Invention Grant
- Patent Title: Airframe wing spar structures with contiguous unitary and integrally fastened upper and lower chord sections
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Application No.: US14791647Application Date: 2015-07-06
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Publication No.: US09656738B2Publication Date: 2017-05-23
- Inventor: Yvan Bovolenta Murta , Renato Campos da Silveira , Clovis Augusto Eça Ferreira , Wanderley Montoro
- Applicant: EMBRAER S.A.
- Applicant Address: BR São José Dos Campos-SP
- Assignee: EMBRAER S.A.
- Current Assignee: EMBRAER S.A.
- Current Assignee Address: BR São José Dos Campos-SP
- Agency: Nixon & Vanderhye P.C.
- Main IPC: B64C3/18
- IPC: B64C3/18

Abstract:
An aircraft wing is provided having a spanwise wing spar which includes a one-piece upright central web extending in a spanwise direction between inboard and outboard ends of the wing spar, and a plurality of contiguously adjacent wing spar sections. At least a first wing spar section includes at least one upper and lower spar chord which is unitarily formed as a one-piece structure with upper and lower ends of the upright central web, respectively, while at least a second wing spar section includes at least one upper and lower spar chord which is a separate structural element integrally fixed to the upper and lower ends of the upright central web, respectively.
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