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A shuttle structure for aircraft

An aircraft and shuttle-shaped technology, applied in the field of aircraft, can solve the problems that affect the use of the aircraft shuttle-shaped structure, and the parts of the aircraft cannot be fixed well, so as to achieve the effect of increasing convenience, safe and convenient use, and convenient and stable support

Active Publication Date: 2022-05-13
NORTH CHINA INST OF AEROSPACE ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • A shuttle structure for aircraft
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Embodiment

[0037] Example: such as Figure 1-7 As shown, the present invention provides a technical solution, a shuttle-shaped structure for an aircraft, including a housing 1, and fixed shafts 2 are installed symmetrically through the outer two ends of the housing 1, and the inside of the housing 1 corresponds to the outer position of the fixed shaft 2. Connected with a shuttle-shaped inner frame 3;

[0038] The top of the shuttle-shaped inner frame 3 is equipped with a stable placement mechanism 4, which includes a placement thread groove 401, a stabilizing top ring 402, a placement screw 403, a fixed top frame 404, an adjustment screw 405, an adjustment pressing plate 406, and a placement bottom frame. 407, clamping telescopic rod 408, clamping spring 409 and clamping arc plate 410;

[0039] The top of the shuttle-shaped inner frame 3 is uniformly provided with a thread groove 401, and the top of the shuttle-shaped inner frame 3 is installed at the position corresponding to the threa...

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PUM

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Abstract

The invention discloses a shuttle-shaped structure for an aircraft, which comprises a casing, fixed shafts are installed symmetrically through the outer two ends of the casing, and a shuttle-shaped inner frame is connected to the outer position of the outer casing corresponding to the fixed shaft. , the top of the shuttle-shaped inner frame is uniformly provided with a thread groove, the top of the shuttle-shaped inner frame is installed at the position corresponding to the thread groove, and a stable top ring is installed, and the top of the stable top ring is embedded in the position corresponding to the thread groove A placement screw is installed. The structure of the present invention is scientific and reasonable, and it is safe and convenient to use. Through the set stable placement mechanism, the aircraft parts can be placed on the top of the placement chassis, and the placed aircraft parts can be placed using the clamping telescopic rod and the clamping spring. Clamping also facilitates the clamping and placement of aircraft parts, improves the stability of aircraft parts when placed, and increases the convenience of the shuttle-shaped structure of the aircraft in use.

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...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/06B64G1/22
CPCB64C1/06B64C1/061B64G1/22
Inventor 田东兴蔡志为
Owner NORTH CHINA INST OF AEROSPACE ENG
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