Invention Grant
- Patent Title: Rotorcraft tail boom, and a rotorcraft
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Application No.: US15318536Application Date: 2015-06-04
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Publication No.: US11001367B2Publication Date: 2021-05-11
- Inventor: Debbie Leusink , David Alfano
- Applicant: AIRBUS HELICOPTERS
- Applicant Address: FR Marignane
- Assignee: AIRBUS HELICOPTERS
- Current Assignee: AIRBUS HELICOPTERS
- Current Assignee Address: FR Marignane
- Agency: Brooks Kushman P.C.
- Priority: FR1401589 20140716
- International Application: PCT/EP2015/062519 WO 20150604
- International Announcement: WO2016/008639 WO 20160121
- Main IPC: B64C5/06
- IPC: B64C5/06 ; B64C23/00 ; B64C27/04 ; B64C5/02 ; B64C27/06 ; B64C27/82

Abstract:
A tail boom having a structure and a protuberance, the protuberance being secure with the structure. In each section of the tail boom, the protuberance extends in elevation over an extension height (Hext) and it extends laterally over an extension thickness (EPext), the extension height (Hext) lying in the range 0.05 times the maximum thickness (EPmax) of the structure, included, to 0.5 times the maximum thickness (EPmax), included, of the section, the extension thickness (EPext) lying in the range 0 to 0.4 times the maximum thickness (EPmax), included, of the section.
Public/Granted literature
- US20170121010A1 A ROTORCRAFT TAIL BOOM, AND A ROTORCRAFT Public/Granted day:2017-05-04
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