发明名称 Display retract mechanism
摘要 A display retract mechanism for moving a display between a retracted position and a deployed position is disclosed and explained. The display retract mechanism is useful, for example, in mounting a liquid crystal display within the cabin of a passenger vehicle, such as an aircraft or bus. A geared chain drive supplies torque necessary for rotating a pivot shaft on which the display is attached. The display is biased toward a retracted position by a gas spring with a substantially linear force curve between the retracted position and the deployed position. Also disclosed are an infrared sensor for detecting when the display is in the deployed position, a solenoid latch for holding the display in the retracted position, and an electromechanical clutch for maintaining the display in a particular position.
申请公布号 US2004075639(A1) 申请公布日期 2004.04.22
申请号 US20020273237 申请日期 2002.10.17
申请人 THALES AVIONICS IN-FLIGHT SYSTEMS, LLC 发明人 LESTER GERALD E.;FOREMAN BRADLEY;MIRAND MAURICIO J.;MCQUAID DORIS
分类号 B60R11/00;B60R11/02;B64D11/00;G06F1/16;G09F;G09G5/00;H04N5/645;(IPC1-7):G09G5/00 主分类号 B60R11/00
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