Propeller telescoping and head tilting device for trans-medium aircraft

A propeller and aircraft technology, which is applied in the field of propeller expansion and nose tilting devices of trans-medium aircraft, can solve the problems of increasing underwater sneak resistance, and cannot completely solve the impact of propeller and impact force, so as to shorten the time of water discharge and solve the power of water discharge Insufficient, fast water effect

Active Publication Date: 2019-06-14
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The design difficulties of the cross-media aircraft mainly focus on the three working modes of water entry mode, underwater sneaking mode and water exiting mode. The propellers in the parts will generate impact on the water surface, which will increase the resistance of underwater divin

Method used

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  • Propeller telescoping and head tilting device for trans-medium aircraft
  • Propeller telescoping and head tilting device for trans-medium aircraft
  • Propeller telescoping and head tilting device for trans-medium aircraft

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Embodiment Construction

[0035] Describe the present invention below in conjunction with accompanying drawing.

[0036] Such as Figure 1 to Figure 8 , Figure 10 , Figure 11 , Figure 13 As shown, the present invention is made up of nose telescopic mechanism A, propeller telescopic mechanism B, propeller drive mechanism C, telescopic drive mechanism D, and nose tilting mechanism E, wherein the tooth on the right side of telescopic shaft 7 in nose telescopic mechanism A Bar I39 meshes with gear III21 in telescopic drive mechanism D; guide rail I8 of nose telescopic mechanism A is fixedly connected to stud group IIId through installation hole II42, and stud group IIId is welded to machine head housing shell 37; propeller telescopic mechanism B The hollow shaft 10 is set on the telescopic shaft 7 of the nose telescopic mechanism A, and is located between the rear cover 6 and the rack I39; the rack II14 of the propeller telescopic mechanism B meshes with the gear IV24 of the telescopic drive mechanis...

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Abstract

Disclosed is a propeller telescoping and head tilting device for a trans-medium aircraft, which belongs to the technical field of trans-medium aircrafts. In the propeller telescoping and head tiltingdevice, a rack I of a head telescoping mechanism is engaged with a gear III of a telescoping driving mechanism. A guide rail I is fixedly connected to a head bin shell. A hollow shaft sleeves the middle of a telescopic shaft in the head telescoping mechanism. A rack II is engaged with a gear IV. A guide rail II is fixedly connected to the head bin shell. A base of a motor I is fixedly connected toa support plate. A base of a motor II in the telescoping driving mechanism is fixedly connected to the head bin shell. A bearing II with a seat and a bearing III with a seat are respectively fixedlyconnected to a bearing mounting plate I and the bearing mounting plate II. The inner ends of a tilting shaft I and a tilting shaft II are fixedly connected to the head bin shell. Bases of a bearing IVwith a seat and a bearing V with a seat are fixedly connected to a fuselage shell. A base of a motor III is fixedly connected to the fuselage shell. The propeller telescoping and head tilting devicefor a trans-medium aircraft can realize the extension and contraction of propellers, which ensures good sealing performance and small underwater running resistance of the aircraft, and can realize rapid out-of-water of the aircraft, which greatly shortens the out-of-water time of the aircraft.

Description

technical field [0001] The invention belongs to the technical field of cross-medium aircraft, and in particular relates to a propeller telescopic and head tilting device for a cross-medium aircraft. Background technique [0002] The cross-media aircraft is a new concept sports platform designed by multi-disciplinary integration of aircraft and underwater vehicles. It is a new multi-functional integrated equipment that can fly in the air and dive underwater. The working mode of the aircraft can be divided into air flight mode, water entry mode, underwater sneaking mode and water exit mode, which can be switched among various working modes according to mission requirements. Cross-media unmanned aerial vehicles can be matched with submarines, surface ships and other equipment to perform tasks such as intelligence collection, reconnaissance and surveillance, communication relay, and electronic countermeasures across the sea and air. [0003] The design difficulties of the trans...

Claims

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Application Information

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IPC IPC(8): B64C11/00B60F5/02
Inventor 张成春齐德波辛振涛甘中林余新月单永航方旭文叶欣仪王晶刘燕韩志武任露泉
Owner JILIN UNIV
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