The invention discloses an assembling tool for a hydraulic system combination block of an aircraft lifting aileron actuator. The assembling tool comprises a first bent connector measuring frame, a first bent connector measuring frame fixing seat, a second bent connector measuring frame, a second bent connector measuring frame fixing seat, a bent connector port fixing assembly and a measuring datum conversion assembly. The first elbow joint measuring frame is of a Z-shaped frame structure, is sleeved outside the first elbow joint, and is assembled with the first elbow joint through a first elbow joint measuring frame fixing seat and an elbow joint port fixing assembly; the second elbow joint measuring frame is of an inverted V-shaped frame structure, is sleeved outside the second elbow joint, and is assembled with the second elbow joint through a second elbow joint measuring frame fixing seat and an elbow joint port fixing assembly; and the measurement basis conversion assembly is used for realizing the conversion of the size measurement basis in the assembly process. The requirements for the assembling size and angle of the pipe joint on the combined block in the aircraft maintenance process are met, and the purposes of guaranteeing the aircraft maintenance quality and safe flight are achieved.
一种飞机升降副翼作动器液压系统组合块装配工装,包括第一弯接头测量架、第一弯接头测量架固定座、第二弯接头测量架、第二弯接头测量架固定座、弯接头端口固定组件和测量基准转换组件;所述第一弯接头测量架为Z型架结构,套装在第一弯接头外面,通过第一弯接头测量架固定座及弯接头端口固定组件将其与第一弯接头装配;所述第二弯接头测量架为倒置的V型架结构,套装在第二弯接头外面,通过第二弯接头测量架固定座及弯接头端口固定组件将其与第二弯接头装配;所述测量基准转换组件用于在装配过程中实现尺寸测量基准的转换。本发明满足了飞机维修过程中组合块上管接头装配尺寸和角度要求,达到了保证飞机维修质量和安全飞行的目的。
Assembly tool for hydraulic system combination block of aircraft lifting aileron actuator
一种飞机升降副翼作动器液压系统组合块装配工装
30.01.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | 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 |
Lifting aileron for unmanned aerial vehicle and lifting aileron control device
Europäisches Patentamt | 2024
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