Fusiform structure for aircraft

An aircraft and shuttle-shaped technology, applied in the field of aircraft, can solve the problems affecting the use of the shuttle-shaped structure of the aircraft, and the parts of the aircraft cannot be well fixed, and achieve the effects of increased convenience, safe and convenient use, and easy stable support.

Active Publication Date: 2021-04-09
NORTH CHINA INST OF AEROSPACE ENG
View PDF17 Cites 0 Cited by
  • 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

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Fusiform structure for aircraft
  • Fusiform structure for aircraft
  • Fusiform structure for aircraft

Examples

Experimental program
Comparison scheme
Effect test

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...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

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...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(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
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap