发明名称 |
SUSPENSION STRUCTURE WITH VARIABLE GEOMETRY OF A TURBOPROP ENGINE ON A STRUCTURAL ELEMENT OF AN AIRCRAFT |
摘要 |
<p>The invention concerns a suspension structure (100) with variable geometry of a turboprop engine (4) on a structural element of an aircraft, comprising a rear cradle (102) intended to be attached to a structural element of an aircraft and a front cradle (104) intended to support a front portion of the turboprop engine, the front cradle being linked to the rear cradle by a pivot link (116) capable of allowing the front cradle to tilt vertically relative to the rear cradle, and by a return spring (120) capable of preventing the front cradle from tilting when the thrust of the turboprop engine is below a predefined threshold.</p> |
申请公布号 |
WO2014111654(A1) |
申请公布日期 |
2014.07.24 |
申请号 |
WO2014FR50072 |
申请日期 |
2014.01.15 |
申请人 |
SNECMA |
发明人 |
HELLEGOUARCH, ANTOINE;POISSON, MATHIEU, ANGE;GALLET, FRANÇOIS |
分类号 |
B64D27/26 |
主分类号 |
B64D27/26 |
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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