Micro flying robot with connecting rod type foldable flapping wings

A flying robot and connecting rod technology, which is applied in the field of overall structure design of foldable flapping wing micro-aircraft, can solve the problems of assembly performance impact of the whole machine, wing bending and deformation, and inability to fold closer, so as to improve folding reliability, The effect of reducing flight load and improving flexibility

Active Publication Date: 2019-06-21
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the aircraft wings currently designed cannot be folded close to the fuselage. During the carrying and transportation process after the flight, the exposed wings are easy to contact with other objects to cause bending deformation, and the assembly performance of the whole aircraft may be affected. Affected, thus affecting the flight attitude of the next mission

Method used

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  • Micro flying robot with connecting rod type foldable flapping wings
  • Micro flying robot with connecting rod type foldable flapping wings
  • Micro flying robot with connecting rod type foldable flapping wings

Examples

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Embodiment Construction

[0035] The present invention is described in detail below in conjunction with accompanying drawing:

[0036] Such as figure 1 As shown, the connecting rod type foldable flapping wing miniature flying robot of the present invention is characterized in that: the present invention is made up of right wing A, nose device B, left wing C and empennage device D. Wherein: said right wing A and left wing C are symmetrical structures about the center line of the fuselage, the j hole of the swing link II5 in the right wing A passes through the bolt and the belt hole of the right swing link I14 in the nose device B The ear pair IIn is movably connected; the j hole of the swing rod II in the left wing C is movably connected with the holed ear pair Ip of the left swing rod I8 in the nose device B through bolts; the right slide rail 6 in the right wing A is connected with the empennage The side of the right steering gear 36 in the device D is affixed; the left slide rail in the left wing C is...

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Abstract

The invention discloses a micro flying robot with connecting rod type foldable flapping wings, belonging to the technical field of design and manufacture of micro aerial vehicles. In the micro flyingrobot with the connecting rod type foldable flapping wings, a right wing and a left wing are symmetrical structures about the center line of a fuselage, and a j hole of an oscillating bar II in the right wing is movably connected with a perforated lug pair II of a right oscillating bar I in a handpiece device through a bolt; a j hole of an oscillating bar II in the left wing is movably connected with a perforated lug pair I of a left oscillating bar I in the handpiece device through a bolt; a right sliding rail in the right wing is fixedly connected with the side surface of a right steering engine in an empennage device; a left sliding rail in the left wing is fixedly connected with the side surface of a left steering engine in the empennage device; a fuselage rod in the handpiece device is fixedly connected with a p hole in the left end of a vertical tail in the empennage device; the foldable flapping wings of the micro flying robot can be tucked and folded after flying, the exposurearea of the wings can be reduced, and the transportation and storage are convenient.

Description

technical field [0001] The invention belongs to the technical field of micro-aircraft design and manufacture, and in particular relates to the overall structural design of a foldable flapping-wing micro-aircraft. Background technique [0002] Insects in the natural world have superb ultra-low-altitude flight capabilities, and their flexibility and maneuverability are beyond the reach of aircraft designed by humans. The development direction of micro-aircraft has gradually become a hot research topic. Most of the aircraft wings currently designed cannot be folded close to the fuselage. During the carrying and transportation process after the flight, the exposed wings are easy to contact with other objects to cause bending deformation, and the assembly performance of the whole aircraft may be affected. Affected, thereby affecting the flight attitude of the next mission. [0003] Coleoptera insect beetles in nature can fold their membranous hind wings under the elytra when th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C33/02
Inventor 刘超孙霁宇李法东杜瑞娟宋泽来李娜王一尘王悦明吴薇马云海佟金
Owner JILIN UNIV
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