PROBLEM TO BE SOLVED: To provide an adhesively bonded SMA (shape memory alloy)-FRPP (fiber reinforced polymeric plies) joint to increase morphing structure design space and efficiency.SOLUTION: A carbon fiber composite structure 200 includes: a first plurality of carbon fiber 220 prepreg plies 212; and a second plurality of sheets of shape memory alloy 202 interleaved with the first plurality of carbon fiber prepreg plies 212.SELECTED DRAWING: Figure 2
【課題】変形構造物の設計空間および効率を高めるために接着された形状記憶合金(SMA)‐繊維強化ポリマー層(FRPP)接合部の提供。【解決手段】第1の複数の炭素繊維220プリプレグ層212と、第1の複数の炭素繊維プリプレグ層212が挟まれた第2の複数の形状記憶合金板202と、を含む炭素繊維複合構造物200。【選択図】図2
SHAPE MEMORY ALLOY/FIBER REINFORCED POLYMERIC COMPOSITE STRUCTURES AND METHOD FOR FORMING
形状記憶合金/繊維強化ポリマー複合構造物および形成方法
2016-06-16
Patent
Elektronische Ressource
Japanisch
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge / C22F CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS OR NON-FERROUS ALLOYS , Verändern der physikalischen Struktur von Nichteisenmetallen oder Nichteisenlegierungen |
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