发明名称 Aircraft, has correction component made of shape memory alloy and exerting correction force between components such that components are transformed from fault position into normal position by changing correction force
摘要 <p>The aircraft has a component (12) i.e. engine nacelle, obtaining a preset normal position and a fault position relative to another component (10) i.e. wing, in a normal operation and a breakdown operation, respectively. A correction component (16) exerts correction force between the components such that the components are transformed from the fault position into the normal position by changing the correction force. The correction component is made of shape memory alloy. The correction force is adjusted by temperature of the correction component.</p>
申请公布号 DE102008063823(A1) 申请公布日期 2010.11.11
申请号 DE20081063823 申请日期 2008.12.19
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 HOMAN, STEFAN;NAGEL, BJOERN. DIPL.-ING.
分类号 B64C7/00;B64C3/00;B64D29/00 主分类号 B64C7/00
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