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74results about How to "Highly miniaturized" patented technology

Minimally invasive transvalvular ventricular assist device

A tiny electrically powered hydrodynamic blood pump is disclosed which occupies one third of the aortic or pulmonary valve position, and pumps directly from the left ventricle to the aorta or from the right ventricle to the pulmonary artery. The device is configured to exactly match or approximate the space of one leaflet and sinus of valsalva, with part of the device supported in the outflow tract of the ventricular cavity adjacent to the valve. In the configuration used, two leaflets of the natural tri-leaflet valve remain functional and the pump resides where the third leaflet had been. When implanted, the outer surface of the device includes two faces against which the two valve leaflets seal when closed. To obtain the best valve function, the shape of these faces may be custom fabricated to match the individual patient's valve geometry based on high resolution three dimensional CT or MRI images. Another embodiment of the invention discloses a combined two leaflet tissue valve with the miniature blood pump supported in the position usually occupied by the third leaflet. Either stented or un-stented tissue valves may be used. This structure preserves two thirds of the valve annulus area for ejection of blood by the natural ventricle, with excellent washing of the aortic root and interface of the blood pump to the heart. In the aortic position, the blood pump is positioned in the non-coronary cusp. A major advantage of the transvalvular VAD is the elimination of both the inflow and outflow cannulae usually required with heart assist devices.
Owner:JARVIK ROBERT

Minimally invasive transvalvular ventricular assist device

A tiny electrically powered hydrodynamic blood pump is disclosed which occupies one third of the aortic or pulmonary valve position, and pumps directly from the left ventricle to the aorta or from the right ventricle to the pulmonary artery. The device is configured to exactly match or approximate the space of one leaflet and sinus of valsalva, with part of the device supported in the outflow tract of the ventricular cavity adjacent to the valve. In the configuration used, two leaflets of the natural tri-leaflet valve remain functional and the pump resides where the third leaflet had been. When implanted, the outer surface of the device includes two faces against which the two valve leaflets seal when closed. To obtain the best valve function, the shape of these faces may be custom fabricated to match the individual patient's valve geometry based on high resolution three dimensional CT or MRI images. Another embodiment of the invention discloses a combined two leaflet tissue valve with the miniature blood pump supported in the position usually occupied by the third leaflet. Either stented or un-stented tissue valves may be used. This structure preserves two thirds of the valve annulus area for ejection of blood by the natural ventricle, with excellent washing of the aortic root and interface of the blood pump to the heart. In the aortic position, the blood pump is positioned in the non-coronary cusp. A major advantage of the transvalvular VAD is the elimination of both the inflow and outflow cannulae usually required with heart assist devices.
Owner:JARVIK ROBERT

Engine start device of a rotary valve carburetor

A compact engine start device of a combustion engine rotary-type carburetor overrides normal operation of a rotary throttle valve to provide a richer mixture of fuel-and-air to start a cold engine. Rotation of a start lever of the start device activates a releasable camming interface coupler causing the throttle lever to rotate about a rotary axis and axially lift partially out of the carburetor at prescribed angular and axial distances. This provides the engine, through a fuel-and-air mixing passage, with a controlled and enriched ratio and volume of a fuel-and-air mixture. Preferably, the start lever has a projecting rod that inserts into a hole in the carburetor body for rotation about an axis orientated substantially parallel to the rotary axis. An outward surface of the start lever is in rotational sliding contact with a low-profile, preferably cantilevered, retention arm preferably formed unitarily to a metering fuel pump cover engaged removably to the body of the carburetor, thus allowing rotational movement but preventing axial movement of the start lever. Because the start lever does not move axially to displace the rotary throttle valve, the height of the start lever is favorably minimized. Moreover, the start lever preferably has a knob for user interface at a distal end of the lever that conforms generally about the retention arm thus maximizing knob size yet not contributing to an increase in carburetor size.
Owner:WALBRO ENGINE MANAGEMENT

Bevel gear-double cycloid speed reduction device for rocket launching movable platform

The invention relates to the technical field of speed reducers, in particular to a bevel gear-double cycloid speed reduction device for a rocket launching movable platform. The device is a two-stage speed reduction device characterized by comprising a bevel gear pair and double-cycloid transmission, wherein (A) the cycloid transmission comprises a base, an output shaft, support bearings, a cycloid wheel, an eccentric bearing, an inner cycloid gear ring, a front base, an input shaft and a W output mechanism, the input shaft is supported in an inner hole of the front base through a bearing, the shaft extension end is connected with the eccentric bearing, and the input end is connected with a big bevel gear; the front base is integrated with the inner cycloid gear ring and the base in sequence; the output shaft is supported in the inner hole of the base through a bearing; and (B) two symmetrically installed small bevel gear shafts engaged with the big bevel gear are supported in wall holes of a front base box through bearings, and the small bevel gear shafts are connected with a motor; and another small bevel gear shaft is connected with a manual handle. The invention has the advantages of two-stage speed reduction, small axial size, light weight and high-degree lightweight; cycloid gear teeth are uninterrupted, so that the bearing capacity is greater than that of planet transmission with only four planet wheels; and the cost is low and is reduced to 40-55%.
Owner:吴声震

Circuit of the electronic ballast with the capability of automatic restart

This present invention discloses a circuit of the electronic ballast with the capability of automatic restart. It includes a rectifier circuit, a trigger circuit of automatic restart, a DC/AC convertor, a output circuit of the lamp, and a circuit of abnormal protection. Its main feature is that there is a discharge loop in the trigger circuit, so it can realize automatic restart only after changing the lamp tube or connecting the lamp pin without turning off the power source when the lamp tube is abnormal and enters into protecting condition or any of the lamp pins is in poor contact. Because the trigger recourse Vt is led out from the lamp loop, when the power source is switched on, the DC/AC convertor is triggered to start after insuring good contact between the lamp tube and the lamp holder, accordingly realizes the self-check function of the connection for the lamp tube. Furthermore, because primary side winding Ta of oscillating coil T of the present invention is connected in series between the lamp pin P1 and the common end of feed-through capacitor C4 and by-pass capacitor C6, the primary side winding Ta of oscillating coil T will disconnect the power source when the lamp is in open circuit or any of the lamp pins is in poor contact. Therefore, the circuit will not come into protecting condition despite the by-pass capacitor C6, which results in the simplification of the task program.
Owner:DONGYANG TOSPO LIGHTING

Cycloid speed-reducing device of rocket launching movable platform

The invention relates to the technical field of speed reducers, in particular to a cycloid speed-reducing device of a rocket launching movable platform, which is characterized in that the cycloid speed-reducing device is a two-stage speed-reducing device comprising a bevel gear pair and a cycloid transmission, wherein (A) the cycloid transmission comprises a base, an output shaft, a supporting bearing, a cycloid gear, an eccentric bearing, a needle-tooth shell, a needle-tooth pin, a front base, an input shaft and an W output mechanism, wherein an input shaft is supported on an inner hole of the front base by bearings, the shaft-extension end of the input shaft is connected with the eccentric bearing, and the input end is connected with a large bevel gear; the front stand is sequentially connected with the needle-tooth shell and the base; the output shaft is supported on the inner hole of the base by the bearings; and (B) two symmetrical small bevel gear shafts meshed with the large bevel gear are both supported in a box wall hole of the front base by the bearings, wherein one small bevel gear shaft is connected with a motor, and the other small bevel gear shaft is connected with amanually-operated handle. The cycloid speed-reducing device has the advantages of two-stage speed reduction, short axial size, light weight and high quantization; in addition, as cycloid gear teeth and semi-buried teeth are continuous, the cycloid speed-reducing device has larger bearing capacity than that of a planetary transmission with only four planet gears; moreover, the cost of the cycloid speed-reducing device is lowered by 40%-55%.
Owner:郑雪霞

High-torque cycloidal speed-reduction device of rocket launching moving platform

The invention relates to the technical field of a speed reducer, in particular to a high-torque cycloidal speed-reduction device of a rocket launching moving platform. The high-torque cycloidal speed-reduction device of the rocket launching moving platform is characterized in that: a two-stage speed-reduction device is formed through cycloidal transmission of a bevel gear pair and three cycloidal wheels, wherein, (A) the cycloidal transmission is constituted by a base, an output shaft, a supporting bearing, three cycloidal wheels with 120 degrees of phase angles, an eccentric bearing, a pin gear housing, a gear pin, a front base, an input shaft and a W-shaped output mechanism, wherein the input shaft is supported in an inner hole of the front base by a bearing, the shaft extension end of the input shaft is connected with the eccentric bearing, and the input end is connected with a bevel gear wheel; the front base is sequentially integrated with the pin gear housing and the base; and the output shaft is supported in the inner hole of the base by a bearing; and (B) two systematical bevel pinion shafts which are meshed with the bevel gear wheel are supported in a box wall hole of the front base by a bearing, and one bevel pinion shaft is connected with a motor and the other bevel pinion shaft is connected with a manual handle. The high-torque cycloidal speed-reduction device of the rocket launching moving platform has the beneficial effects that: (a) two-stage reduction is adopted, the axial size is short, the weight is small and the height is lightened; (b) cycloidal gear teeth and half-buried teeth are not broken, and three cycloidal wheels are adopted, therefore, the bearing capacity of three cycloidal wheels is higher than that of epicyclic transmission of four planet wheels; and (c) the cost is reduced by 40-55 percent.
Owner:吴声震
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