US2022118727A1PendingUtilityA1

Composite stiffener

Assignee: AIRBUS OPERATIONS LTDPriority: Mar 1, 2019Filed: Dec 28, 2021Published: Apr 21, 2022
Est. expiryMar 1, 2039(~12.6 yrs left)· nominal 20-yr term from priority
B29C 70/207B29C 70/302B64C 3/185B64C 3/18B29D 99/0014B64C 1/00B29C 70/30B64C 3/20B32B 5/024B29L 2031/3085B29C 2793/0081B64C 1/064B29L 2031/3076B29C 70/222B64C 3/182B32B 2262/106B64C 3/26B64C 2001/0072B32B 7/03B29C 70/443B29C 70/085B29B 11/16B29C 70/48B29C 70/462Y02T50/40B29D 99/001B29L 2031/3082B29D 99/0003
62
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

A composite stiffener for a stiffener reinforced panel is disclosed. The stiffener has a longitudinal direction and a run-out region which terminates at an end of the stiffener. The stiffener also has a constant section region inboard of the run-out region in the longitudinal direction and having a constant cross section transverse to the longitudinal direction with a crown between adjacent foot portions. The run-out region has a changing cross section transverse to the longitudinal direction with a crown between adjacent foot portions and the crown reduces in height towards the end of the stiffener forming a ramp. The composite stiffener comprises a number of blankets of non-crimp fabric layers.

Claims

exact text as granted — not AI-modified
1 . A method of manufacturing a stiffener, comprising laying up a plurality of blankets of non-crimp fabric layers and a plurality of woven fabric layers as dry fabrics on a mould tool and co-infusing the dry fabrics with resin followed by co-curing to form the stiffener. 
     
     
         2 . A method according to  claim 1 , wherein the stiffener has a longitudinal direction with a run-out region at which terminates at an end of the stiffener, and a constant section region inboard of run-out region longitudinal direction and having a constant cross section transverse to the longitudinal direction with a crown between adjacent foot portions,
 wherein the run-out region has a changing cross section transverse to the longitudinal direction with a crown between adjacent foot portions and the crown reduces in height towards the end of the stiffener forming a ramp,   the composite stiffener comprises a plurality of blankets of non-crimp fabric layers, and a transition region between the constant section region and the run-out region, wherein the method comprises laying up a plurality of blankets of non-crimp fabric layers sandwiched between woven fabric layers in the constant section region, and cutting at least one of the blankets of non-crimp fabric layers so that the blanket is terminated in the transition region.   
     
     
         3 . A method according to  claim 2 , wherein the run-out region comprises one or more woven fabric layers. 
     
     
         4 . A method according to  claim 3 , wherein the one or more woven fabric layers extends from a top of the ramp to the bottom of the ramp. 
     
     
         5 . A method according to  claim 2 , further comprising cutting all of the blankets of non-crimp fabric layers so that all of the blankets are terminated in the transition region. 
     
     
         6 . A method according to  claim 2 , wherein the run-out region includes the woven fabric layers and no non-crimp fabric blankets. 
     
     
         7 . A method according to  claim 2 , wherein the run-out region has a ramped portion including the ramp, and a substantially planar toe portion between the ramp and the end of the stiffener. 
     
     
         8 . A method according to  claim 2 , wherein each of the blankets of non-crimp fabric layers include a first layer having a 0-degree fibre orientation aligned with the stiffener longitudinal direction and a second layer having a fibre orientation not aligned with the stiffener longitudinal direction. 
     
     
         9 . A method according to  claim 2 , wherein the run-out region includes one or more of the non-crimp fabric blankets. 
     
     
         10 . A method according to  claim 9 , wherein the blanket has a dart cut out and overlaps itself in the run-out region. 
     
     
         11 . A method according to  claim 2 , wherein the constant section region has an omega section. 
     
     
         12 . A method according to  claim 2 , wherein the constant section region has a cross section with continuous layers extending through the crown and the adjacent foot portions. 
     
     
         13 . A method according to  claim 2 , wherein the stiffener comprises carbon fibre composite material. 
     
     
         14 . A method according to  claim 1 , further comprising laying up the plurality of woven fabric layers on a portion of the mould tool to define the shape of the ramp in the run-out region followed by the co-curing step without an intermediate step of cutting the woven fabric layers laid up on the mould tool.

Join the waitlist — get patent alerts

Track US2022118727A1 — get alerts on status changes and closely related new filings.

We store only your email — no account needed. See our privacy policy.