The invention provides a machine empennage front edge deicing sleeve bonding method, which mainly comprises the processes of deicing sleeve bonding surface polishing, adhesive preparation, adhesive coating, deicing sleeve bonding, bag making, vacuumizing curing, edge sealing adhesive brushing, conductive coating brushing, inflation test and the like, and solves the problems of easy adhesive failure, debonding and the like of a deicing sleeve in a traditional method. And the service life of the deicing sleeve is prolonged.
本发明提供了一种机尾翼前缘除冰套粘接方法,发明主要包括打磨除冰套粘接面、胶粘剂准备、涂胶、粘接除冰套、制袋、抽真空固化、涂刷封边胶、涂刷导电涂层、充气试验等过程,解决了传统方法除冰套易开胶、脱粘等问题,提高了除冰套的使用寿命。
Bonding method for deicing sleeve at front edge of empennage
一种机尾翼前缘除冰套的粘接方法
2024-01-02
Patent
Electronic Resource
Chinese
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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |
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