Invention Grant
US08408495B2 Fittings for attaching the vertical tail stabilizer of an aircraft
有权
用于安装飞机的垂直尾翼稳定器的配件
- Patent Title: Fittings for attaching the vertical tail stabilizer of an aircraft
- Patent Title (中): 用于安装飞机的垂直尾翼稳定器的配件
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Application No.: US12714333Application Date: 2010-02-26
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Publication No.: US08408495B2Publication Date: 2013-04-02
- Inventor: Diego Folch Cortés , Enrique Vera Villares , Javier Cabeza Huertas , José María Pina López , Elena Arévalo Rodríguez
- Applicant: Diego Folch Cortés , Enrique Vera Villares , Javier Cabeza Huertas , José María Pina López , Elena Arévalo Rodríguez
- Applicant Address: ES Madrid
- Assignee: Airbus Operations, S.L.
- Current Assignee: Airbus Operations, S.L.
- Current Assignee Address: ES Madrid
- Agency: Seed IP Law Group PLLC
- Priority: ES200901039 20090421
- Main IPC: B64C1/26
- IPC: B64C1/26

Abstract:
A fitting is provided to fix a vertical tail stabilizer of an aircraft to a composite skin and a composite frame of the aircraft in an area of a rear fuselage thereof. The fitting includes a first composite piece having lugs to attach to the vertical tail stabilizer and having vertical walls to fix the fitting to the composite frame of the rear fuselage. The fitting further includes at least one pair of additional composite pieces, each having a horizontal wall to fix the fitting to the composite skin of the rear fuselage. A second pair of additional composite pieces may be provided to further secure the fitting to the skin of the aircraft.
Public/Granted literature
- US20100264271A1 FITTINGS FOR ATTACHING THE VERTICAL TAIL STABILIZER OF AN AIRCRAFT Public/Granted day:2010-10-21
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