Sealing and riveting tool and sealing and riveting method applicable to composite vertical tail wing box of airplane
A composite material and vertical tail technology, which is applied to household appliances, other household appliances, household components, etc., can solve the problems of inability to reset, large product structure and difficult installation of fasteners, etc., to achieve a wide range of applications and improve product quality. , the effect of reducing the impact of structural strength
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Embodiment 1
[0026] Such as figure 1 with figure 2 As shown, a riveting tool suitable for an aircraft composite material vertical tail wing box includes an endoscope lens 1, a magnetic chuck 2, an extension tube 3, a handle 4, a wind pipe 5, a wind control switch 6 and a display screen 7. .
[0027] The handle 4 is connected with the extension tube 3, and the extension tube 3 is connected with the magnetic chuck 2. One end of the air tube 5 is connected to the wind control switch 6, and the other end passes through the handle 4 and the extension tube 3 and then communicates with the magnetic chuck 2. The endoscope lens 1 is installed on the magnetic chuck 2, and the endoscope lens 1 is connected to the display screen 7 through a wire.
[0028] The magnetic chuck 2 is provided with a groove 2-1, and a permanent magnet 2-2 is arranged in the groove 2-1.
Embodiment 2
[0030] During the assembly process of the aircraft, the vertical tail wing box of the aircraft is composed of the right side wall plate I10 and the left side wall plate II20 to form a "closed box section". The beam at the lower end of the "closed box section" is provided with a "lightening hole" 40. The inside of the "closed box section" that constitutes the wing box is supported by ribs. All of the above are composite materials. At the joint between the ribs and the long truss, the design uses connecting corners to strengthen the structural strength. There are 82 corners in total, and each corner is on Two fasteners need to be installed in a closed space.
[0031] A method for sealing riveting suitable for aircraft composite material vertical tail wing box, using the riveting tool suitable for aircraft composite material vertical tail wing of embodiment 1, includes the following steps:
[0032] 1) Such as image 3 As shown, the two wall panels that constitute the vertical tail wi...
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