The present invention comprises: a mold composed of a central mold plate, a peripheral mold plate to which the central mold plate is movably coupled in the vertical direction, a lifting drive part for moving the central mold plate in the vertical direction, and a film adsorbed in a vacuum on the upper surface of the lifting drive part, the central mold plate, and the peripheral mold plate; and an automatic fiber laminating machine composed of a supply unit for supplying carbon fiber tape, a head unit for laminating, cutting, heating, and pressing the supplied carbon fiber tape, and a robot unit for moving the head unit to a set position and forming a laminate by laminating the carbon fiber tape on the upper surface of the film. Even if the thickness of the laminate is gradually increased, the height of the upper part of the laminate with respect to the upper part of the peripheral mold plate is kept constant. Therefore, when a pressing part moves up along the edge of the laminate, damage to the edge of the laminate by collision with the pressing part is prevented.
본 발명은, 중앙몰드판과, 중앙몰드판이 상하방향으로 이동 가능하게 결합되는 주변몰드판과 중앙몰드판을 상하방향으로 이동시키는 승강구동부와 중앙몰드판과 주변몰드판의 상면에 진공흡착된 필름으로 구성된 몰드와, 탄소섬유테이프를 공급하는 공급유닛과 공급된 탄소섬유테이프를 적층, 절단, 가열, 가압하는 헤드유닛과 헤드유닛을 설정된 위치로 이동시키는 로봇유닛으로 구성되어 상기 필름의 상면에 상기 탄소섬유테이프를 적층하여 적층물을 형성하는 자동섬유적층기를 포함하는 것을 특징으로 한다. 이로 인해, 적층물의 두께가 점점 두꺼워지더라도 주변몰드판의 상단부에 대한 적층물의 상단부의 높이를 일정하게 유지시켜 가압부가 적층물의 모서리(edge)를 타고 올라올 때 가압부와의 충돌에 의해 적층물의 모서리가 손상되는 것이 방지된다.
Aircraft Wing End Composite Structure Manufacturing Equipment
항공기 날개 끝단 복합재 구조물 제조장치
2021-11-05
Patent
Electronic Resource
Korean
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
European Patent Office | 2016
|COMPOSITE MATERIAL, LAYERED STRUCTURE, AIRCRAFT WING, AND COMPOSITE MATERIAL MANUFACTURING METHOD
European Patent Office | 2019
|European Patent Office | 2018
|European Patent Office | 2015
|European Patent Office | 2017
|