Invention Grant
- Patent Title: Braided composite spar
-
Application No.: US14784959Application Date: 2014-04-17
-
Publication No.: US10023292B2Publication Date: 2018-07-17
- Inventor: Tony Fong , Timothy Axford
- Applicant: AIRBUS OPERATIONS LIMITED
- Applicant Address: GB Bristol
- Assignee: AIRBUS OPERATIONS LIMITED
- Current Assignee: AIRBUS OPERATIONS LIMITED
- Current Assignee Address: GB Bristol
- Agency: Hauptman Ham, LLP
- Priority: GB1307066.9 20130418
- International Application: PCT/GB2014/051227 WO 20140417
- International Announcement: WO2014/170691 WO 20141023
- Main IPC: B64C3/18
- IPC: B64C3/18 ; B64C23/06 ; B64F5/10 ; B29C70/22 ; B29C70/32 ; B29C70/30 ; B32B38/18 ; B29L31/30

Abstract:
A braided composite spar or preform for a braided composite spar, comprising a plurality of tubular plies of braided fibers, wherein the spar or preform has a center line which extends lengthwise from a root to a tip, and at least part of the center line follows a curved path which does not lie in a single plane. The spar or preform can be used to provide a tubular main spar for a winglet. The winglet also has a front spar with a front spar web, an upper front spar cap, and a lower front spar cap. An upper skin of the winglet is joined to the braided spar and the upper front spar cap. A lower skin of the winglet is joined to the braided spar and the lower front spar cap.
Public/Granted literature
- US20160075425A1 BRAIDED COMPOSITE SPAR Public/Granted day:2016-03-17
Information query