Fusiform structure for aircraft

Abstract

The invention discloses a fusiform structure for an aircraft. The fusiform structure comprises an outer shell, fixing shafts are symmetrically installed at the two ends of the outer side of the outer shell in a penetrating mode, fusiform inner frames are connected to the positions, corresponding to the outer sides of the fixing shafts, in the outer shell, and placing threaded grooves are evenly formed in the top ends of the fusiform inner frames; a stable top ring is installed at the position, corresponding to the placing threaded groove, of the top end of each fusiform inner frame, and a placing threaded rod is installed at the position, corresponding to the placing threaded groove, of the top end of the stable top ring in an embedded mode. The fusiform structure has scientific and reasonable structure, safe and convenient use, and the aircraft parts can be placed at the top of a placing chassis through an arranged stable placing mechanism, clamping telescopic rods and clamping springs are used for clamping the placed aircraft parts, clamping and placing of the aircraft parts are also facilitated, the stability of the aircraft parts during placing is improved, and the convenience of the fusiform structure for the aircraft during use is improved.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a shuttle structure for an aircraft. Background technique [0002] Aircraft is a device that flies in the atmosphere or outside the atmosphere. Aircraft are divided into three categories: aircraft, spacecraft, rockets, and missiles. Those flying in the atmosphere are called aircraft, such as balloons, airships, and airplanes. The aerodynamic lift-off flight generated by buoyancy or the relative motion of the air is called a spacecraft that flies in space, such as artificial earth satellites, manned spacecraft, space probes, space shuttles, etc., and they obtain the necessary speed under the push of the launch vehicle Enter space, and then rely on inertia to do orbital motion similar to celestial bodies; [0003] However, when the existing aircraft shuttle structure is in use, the aircraft parts cannot be fixed well in the shuttle structure. It is necessary to customize the shut...

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a technical solution, which can effectively solve the problem that the aircraft parts cannot be fixed well in the shuttle-shaped structure proposed in the above-mentioned background technology. It is necessary to customize the shuttle-shaped structure according to the size and shape of the aircraft parts, which is easy to affect the aircraft. Problems with the use of fusiform structures

Images