| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | Gas turbine engine system | US10570017 | 2004-08-30 | US07621116B2 | 2009-11-24 | Haim Rom; Guy Rom |
| An engine system comprises a first transfer positive displacement, volumetric device, at least one second positive displacement, volumetric device, and a transmission in engagement with two adjacent volumetric devices. The transmission has a ratio designed to cause the at least one second volumetric device to rotate at a higher angular velocity than the first volumetric device, inducing expansion of a compressible fluid during continuous flow from the first volumetric device to the at least one second volumetric device while performing work. | ||||||
| 82 | Piston Valve Internal Combustion Engine | US12100420 | 2008-04-10 | US20090255507A1 | 2009-10-15 | Craig Louis Althen |
| An internal combustion engine of two perpendicular, toroidal cylinders intersecting at two junctions with each cylinder containing one piston filling half of its volume. The pistons are 180 degrees out of phase; each alternately occluding one intersection or the other. Each piston completes a full power, exhaust, intake, and compression stroke in one revolution. Endplates of 45 degrees allow the combustion chamber junction to be permanently filled and sealed at all times; first by one piston, then by the tips of both pistons as the complementary-angled endplates tangentially slide past one another, and then by the other piston. Compressed gases are shunted into the crossing cylinder's combustion chamber. Both pistons orbit continuously, one-way. Airflow is also one-way. Each piston is mounted to a sealed, 360-degree, counterbalanced ring gear. One ring gear is positioned centrally and the other peripherally to prevent interference. These maintain coordination between the pistons and provide output. | ||||||
| 83 | PROGRESSIVE CAVITY APPARATUS WITH TRANSDUCER AND METHODS OF FORMING AND USE | US11967941 | 2007-12-31 | US20090169364A1 | 2009-07-02 | Geoff Downton |
| The present invention relates to a stator (100-1000) with a profiled helical bore (106,206,306,606,706,806,906,1006) having a cast material layer (102;202;302;602;702;802;902;1002) with transducers (104A-104D;304;604A-604D;710;804;904A-904C;1010) disposed therein and describes the methods of forming such stators. Cast material can be fluidic during displacing of a transducer therein. Cast material layer 202 can include housings (218,222) disposed therein and/or a cavity 226 formed therein. Transducer can be a sensor (104A-104C) and/or an actuator 104D. Transducer 804 can extend axially along a length of the stator 800. Transducer or plurality of transducers (904A-904C) can extend along a helical path. Additionally or alternatively, sleeve 1008 can include a transducer 1010. | ||||||
| 84 | Free Swinging Piston Heat Machine | US11913482 | 2006-04-24 | US20080178847A1 | 2008-07-31 | Sigitas Kudarauskas; Leonas Antanas Kucinskas |
| The invention relates to positive-displacement free-piston heat machines with variable working chambers, which could be applied as an internal or external combustion engine, compressor, pump. The machine comprises two analogous assemblies of pistons, each consisting of two or more vanes having form of symmetrical star and attached to the hub. The assemblies of pistons are placed in the cylindrical cavity that is limited by two concentric cylindrical surfaces and two planes at the ends. The vanes the different assemblies are alternately displaced in the cavity. When the assemblies of pistons swing in opposite directions, variable working chambers are got between the adjacent vanes. The external loading or driving devices are connected directly to the assemblies of pistons either by coaxial shafts, radial junctions, planar or cylindrical rings. The machine with two bodies swinging in opposite direction presents well-balanced mechanical system, and vibration of the frame is avoided. | ||||||
| 85 | Rotary piston machine with an oval rotary piston | US11544461 | 2006-10-06 | US20070089701A1 | 2007-04-26 | Boris Schapiro |
| An internal combustion engine having at least one working chamber limited by a piston and means for fuel injection, wherein said fuel injection means are arranged in a separate ignition chamber communicating with said working chamber, and means for tuning said ignition chamber and fuel injected by said fuel injection means such that substantially only burnt, expanding combustion gas enters the working chamber. | ||||||
| 86 | Gas turbine engine system | US10570017 | 2004-08-30 | US20070051087A1 | 2007-03-08 | Haim Rom; Guy Rom |
| An engine system is disclosed which comprises a first volumetric device, at least one second volumetric device, and a transmission in engagement with two adjacent volumetric devices. The transmission has a ratio designed to cause the at least one second volumetric device to rotate at a higher angular velocity than the first volumetric device, inducing expansion of a compressible fluid during continuous flow from the first volumetric device to the at least one second volumetric device while performing work. | ||||||
| 87 | Gerotor apparatus for a quasi-isothermal Brayton cycle Engine | US10359487 | 2003-07-25 | US07186101B2 | 2007-03-06 | Mark T. Holtzapple; George A. Rabroker |
| According to one embodiment of the invention, a gerotor apparatus includes an outer gerotor having an outer gerotor chamber, an inner gerotor, at least a portion of which is disposed within the outer gerotor chamber, and a synchronizing apparatus operable to control the rotation of the inner gerotor relative to the outer gerotor. The inner gerotor includes one or more entrance passages operable to communicate a lubricant into the outer gerotor chamber. | ||||||
| 88 | Gerotor apparatus for a quasi-isothermal Brayton cycle engine | US11369202 | 2006-03-06 | US20060239849A1 | 2006-10-26 | Mark Heltzapple; George Rabroker; Thomas Beck; Mark Ehsani; Matthew Whiteacre; Michael Ross; Gary Noyes |
| According to one embodiment of the invention, a gerotor apparatus includes an outer gerotor having an outer gerotor chamber, an inner gerotor, at least a portion of which is disposed within the outer gerotor chamber, and a synchronizing apparatus operable to control the rotation of the inner gerotor relative to the outer gerotor. The inner gerotor includes one or more entrance passages operable to communicate a lubricant into the outer gerotor chamber. | ||||||
| 89 | Drive shaft coupling device | US10653422 | 2003-09-03 | US07040276B2 | 2006-05-09 | Tadaaki Makino; Katsumi Mori; Katsunori Furuta |
| An oil supply means is provided to supply the center portion of a rotating part of an Oldham coupling with oil. The oil spreads from the center of rotation to the outside of the Oldham coupling and makes it possible to prevent the Oldham coupling from wearing. A recess is also provided to direct the oil supplied from an engine to the inward portion of the Oldham coupling. Accordingly, the oil is supplied all over an Oldham projection so that it is possible to prevent the frictional wearing of the Oldham projection disposed inside the Oldham coupling. | ||||||
| 90 | Turbostatic compressor, pump, turbine and hydraulic motor and method of its operation | US10977664 | 2004-10-28 | US20050260092A1 | 2005-11-24 | Stephen Bolger |
| A variable-volume positive-displacement device configured to accommodate large flow volumes is disclosed. The variable-volume positive-displacement device despite being compact and lightweight, maintains pressure ratios of over 10 to 1 in a single stage operation. There is little loss of working fluid leakage, due to optimum sealing configurations and extremely low-seal sliding speeds. The device comprises a housing defining a closed chamber within opposing walls and a displacer mounted within the housing. The displacer maintains sliding contact with each of the inner wall surfaces of the chamber as it orbits and engages each of the inner wall surfaces in sequence. The volumes of the chambers surrounding the displacer vary as the displacer moves, depending on the position of the displacer. Working fluid is introduced into the chamber via inlet ports or is discharged via an outlet. This device may be used to replace conventional piston pumps, rotary pumps, scroll pumps, screw pumps, roots blowers, gear pumps and wankel displacers for pumping gases and liquids in applications requiring reduced frictional losses and tight sealing and relatively large displacement in a small volume. With integral valve-operators, the inventive device replaces turbines used for expansion of gases with large pressure ratios. This invention is particularly useful for constructing Brayton cycle engines and refrigerators. The inventive device offers improved operation and functional characteristics and lower cost of manufacture. | ||||||
| 91 | Fluid machine | US10827246 | 2004-04-20 | US20040211180A1 | 2004-10-28 | Shigeru Hisanaga; Yasushi Yamanaka |
| A fluid machine for a waste heat collecting system for an internal combustion engine has an object to make most use of the collected waste heat and an operation of a compressor, an alternator or the like by a rotational driving force from an expansion device function well even during an engine running is stopped. The fluid machine according to the present invention has a pulley connected to the engine, an expansion device for generating a rotational driving force from the collected waste heat, a compressor device driven by the pulley and the expansion device, wherein a rotating shaft is commonly used for the pulley, the expansion device and the compressor device. The expansion device is an expansion device for changing its expansion volume, so that the Rankine cycle for collecting the waste heat can be operated most effectively. | ||||||
| 92 | Drive shaft coupling device | US10653422 | 2003-09-03 | US20040074468A1 | 2004-04-22 | Tadaaki Makino; Katsumi Mori; Katsunori Furuta |
| An oil supply means is provided to supply the center portion of a rotating part of an Oldham coupling with oil. The oil spreads from the center of rotation to the outside of the Oldham coupling and makes it possible to prevent the Oldham coupling from wearing. A recess is also provided to direct the oil supplied from an engine to the inward portion of the Oldham coupling. Accordingly, the oil is supplied all over an Oldham projection so that it is possible to prevent the frictional wearing of the Oldham projection disposed inside the Oldham coupling. | ||||||
| 93 | Two-stage rotary vane motor | US139184 | 1998-08-25 | US6086347A | 2000-07-11 | Antonin Ryska; Jiri Ota; Herman H. Viegas; Bruce E. McClellan |
| A two-stage rotary vane motor is provided that is particularly efficient for use in cryogenic refrigeration systems where the mass flow rate of the drive fluid (which may be expanding cryogen gas) varies substantially. The two-stage rotary vane motor includes a housing enclosure having first and second fluid chambers, each with their own inlets for receiving pressurized cryogen, and first and second rotors rotatably mounted within the chambers by means of a shaft assembly having an output end. In operation, when the mass flow of the drive fluid is high (350 pounds per hour), fluid is admitted through the inlets of both the chambers of the housing enclosure to drive both of the rotors. However, when the mass flow of the drive fluid drops to a low level (i.e., 100 pounds per hour), expanding cryogen is admitted only through the second chamber of the housing enclosure to drive only the second rotor. An overrunning clutch may be used to engage and disengage the first rotor from the shaft assembly in coordination with the admission of drive fluid through both or only one of the housing inlets. | ||||||
| 94 | Vane motor with brake | US981948 | 1998-01-02 | US6077061A | 2000-06-20 | Dieter Peters; Peter Krebs |
| A vane motor comprises a casing and a vane rotor being mounted in the casing. A friction brake device is arranged in the casing and it is intended for braking, stopping and releasing the vane rotor. At least one of the two end faces of the vane rotor is part of the brake device and forms a friction pair with a braking surface of a brake element of the brake device. The brake element is arranged next to the said end face of the vane rotor and is axially movable upon actuation of the friction brake device for braking, stopping and releasing the vane rotor. | ||||||
| 95 | Nutating positive displacement device having a magnetic element wire sensing arm | US113019 | 1993-08-30 | US5385457A | 1995-01-31 | John E. Durand |
| A positive displacement device is presented. The mechanism comprises a nutator capable of nutating within a nutating chamber defined by the interior surface of the body of the positive displacement device between an inlet into and an outlet out of the positive displacement device, an inverted pendulous, low friction, substantially non-sliding nutator, vertically elongated double pivoting fulcrum; a magnetic signal pickup mechanism comprising a pivoting cruciform shaped magnet element low inertia wire magnetically tracking a nutator and a means of sensing movement; a third magnetic element to dampen or amplify movement of the cruciform wire; a balance plate bearing on the basic elements of the positive displacement device by means of a resilient spring force; and static elements which provide magnetic attraction to the moving elements effecting a sealing influence between the static and moving elements. | ||||||
| 96 | Rotor for fluidic apparatus | US401641 | 1989-09-05 | US4971536A | 1990-11-20 | Toshio Takeda; Yoshiharu Okochi |
| A rotor for fluidic apparatus such as, blowers, compressors, fluidic motors and vacuum pumps includes a drive shaft having concaved portions on its periphery and a rotatable member cast around the concaved portions of the drive shaft. The rotor according to the present invention is manufactured through the steps of forming the drive shaft, disposing the formed drive shaft into the cavity of a molding die, and then pouring the molten metal into the cavity while disposing the drive shaft therein. The resulted rotor has no play in the direction of its rotation of its rotatable member. | ||||||
| 97 | Scroll type fluid displacement apparatus with balanced drive means | US244961 | 1981-03-18 | US4824346A | 1989-04-25 | Masaharu Hiraga; Kiyoshi Terauchi; Kiyosh Miyazawa; Seiichi Sakamoto |
| A scroll-type fluid displacement apparatus, in particular, a compressor unit is disclosed. The unit includes a housing with a fluid inlet port and a fluid outlet port. A fixed scroll with first end plate and first spiral element is fixedly disposed in the housing. An orbiting scroll with a second end plate and a second spiral element is disposed for orbiting motion in the housing. The first and second spiral elements interfit with one another at an angular offset to make a plurality of line contacts to define at least one pair of sealed off fluid pockets. A drive pin extends from an inner end of a drive shaft. The orbiting scroll has a boss which rotatably supports a bushing. An eccentric hole is formed in the bushing and the drive pin is received within this hole. The center of the drive pin is located on an opposite side to the center of the drive shaft with regard to a straight line, which passes through the center of the bushing and is perpendicular to a connecting line passing through the center of the drive shaft and the center of the bushing. The center of the drive pin also is beyond the connecting line in the direction of rotation of the drive shaft. The bushing has a balance weight for cancelling a centrifugal force which arises because of the orbiting motion of the scroll member and bushing. Dynamic balance is accomplished by the use of a pair of balance weights affixed to the drive shaft for generating a moment of the same amount, but opposite in direction, to the moment generated by a force due to the interaction of the centrifugal force of the orbiting parts and the first balance weight. | ||||||
| 98 | Rolling cylinder engine system | US137959 | 1987-12-23 | US4776777A | 1988-10-11 | George D. Doty |
| An engine for rotating an output shaft includes a housing which defines an inner cylindrical surface coaxial with the output shaft. A roller member is disposed within the housing and includes an inner cylindrical bearing surface and an outer cylindrical surface spaced from the inner surface of the housing. Longitudinal axis of the rolling member is radially offset from the axis of the housing and the shaft. A mechanism is provided for preventing relative rotation and movement between the housing and the rolling member, and a plurality of chambers are defined between the housing and the rolling member. Devices are provided for selectively introducing expansive gas or fluid into the chamber in rotationally sequential fashion, and devices are further provided for exhausting expanding gas or fluid from the chambers in rotationally sequential fashion to urge the roller member away from the housing and expand the chambers at the site of the expansive gas or fluid introduction. This rolls the roller member about the inner cylindrical surface of the housing with the axis of the roller member rolling about the central axis of the housing and shaft. Finally, a mechanism is provided for rotating the shaft in response to the rolling movement of the roller member within the housing. | ||||||
| 99 | Scroll-type fluid transferring machine with loose drive fit in crank shaft recess | US842235 | 1986-03-21 | US4715796A | 1987-12-29 | Tsutomu Inaba; Tadashi Kimura; Norihide Kobayashi; Masahiro Sugihara; Tetsuzo Matsugi |
| A scroll-type fluid transferring machine comprises a stationary scroll member and an oscillatable scroll member, each of which has a spiral wrap of an involute curve or other curves projecting from a base plate and which cooperate to form a compression chamber between the spiral wraps and the base plates by mutually fitting one into the other, an oscillatable scroll shaft provided on the surface of the base plate at the position opposite the spiral wrap of the oscillatable scroll member, a crank shaft having an eccentric recess having its axis which is shifted by a predetermined distance from the axis of the crank shaft, wherein a cylindrical bush having the coaxial outer and inner circles is loosely fitted in the eccentric recess of the crank shaft with a gap between the outer circumference of the bush and the inner wall of said eccentric recess, and the shaft of the oscillatable scroll member is fitted in the inner circumference of the bush in a freely rotatable manner. | ||||||
| 100 | Method of manufacturing a rotor | US812610 | 1985-12-23 | US4680844A | 1987-07-21 | James W. Rupp |
| A method of manufacturing a rotor (70) for use in an air motor. A shaft (10) is machined to have bearing surfaces (16 and 18) and adjacent ends (12 and 14), respectively. A working surface (20) with helix grooves (22, 24 and 26) is machined into the shaft (10). A locking surface (34) is machined into the shaft between the working surface (20) and end (14). A ring (36) is machined with helix grooves (38, 40 and 42) on its periphery and an inner diameter (44). The inner diameter has a diameter less than the locking surface (34) but greater than the bearing surface (18). The ring (36) is placed on bearing surface (18) of shaft (10). The shaft (10) with ring (36) on bearing surface (18) is placed in a fixture (50) and a tension force is applied to ends (12) and 14 ). The tension force causes the shaft (10) to axially expand and radially contract. When the diameter of the locking surface (34) is approximately equal to the diameter (44) of the ring (36), the ring (36) is pushed into contact with the working surface (20). After the helix grooves (22, 24, 26) are aligned with helix grooves (38, 40 and 42), the tension force is released allowing the locking surface to expand and frictionally hold the shaft (10) and ring (36) together such that a herringbone pattern is formed for rotor (70). | ||||||
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