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141results about How to "Improve pressure distribution" patented technology

Shape memory spring driven hinder margin camber variable wing

The invention provides a wing with changeable trailing edge camber driven by a shape memory spring, relating to a wing with a changeable trailing edge camber, and aiming at the problems of traditional airplanes that a mechanism is complex and heavy, airflow breakaway is quite early and aerodynamic efficiency is low. The front end face and the back end face of an upper metal plate are fixedly connected with the front end faces of a connecting plate and the trailing edge; the front end face and the back end face of the lower metal plate are fixedly connected with the front end face of the connecting plate and the trailing edge; the same side surface of the upper metal plate and the lower metal plate are fixed with an upper prop stay and a lower prop stay; the two ends of a first shape memory spring are fixedly connected with a fixed plate and the upper metal plate; the two ends of a second shape memory spring are fixedly connected with the front end faces of the upper prop stay and the trailing edge; the two ends of a third shape memory spring are fixedly connected with the fixed plate and the lower metal plate; and the two ends of a fourth shape memory spring are fixedly connected with the front end faces of the lower prop stay and the trailing edge. The invention has the advantages of light weight, simple structure and high aerodynamic efficiency.
Owner:HARBIN INST OF TECH

Complex-hinge transformable trailing edge mechanism based on planar linkage closed-loop units

The invention provides a complex-hinge transformable trailing edge mechanism based on planar linkage closed-loop units. The complex-hinge transformable trailing edge mechanism comprises at least three closed-loop linkage units and a drive mechanism. Each closed-loop linkage unit is a planar linkage structure based on a 6R closed-loop unit and has one freedom degree. The closed-loop linkage units include a tail-end unit, at least one middle unit and a starting-end unit which are parallelly arranged, and the middle units are arranged between the starting-end unit and the tail-end unit. Compared with the prior art, the complex-hinge transformable trailing edge mechanism has the advantages that the basic units of the complex-hinge transformable trailing edge mechanism are independent 6R closed-loop units, the units influence on another, and the output of the previous unit is the input of the next unit; the whole mechanism contains few linkages and is lightweight; the freedom degree of the whole mechanism is 1, the mechanism can be driven by only one drive motor, the weight of the mechanism is reduced, system control difficulty is lowered, and the gradual bending effect of a transformable wing is good due to the fact that multiple basic unit modules are used.
Owner:HARBIN INST OF TECH SHENZHEN GRADUATE SCHOOL

Gas film pressure vector control device for aerostatic bearing

PendingCN110030266AControllable outlet pressureRealize vector controlHydrostatic bearingsControl vectorEngineering
The invention provides a gas film pressure vector control device for an aerostatic bearing. The control device comprises a main shaft and a bearing, wherein the bearing is arranged outside the main shaft, an air film is formed in a gap area between the main shaft and the bearing, and throttling holes are uniformly distributed in the bearing; an air chamber coat sleeves outside the bearing, a closed area formed between the air chamber coat and the bearing is the air chamber, and the throttling holes communicate the air film and the air chamber; a flow control valve is arranged on the wall surface of the air chamber coat opposite to the throttling holes in a penetrating mode, the flow control valve is coaxially arranged with the throttling holes, and the valve element of the flow control valve is used for adjusting the opening degree of the throttling holes; an air inlet hole penetrates through the wall surface of the air chamber coat and is externally connected with an air inlet pipe; awireless pressure sensor is arranged in a groove formed in the inner wall of the bearing, the shape, close to one side of the main shaft, of the wireless pressure sensor is consistent with the shapeof the inner wall surface of the bearing, and namely the wireless pressure sensor and the gas film flow field do not interfere with each other; the flow control valve is connected with a wire collecting terminal through a wire harness; the control device is connected with the wire collecting terminal through an anti-interference bus; and the vector control of the gas film pressure of the aerostatic bearing can be realized.
Owner:ZHEJIANG UNIV OF TECH

Vertical axis wind turbine blade module and synthesized jet control method thereof

The invention discloses a vertical axis wind turbine blade module and a synthesized jet control method thereof. The vertical axis wind turbine blade module is arranged on a base of a vertical axis wind turbine, and comprises multiple blade bodies, synthesized jet exciters and multiple jet holes, wherein the upper and lower ends of each blade body are fixed on a rotating shaft of the vertical axiswind turbine through fixed rod pieces; the synthesized jet exciters are uniformly and serially arranged in the blade bodies in the blade height directions of the blade bodies; the multiple jet holes are formed in the tail edges of the blade bodies; the synthesized jet exciters comprise shells, piezoelectric films, jet channels, piezoelectric drivers and control boxes, wherein the shells are squares, and are provided with upper openings and the lower openings; the piezoelectric films are squares, and cover the lower openings; the jet channels communicate with the upper openings; the piezoelectric drivers are arranged below the piezoelectric films, and are driven by rectangular pulse signals to generate a reverse piezoelectric effect so as to drive the square piezoelectric films to periodically vibrate up and down; and the control boxes are arranged above rotating shafts, are electrically connected with the piezoelectric drivers, and are used for inputting the rectangular pulse signals to the piezoelectric drivers.
Owner:UNIV OF SHANGHAI FOR SCI & TECH
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