子分类：
| 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 | 圧縮装置 | JP2014168559 | 2014-08-21 | JP6242769B2 | 2017-12-06 | 橋本 宏一郎; 西村 和真; 足立 成人; 成川 裕; 松田 治幸; 垣内 哲也; 壷井 昇; 福原 一徳 |
| 42 | 圧縮装置 | JP2014168559 | 2014-08-21 | JP2016044583A | 2016-04-04 | 橋本 宏一郎; 西村 和真; 足立 成人; 成川 裕; 松田 治幸; 垣内 哲也; 壷井 昇; 福原 一徳 |
| 【課題】圧縮ガスの有する熱エネルギーの有効回収と圧縮ガスの圧力損失の低減との双方を達成可能な圧縮装置を提供すること。 【解決手段】圧縮装置であって、圧縮機(102)と、圧縮ガスの熱エネルギーを回収する熱エネルギー回収部(200)と、を備え、熱エネルギー回収部(200)が、流入口(202a)を有するとともに圧縮ガスの熱により作動媒体を加熱する熱交換器(202)と、膨張機(210)と、動力回収部(212)と、凝縮器(214)と、ポンプ(222)と、を備え、熱交換器(202)は、膨張機(210)よりも圧縮機(102)に近い位置でかつ流入口(202a)が圧縮機(102)側を向く姿勢で配置されていること。 【選択図】図1 |
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| 43 | ＩＤＡＲ−ＡＣＥ逆変位非対称回転−選択的コアエンジン | JP2015500536 | 2013-03-13 | JP2015514175A | 2015-05-18 | アンダースン，ウィリアム; ルカチック，トレント; ルカチック，ウィリアム |
| 本開示は、中心軸Aを画定する回転可能シャフトを含み、該シャフトが第1の端部および第2の端部を有する、エンジンまたはポンプを提供する。シャフトは、その上に配置される細長い第1のアイランドを有することができる。第1のアイランドは、離間される前面と後面との間に一般に画定される容積を伴う、本体を有することができる。前面および後面は、半径方向軸Rに平行な面の中に位置することができる。前面および後面の周辺部は、それらの間に湾曲周辺面を画定することができる。エンジンまたはポンプはさらに、第1のアイランドの前面に隣接して配置される前サイドプレートと、第1のアイランドの後面に隣接して配置される後サイドプレートとを含むことができる。エンジンまたはポンプはまた、前サイドプレートと後サイドプレートとの間に配置される、第1の輪郭部アセンブリも含む。【選択図】図1 | ||||||
| 44 | 遊星回転式流体モータ又は発動機及び圧縮機又はポンプ | JP2013513532 | 2011-05-31 | JP5629371B2 | 2014-11-19 | 其 槐 姚; ▲鎮▼ 姚 |
| 45 | ROTARY ENGINE | US16026098 | 2018-07-03 | US20180313262A1 | 2018-11-01 | Zhaoyan HAN |
| The present disclosure relates to a rotary engine which includes a cylinder having a gas inlet and a gas outlet, two rotors which are mounted inside the cylinder and can rotate freely, pistons fixed on the rotors, an ignition device provided on an inner wall of the cylinder and a planetary conical gear differential located outside the cylinder. The planetary conical gear differential includes a first sun gear and a second sun gear. The first rotor and the second rotor are superposed concentrically, the first rotor is connected to the first sun gear through a spindle, and the first rotor and the second rotor are connected to the planetary conical gear differential on a same side of the planetary conical gear differential. The cylinder is a circular ring body. The pistons are in circular motion along with the rotors. A differential rotary engine capable of rotating normally is provided. | ||||||
| 46 | Rotary directional pressure engine | US14705210 | 2015-05-06 | US10006360B2 | 2018-06-26 | Brian Schmidt |
| 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. | ||||||
| 47 | Wankel engine rotor | US13684390 | 2012-11-23 | US09593580B2 | 2017-03-14 | Jean-Gabriel Gauvreau; David Gagnon-Martin |
| A rotor for a Wankel engine including a plurality of ribs extending from a bearing support to each one of the flanks, the plurality of ribs including, for each flank, first and second ribs connected to the flank between the recess and a respective one of the apex portions. The first and second ribs are curved along at least a portion thereof, and/or the first and second ribs are closest to the respective apex portion and connected to the flank adjacent a junction between a portion of the flank defining the recess and a respective portion of the flank connected thereto. A method of reducing pinching of apex seals in a rotor of a Wankel engine is also discussed. | ||||||
| 48 | Internal gear pump having an eccentric inner rotor and outer rotor having teeth non-trochoid tooth profiles and a moving center of the outer rotor | US13670365 | 2012-11-06 | US09464525B2 | 2016-10-11 | Kenichi Fujiki; Masato Izutsu |
| An internal gear pump in which an inner rotor and an outer rotor are arranged in a rotor housing chamber. A deepest meshing section is located in the vicinity on a line connecting a center of the inner rotor and a center of the outer rotor. A center of the rotor housing chamber is offset, from a position in which the center and the center of the outer rotor coincide with each other, to the deepest meshing section side by an amount smaller than a tip clearance, which is a gap between the tooth tip of the inner rotor and the tooth tip of the outer rotor in the vicinity of a seal land between a terminal end side of an intake port and a start end side of a discharge port. | ||||||
| 49 | Rotary three dimensional variable volume machine | US13868237 | 2013-04-23 | US09206801B2 | 2015-12-08 | Arvind Kumar Sharma; Arvind Kumar Singh |
| An embodiment may have two rotary discs including a second disc (a cap) and a first disc; and a rotary ‘cam’ (having ports) placed in the central hole of the first disc. A cap is half the diameter of the first disc. Both face each other and maintain contour complementarity during both of two modes of operation The cap seals the cavity underneath, and without jeopardizing the sealing, permits entry and exit of the radial ridges and furrows of the first disc into it. The ridges sweep the floor (under surface) of the cap and divide the cavity into variable volume compartments that suck and expel fluid simultaneously through the ‘cam’. The machine is designed to work as rotary pump, compressor, turbine or internal combustion engine. | ||||||
| 50 | SYSTEM AND METHOD OF TRANSDUCING ENERGY FROM HYDROGEN | US13709836 | 2012-12-10 | US20140123923A1 | 2014-05-08 | Lawrence McMillan |
| A method of transducing energy from hydrogen, the method comprising: providing a chamber; maintaining a pressure of 75 psi to 30 in. vacuum within the chamber; injecting fuel into the chamber, where the fuel is hydrogen or a mix of hydrogen and oxygen; and igniting the fuel within the chamber. | ||||||
| 51 | IDAR-ACE inverse displacement asymmetric rotating alternative core engine | US13868359 | 2013-04-23 | US08714135B2 | 2014-05-06 | William Anderson; William Lukaczyk; Trent Lukaczyk |
| The disclosure provides engines or pumps that includes 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 engine or pump can further include a front side plate disposed adjacent to the front surface of the first island, and a rear side plate disposed adjacent to the rear surface of the first island. The engine or pump also includes a first contour assembly disposed between the front side plate and the rear side plate. | ||||||
| 52 | ROTARY THREE DIMENSIONAL VARIABLE VOLUME MACHINE | US13868237 | 2013-04-23 | US20140076155A1 | 2014-03-20 | Arvind Kumar Sharma; Arvind Kumar Singh |
| An embodiment may have two rotary discs including a second disc (a cap) and a first disc; and a rotary ‘cam’ (having ports) placed in the central hole of the first disc. A cap is half the diameter of the first disc. Both face each other and maintain contour complementarity (wall height of the second disc+radial depth of the first disc is constant at contact); either, when both discs rotate on their axes, placed the second disc's radius apart, or when the second disc rotates and revolves on the face of stationary first disc. The cap seals the cavity underneath during the two motions, and without jeopardizing the sealing, permits entry and exit of the radial ridges and furrows of the first disc into it. The ridges sweep the floor (under surface) of the cap and divide the cavity into variable volume compartments that suck and expel fluid simultaneously through the ‘cam’. The machine is designed to work as rotary pump, compressor, turbine or internal combustion engine. | ||||||
| 53 | IDAR-ACE INVERSE DISPLACEMENT ASYMMETRIC ROTATING ALTERNATIVE CORE ENGINE | US13868359 | 2013-04-23 | US20130251579A1 | 2013-09-26 | William Anderson; William Lukaczyk; Trent Lukaczyk |
| The disclosure provides engines or pumps that includes 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 engine or pump can further include a front side plate disposed adjacent to the front surface of the first island, and a rear side plate disposed adjacent to the rear surface of the first island. The engine or pump also includes a first contour assembly disposed between the front side plate and the rear side plate. | ||||||
| 54 | PLANETARY ROTARY TYPE FLUID MOTOR OR ENGINE AND COMPRESSOR OR PUMP | US13703202 | 2011-05-31 | US20130089447A1 | 2013-04-11 | Qihuai Yao; Frank Yao |
| A planetary rotary type rotation device comprises a stator, a rotor, and a center sun wheel drum (10). The stator includes a hollow cylinder block (1) having a cylinder. The rotor includes a main shaft (3), planetary piston wheel fixation flanges (9), and a planetary piston wheel (8). The two planetary piston wheel fixation flanges (9) are symmetrically fixed to the main shaft (3). The center sun wheel drum (10) is disposed between the two planetary piston wheel fixation flanges (9) and fitted over the main shaft (3). An annular piston space (19) is formed between an outer circular surface of the center sun wheel drum (10) and a cylinder wall of the cylinder of the cylinder block (1). The planetary piston wheel (8) is a cylindrical roller. The cylindrical roller is disposed in the annular piston space (19) in a rolling manner. Both ends of the cylindrical roller are fixed to the planetary piston wheel fixation flanges (9). A planetary rotary type fluid motor or engine, their operation method, and a planetary rotary type compressor or pump are disclosed. The planetary rotary type rotation device has a simple structure, a small volume, and a light weight. | ||||||
| 55 | OIL SEAL ARRANGEMENT FOR ROTARY INTERNAL COMBUSTION ENGINE | US13271883 | 2011-10-12 | US20130028771A1 | 2013-01-31 | Eugene GEKHT; Sebastlen Bolduc; Mike Fontaine |
| A rotor of a rotary internal combustion engine, including an annular oil seal assembly snugly received within each oil seal groove, each oil seal assembly including a seal ring retaining first and second axially spaced apart annular sealing elements in substantial radial alignment with one another, the seal ring radially pressing each of the sealing elements in sealing engagement with a respective surface in the groove in opposite directions from one another, and a spring member biasing the seal ring axially away from the end face. | ||||||
| 56 | Rotary internal combustion engine with oscillating pistons | US620507 | 1975-10-07 | US4024841A | 1977-05-24 | David B. Smith |
| This invention relates to an internal-combustion engine of generally spherical configuration having a generally spherical rotor mounted on a rotor shaft in a generally spherical shell. Combustion chambers are formed in appropriate recesses in the rotor and the inside of the spherical shell. The recesses are bounded by fixed partitions and movable pistons between the fixed partitions so that a series of combustion chambers are formed one on each side of each piston. The pistons are each connected to a central hub at the center of the rotor, and the hub is rotatable to a limited extent in a direction perpendicular to the rotor shaft. The pistons are therefore able to sweep through limited angular motion and during each motion increase the volume of one series of combustion chambers and decrease the volume of the other series of combustion chambers. A mechanical activating mechanism is provided so that the central hub is caused to rotate in a reciprocating manner through various angular positions that are predetermined in relation to the angular position of the rotor; in this manner the piston sweeping motion is precisely linked to the angular position of the rotor. Appropriate ports and ignition components are provided so that fuel and air can enter the various combustion chambers in proper sequence, be compressed, burned and exhausted also in proper sequence. | ||||||
| 57 | Fluid motor | US61651532 | 1932-06-10 | US1959152A | 1934-05-15 | BELMONT LEONARD L |
| 58 | ＩＤＡＲ－ＡＣＥ 역변위 비대칭 회전 교류 코어 엔진 | KR1020147028334 | 2013-03-13 | KR1020140138270A | 2014-12-03 | 앤더슨,윌리엄; 루카크직,트렌트; 루카크직,윌리엄 |
| 본 발명은 중심축(A)을 한정하는 회전식 샤프트를 포함하는 엔진들 또는 펌프들을 제공하고, 상기 샤프트는 제1 단부 및 제2 단부를 갖는다. 샤프트는 그 위에 배치된 제1 세장형 아일랜드를 가질 수 있다. 제1 아일랜드는 이격되는 전면 및 후면 표면들 사이에 대체로 한정된 부피를 갖는 바디를 가질 수 있다. 전면 및 후면 표면들은 방사축(R)에 평행한 평면에 놓일 수 있다. 전면 및 후면 표면들의 주변들은 그 사이의 굴곡진 주변 표면을 한정할 수 있다. 엔진 또는 펌프는 제1 아일랜드의 전면 표면에 인접하게 배치된 전방 측면 플레이트와, 제1 아일랜드의 후면 표면에 인접하게 배치된 후방 측면 플레이트를 더 포함한다. 엔진 또는 펌프는 또한 전방 측면 플레이트와 후방 측면 플레이트 사이에 배치된 제1 윤곽 조립체를 포함한다. | ||||||
| 59 | 자유 피스톤 가스터빈 엔진 | KR1020050012959 | 2005-02-17 | KR1020050029165A | 2005-03-24 | 김우균 |
| A free piston gas turbine engine is provided to produce a large quantity of high-temperature and high-pressure gas through ignition and explosion of fuel by successively executing reciprocation, suction, compression, explosion, and exhaust of four pistons attached to a circular ring. A free piston gas turbine engine has a circular body in which plural cylinders(4) are arranged and plural pistons(6) are attached to a circular ring(12) to execute reciprocation, suction, compression, explosion, and exhaust. Plural paths for exhaust are arranged to the circular ring. Exhaust gas is exhausted when fixed exhaust ports(8) attached to a moving ring accord with fixed exhaust rings(7) attached to a fixed exhaust ring(10). Simultaneous exhaust is executed from four spots toward the turbine. | ||||||
| 60 | Device for obtaining mechanical work from a non-thermal energy source (variants) | US15571126 | 2015-10-19 | US10125609B2 | 2018-11-13 | Igor Mykolaiovych Dubynskyi; Andrey Igorevich Dubinskiy |
| The invention relates to mechanical engineering. The present device for obtaining mechanical work from a non-thermal energy source comprises a cylindrical housing, a rotor, a vacuum chamber, movable elements, and systems for removal and supply of a working fluid. The rotor is provided with blades and is fastened to the power shaft, disposed inside the housing. The chamber is formed by the outside surface of the bladed rotor and the inside surface of the housing. The movable elements are mounted in diametric opposition inside the housing of the device and divide the chamber into equal parts. The shaft and blades of the rotor are hollow. The inlet ports and outlet ports are provided in surfaces of the rotor blades. Or outlet ports are provided in the housing. The technical result is an increase in the output, efficiency and environmental friendliness of the device, together with a simplified design. | ||||||
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