an exhaust channel, and a rotor shaft coupled to the rotor. The rotor shaft has an inflow channel in communication with the intake channel and/or an outlet channel in communication with the exhaust channel. The rotary engine includes a housing having a working chamber formed between the housing and the rotor, the working chamber configured to handle, in succession, an intake phase, a compression phase, a combustion phase, an expansion phase, and an exhaust phase. The inflow channel cyclically communicates with the intake port and forms a passage between the intake port and the working chamber through the rotor shaft and the intake channel. The outlet channel cyclically communicates with the exhaust port and forms a passage between the exhaust port and the working chamber through the rotor shaft and the exhaust channel. | ||||||
| 51 | SCISSOR TYPE COMPRESSION AND EXPANSION MACHINE USED IN A THERMAL ENERGY RECUPERATION SYSTEM | US15551927 | 2016-02-19 | US20180030858A1 | 2018-02-01 | Abdelaziz Gormat; Jean-Sylvain Bernard; Stéphane Tondelli; Bertrand Gessier |
| The invention relates to a compression and expansion machine comprising a body (12a) with at least one chamber (12) of revolution about an axis of symmetry, and pistons (14a, 14b, 14c, 14d) rotating about the axis of symmetry and dividing the chamber into cells (15a, 15b, 15c, 15d) rotating with the pistons, said machine furthermore comprising a device (22) for coordinating the movement of said pistons and configured so that, during one rotation cycle, each cell (15a, 15b, 15c, 15d) performs at least one first expansion/contraction cycle corresponding to a stage of compressing a first stream of gas passing through this cell and at least one second expansion/contraction cycle corresponding to a stage of expanding a second stream of gas passing through this cell. | ||||||
| 52 | Rotary piston and cylinder devices | US13060752 | 2009-08-28 | US09879534B2 | 2018-01-30 | Stephen F. Lindsey |
| A transmission assembly for a rotary piston and cylinder device, comprising a first gear (120) and a gear sub-assembly (15, 16, 17, 18, 19), the first gear connectable to a rotatably mounted shutter (12) of the device, and the first gear extending from a side of the shutter, and the first gear connected to the gear sub-assembly which converts rotation to an axis of rotation different to that of the shutter. | ||||||
| 53 | Compound engine assembly with cantilevered compressor and turbine | US14864084 | 2015-09-24 | US09869240B2 | 2018-01-16 | Sylvain Lamarre; Mike Fontaine; Andre Julien; Michael Gaul; Jean Thomassin; Lazar Mitrovic |
| A compound engine assembly with an engine core including at least one internal combustion engine, a compressor, and a turbine section where the turbine shaft is configured to compound power with the engine shaft. The turbine section may include a first stage turbine and a second stage turbine. The turbine shaft is rotationally supported by a plurality of bearings all located on a same side of the compressor rotor(s) and all located on a same side of the turbine rotor(s), for example all located between the compressor rotor(s) and the turbine rotor(s), such that the compressor rotor(s) and the turbine rotor(s) are cantilevered. A method of driving a rotatable load of an aircraft is also discussed. | ||||||
| 54 | Scroll Fluid Machine | US15505435 | 2015-03-17 | US20170268340A1 | 2017-09-21 | Hisashi OOTANI; Yasuomi MATSUMOTO; Takahisa TOBE |
| Scroll fluid machine (1) in which the dislodgement of a slide bush (56) and a spring (61), which are provided in an eccentric bush (36), is prevented. Provided in receiving hole (58) of eccentric bush (36) are slide bush (56), which is movable in the direction of eccentricity, and spring (61), which biases slide bush (56) in a moving direction. A spring holding section (56b) and engagement projections (56a) are formed on slide bush (56). After slide bush (56) is placed in the receiving hole (58), engagement projections (56a) engage with eccentric bush (36) in a state in which slide bush (56) has been moved by the biasing force of spring (61), thus preventing slide bush (56) from falling off the receiving hole (58), and the spring holding section (56b) prevents the spring (61) from falling off the receiving hole (58). | ||||||
| 55 | COMPRESSOR HAVING WASTE HEAT RECOVERY WITH GAS RECYCLER | US15006485 | 2016-01-26 | US20170211891A1 | 2017-07-27 | James C. Collins |
| A compressor and waste heat recovery system is disclosed in which mechanical work from a prime mover along with work generated from the waste heat recovery system are used to operate the compressor. A gas producing system is heated by waste heat from operation of the compressor to produce a stream of gas used to drive a turbine. The turbine is in work communication with the compressor. In one embodiment the gas producing system is a metal hydride. An overrunning clutch can be used with the turbine. In one form multiple gas producing systems are used, one of which to emit gas while the other is used to receive and capture the emitted gas. | ||||||
| 56 | Radial piston rotary device with compact gear drive mechanism | US15295985 | 2016-10-17 | US09677401B1 | 2017-06-13 | Adel K. Alsubaih; Khaled A. Alsubaih |
| The radial piston rotary device with compact gear drive mechanism includes a base, a casing mounted to the base, and a gearbox coupled to the casing. The casing houses a piston assembly with a pair of first radial pistons and a pair of second radial pistons coaxially mounted to the first radial pistons with each pair rotating at asynchronous, cyclically varying velocities. During a power cycle, a leading pair of radial pistons powers the associated gear assembly, and the gear assembly drives a flywheel assembly. A drive shaft axially extends from the flywheel assembly outside the gearbox to be selectively coupled to a driven component. The flywheel drives the pair of lagging radial pistons. During operation, each pair of radial pistons rotate at cyclically varying angular velocities out of phase with each other, yet produce a uniform output to the drive shaft. | ||||||
| 57 | FLUID DEVICE OUTPUT SHAFT WITH COATING | US14913051 | 2014-08-22 | US20160201463A1 | 2016-07-14 | Konishi Takashi; Eiji Fukuchi |
| A fluid device includes a housing defining a central bore, a plurality of commutator holes that extend radially outward from the central bore and a plurality of axial passages in fluid communication with the commutator holes. A fluid displacement assembly is in fluid communication with the housing. The fluid displacement assembly includes volume chambers in fluid communication with the axial passages of the housing. An output shaft includes a valving portion disposed in the central bore of the housing. The valving portion includes a first and second lands and a valving land disposed between the first and second lands. The first land cooperates with the central bore to define a first journal bearing and the second land cooperates with the central bore to define a second journal bearing. A coating is applied to the first and second lands of the output shaft. The coating includes a polyamide 11 material. | ||||||
| 58 | ROTARY DEVICE INCLUDING A COUNTERBALANCED SEAL ASSEMBLY | US14472151 | 2014-08-28 | US20160061039A1 | 2016-03-03 | Steven Lee Herbruck; Bradley Scott Farrenkopf |
| A rotary device is provided. The rotary device includes a housing having an inner surface and a rotor assembly mounted for rotation in the housing about an axis defining an axial direction of the rotary device. The rotor assembly includes a rotor and a seal assembly. The rotor includes a central portion and a plurality of arms extending radially outward from the central portion. Each arm has a distal end disposed for sliding engagement with the inner surface, and at least one of the arms has a channel defined therein. The seal assembly is disposed within the channel, and includes a seal, a base defining a seal channel configured to receive the seal, and a counterweight mechanism pivotally coupled to the base. The counterweight mechanism is configured to control a contact pressure exerted by the seal on the inner surface resulting from rotation of the rotor. | ||||||
| 59 | Combined motor and brake with rotating brake-release piston | US13944405 | 2013-07-17 | US09175563B2 | 2015-11-03 | Trimbak S. Attarde; Hrishikesh N. Thakur; Jay Paul Lucas |
| The present disclosure relates to a combined hydraulic motor and brake including a hydraulic motor having a hydraulic motor housing, a drive shaft assembly that is driven by the hydraulic motor, a stationary housing that is fixed relative to the hydraulic motor housing, and a rotatable housing that is rotatably driven by the drive shaft assembly. The combined hydraulic motor and brake also includes a brake for resisting relative rotation between the rotatable housing and the stationary housing, and a piston that is hydraulically actuated to release the brake. The piston is carried with the rotatable housing such that the piston, the rotatable housing and at least a portion of the drive shaft assembly are configured to rotate as a unit. | ||||||
| 60 | Rotary engine | US13733138 | 2013-01-02 | US09022005B2 | 2015-05-05 | Manousos Pattakos; Argyro Pattakou; Emmanouel Pattakos |
| In a “cat and mouse” rotary engine two rotor-pistons are connected by concentric crosses to two inclined power shafts, improving the balance of the engine, ridding the bearings of the rotor-pistons from heavy idle loads, allowing lighter and more robust structure and making the arrangement proper for divided load applications like portable flyers, REM etc. | ||||||
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