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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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