The present disclosure discloses a device and a method for converting reciprocating motion into continuous rotation, and application includes: a central shaft and rotating discs, each rotating disc is connected to the central shaft through a bearing, the rotating disc is arranged concentrically with the bearing, wings are arranged on a circumference of rotating disc, upper wing surfaces of the wings are of convex structures. According to the device for converting reciprocating motion into continuous rotation of the present disclosure, the rotating directions of the wings can be kept unchanged all the time during the reciprocating motion of the device by using airfoil structures of the wings in the device and limiting mounting angles of the wings, so as to obtain a continuous lifting force with a constant direction.

The present disclosure discloses a device and a method for converting reciprocating motion into continuous rotation, and application includes: a central shaft and rotating discs, each rotating disc is connected to the central shaft through a bearing, the rotating disc is arranged concentrically with the bearing, wings are arranged on a circumference of rotating disc, upper wing surfaces of the wings are of convex structures. According to the device for converting reciprocating motion into continuous rotation of the present disclosure, the rotating directions of the wings can be kept unchanged all the time during the reciprocating motion of the device by using airfoil structures of the wings in the device and limiting mounting angles of the wings, so as to obtain a continuous lifting force with a constant direction.

A method for pressure and temperature control of fluid in a series of cryogenic compressors. An actual speed for each compressor and an actual inlet pressure and actual inlet temperature at entry are determined. The maximum speed for each compressor and a desired inlet pressure for the first compressor is provided. A speed index for each compressor is determined from the maximum speed and actual speed of each compressor. A proportional value is determined from the deviation of the actual and desired inlet pressure. A priority value is determined from the smaller of the proportional value and the smallest speed index. A desired inlet temperature for the first compressor and a desired speed for each compressor are determined from the priority value. The actual inlet temperature is adjusted to the determined desired inlet temperature and the actual speed for each compressor is adjusted to the determined desired speed.

A method for pressure and temperature control of fluid in a series of cryogenic compressors. An actual speed for each compressor and an actual inlet pressure and actual inlet temperature at entry are determined. The maximum speed for each compressor and a desired inlet pressure for the first compressor is provided. A speed index for each compressor is determined from the maximum speed and actual speed of each compressor. A proportional value is determined from the deviation of the actual and desired inlet pressure. A priority value is determined from the smaller of the proportional value and the smallest speed index. A desired inlet temperature for the first compressor and a desired speed for each compressor are determined from the priority value. The actual inlet temperature is adjusted to the determined desired inlet temperature and the actual speed for each compressor is adjusted to the determined desired speed.

An evaporated fuel processing device includes a fuel tank, a canister, an atmospheric passage, a vapor passage, an intake pipe, a purge passage, a purge pump, and a flow rate control valve. The evaporated fuel is desorbed utilizing only negative pressure in the intake pipe when sufficient negative pressure is generated in the intake pipe. The purge pump is driven to desorb the evaporated from the canister when sufficient negative pressure is not generated in the intake pipe. The purge pump and the flow rate control valve may be provided in the purge passage. The purge pump is a vortex pump through which the gas can flow even when drive is stopped. The minimum cross-sectional area of the internal space of the flow passage of the purge pump is equal to or larger than the minimum cross-sectional area of the internal space of the other parts of the purge passage.

Methods, systems, and apparatus, including a housing defining a top surface, a bottom surface, and first and second side surfaces. Also included is a first rail extending from the first side surface and a second rail extending from the second surface such that when the first and second rails are slidably engaged with a third surface. A blower device is included that is axially disposed between the top and bottom surface, wherein a first end of the housing defines a first plenum outlet, the top surface defines a plenum inlet, the bottom surface defines a second plenum outlet that is positioned on a second side of the blower device and that fluidly couples the first plenum chamber to the second plenum chamber. Further, the second plenum chamber is formed by the first and second rails, the bottom surface and the third surface has a third plenum outlet.

Methods, systems, and apparatus, including a housing defining a top surface, a bottom surface, and first and second side surfaces. Also included is a first rail extending from the first side surface and a second rail extending from the second surface such that when the first and second rails are slidably engaged with a third surface. A blower device is included that is axially disposed between the top and bottom surface, wherein a first end of the housing defines a first plenum outlet, the top surface defines a plenum inlet, the bottom surface defines a second plenum outlet that is positioned on a second side of the blower device and that fluidly couples the first plenum chamber to the second plenum chamber. Further, the second plenum chamber is formed by the first and second rails, the bottom surface and the third surface has a third plenum outlet.

A method and load wrapping apparatus in some instances may utilize a flow stabilized high speed axial fan blower to direct a flow of fluid towards a packaging material tail to assist in adhering a packaging material tail to the side of a load at the completion of a wrapping operation.

A method and load wrapping may utilize a flow device disposed downstream of a wrap position at which the load is wrapped to direct a flow of fluid towards a packaging material tail to increase adherence of the packaging material tail to the side of a load after the load has been wrapped and conveyed away from the wrap position.

A fan control system includes a control module, a first fan module and a second fan module. The control module provides a first control signal to the first fan module to adjust the rotation state of the first fan module. The first fan module provides a second control signal to the second fan module based on the first control signal to adjust the second fan module. The first fan module includes a first terminal and a second terminal. The second fan module includes a first terminal and a second terminal. The first terminal of the first fan module is electrically connected to the control module to receive the first control signal. The second terminal of the first fan module is electrically connected to the first terminal of the second fan module. The second terminal of the second fan module is electrically connected to a reference voltage.