Latch for joining two panels of an airplane structure
A technology of latches and components, applied in the field of latches, which can solve problems such as the weight, size and reliability of latches, and achieve the effect of improving overall safety and reliability and compact structure
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[0026] Figure 1 to Figure 5 As shown, the latch 1 in the first preferred implementation of the present invention is used to connect two wings 16, 17 in the aircraft component to each other. 18 combination, on the other hand, is firmly fixed on the wing plate 17 by the main pin 3.
[0027] The latch 1 has a hinge comprising: a pair of first pressurized links 4 and a pair of second pressurized links 5; The operating part constituted; the spring 9 for pushing the above-mentioned handle 6 to disengage from the hook 2;
[0028] More specifically, the hook 2 has a curved end 12, and the handle 6 is pivotally mounted, rotatably, on an end pin 13 located at an end position opposite to the curved end 12, this end pin 13 passing through the handle 6 The two side flanges of 8. The two connecting rods 4 and 5 of each pair of connecting rods are installed on both sides of the hook 2 respectively, wherein each connecting rod 4 can rotate around the main pin 3 and can also rotate around ...
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