Aircraft structural components

Details Aircraft structural components Aircraft structural components

2002-07-11

2009-12-08

Chevalier, Alicia (Department: 1794)

Stock material or miscellaneous articles

Structurally defined web or sheet

Including aperture

C244S123100

Reexamination Certificate

active

07629037

ABSTRACT:
A structural component such as a wing skin for an aircraft is formed generally of a first composite fiber and matrix material exhibiting a first tensile modulus in respect of tensile stress and a first tolerance of strain resulting from such stress. One or more openings are provided in the component and the material of a portion of the component bounding the opening(s) is a second composite fiber and matrix material. The second material exhibits a second tensile modulus in respect of tensile stress that is smaller than the first tensile modulus of the first material and a second tolerance of strain resulting from such stress that is greater than the first tolerance of strain of the first material.

REFERENCES:
patent: 3260398 (1966-07-01), Levenetz
patent: 3946127 (1976-03-01), Eisenmann et al.
patent: 5452867 (1995-09-01), Grunwald et al.
patent: 5914163 (1999-06-01), Browne
patent: 199 25 953 (2000-09-01), None
patent: WO 00/24553 (2000-05-01), None
patent: WO 01/58680 (2001-08-01), None

Affiliated with

Also associated with

Rating

Aircraft structural components does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft structural components, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft structural components will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-4148699