Invention Application
- Patent Title: Ducting For A Fluid Transfer Pipeline For An Aircraft Or Spacecraft, Method For Producing Same And Aeronautical Structure Incorporating Same
- Patent Title (中): 用于航空器或航天器的流体输送管线的管道,产生与其相同的航空结构的方法
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Application No.: US14448144Application Date: 2014-07-31
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Publication No.: US20140338816A1Publication Date: 2014-11-20
- Inventor: Jean-Pierre Ciolczyk , Marc Dolez , Bertrand Florentz
- Applicant: Hutchinson
- Priority: FR0805782 20081017
- Main IPC: B29D23/00
- IPC: B29D23/00 ; B29C65/08 ; B29C49/04 ; B29C70/44 ; B29C49/44 ; B29C53/08 ; B29C70/30 ; B29C65/66 ; B29C49/26

Abstract:
A ducting and associated method is provide in which the ducting includes a pipe with a thermoplastic or thermoplastic elastomeric layer and a reinforcing layer. The pipe has a curved or bent geometry and the reinforcing layer is made of a composite material based on reinforcement in intimate and direct contact with the subjacent layer. The geometry is obtained by hot forming the inner layer to give the geometry, and the reinforcement is either impregnated with a thermosetting matrix to form a thermosetting composite, or reinforcing fibers are intermixed with thermoplastic fibers or powders, or impregnated with a plastic polymeric coating that is curable chemically. Alternatively, the inner layer is first covered with the reinforcing layer in which the reinforcement includes reinforcing fibers intermixed with a thermoplastic material in the form of fibers, film or powder is blow-molded to give the pipe its final geometry.
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