发明名称 |
CONFIGURATION OF A REAR FUSELAGE TAIL CONE OF AN AIRCRAFT WITH AN AUXILIARY POWER UNIT |
摘要 |
Configuration of a rear fuselage tail cone of an aircraft with an auxiliary power unit, whereby a fire compartment of the rear fuselage tail cone defines a housing for the auxiliary power unit in which the auxiliary power unit is housed laterally and asymmetrically with respect to a longitudinal axis (X) of the rear fuselage tail cone and the auxiliary power unit is directly fasten attached to a structural skin wall of the housing. Additionally, by struts or rods attached to opposite side and upper structural skin wall of the fire compartment.
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申请公布号 |
US2011259998(A1) |
申请公布日期 |
2011.10.27 |
申请号 |
US201113091185 |
申请日期 |
2011.04.21 |
申请人 |
SANZ MARTINEZ PABLO TIMOTEO |
发明人 |
SANZ MARTINEZ PABLO TIMOTEO |
分类号 |
B64D27/00;B23P11/00;B64C1/10;B64D41/00 |
主分类号 |
B64D27/00 |
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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