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.
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
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