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Hub motor type anchoring vehicle

A hub motor and anchoring car technology, applied in the field of aircraft and tethered balloons, can solve the problems of insufficient mobility, large wind load on the capsule body, and inability to realize the wind chasing function, etc., and achieve the effect of being convenient for road and air delivery

Pending Publication Date: 2018-07-24
丹阳昊天飞行器技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The traditional mooring vehicle has the disadvantage of insufficient maneuverability, and cannot realize the wind chasing function during the inflation stage of the tethered balloon and the transition stage of anchoring, so that the balloon body bears a large wind load during the inflation process, which has an unpredictable impact on the balloon structure

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0119] Such as figure 1 As shown, Embodiment 1 of the present invention provides a specific hub motor type anchor parking solution, which includes a chassis 1, a slewing platform 2, a mobile system 3, a retractable system 4, a mooring system 5 and a boat support command room 6 . This embodiment is based on figure 1 Describe the orientation of the identification, figure 1 The right side is in front of the anchor car, figure 1 On the left is the rear of the anchored vehicle.

[0120] Such as figure 2 As shown, the chassis 1 includes a rectangular frame frame 10 , four telescopic hydraulic legs 11 , an energy pod 12 and a hanger 13 . The bottom of the chassis 1 is connected to the four wheel assemblies through the connecting flange 34 , and the top is connected to the slewing platform 2 through the slewing support 22 . Circuits, oil circuits and signal systems are arranged on the chassis 1 .

[0121] The frame frame 10 is welded by square steel, and the cable installation...

Embodiment 2

[0137] Embodiment 2 of the present invention provides a specific nose cone lock, which is an internal rotation unlocking nose cone lock.

[0138] see Figure 6 and 7 , The internal rotation unlocking nose cone lock described in this embodiment includes a cavity unit 501 , an internal rotation unlocking unit 502 , a latch unit 503 , a mounting seat 504 , a driving unit 505 , and a guide pulley unit 506 .

[0139] see Figure 8 , the cavity unit 501 includes a cavity flange 5011 and a cavity bell mouth 5012 . Both ends of the cavity flange 5011 have flange surfaces, wherein the larger flange is connected to the mounting seat 504, and the smaller flange is connected to the flange side of the bell mouth 5012 of the cavity. There are three through holes 50121 on the outer surface of the smaller diameter end of the bell mouth 5012 of the cavity, that is, the neck, for the lock block 5035 to pass through. Three latch units 503 are installed on the corresponding positions, such as...

Embodiment 3

[0150] Embodiment 3 of the present invention provides a tethered balloon used in conjunction with the mooring vehicle of Embodiment 1. The tethered balloon is characterized in that it has a high-strength nose cone connection device.

[0151] Specifically, the high-strength nose-cone connecting device described in this embodiment includes a head skin 92, a hull skin 91, a first reinforcement cloth 93, a second reinforcement cloth 94, an edge reinforcement strip 95, and an eyelet button 96. and rope 97. The first reinforcing cloth 93 and the second reinforcing cloth 94 are ring-shaped, and the ring part is overlapped and welded between the head skin 92 and the hull skin 91, and the edge part connected with the ring part passes through the hull The inner ring of the skin 91 is folded away from the tethered balloon, that is, toward the nose cone, so the inner ring of the hull skin 91 constrains the ring portions of the first reinforcing cloth 93 and the second reinforcing cloth 94...

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Abstract

The invention belongs to the field of captive balloons and relates to a hub motor type anchoring vehicle which comprises a chassis (1), a rotary support (22) arranged on the chassis (1), a rotary platform (2) arranged on the rotary support (22), a retrieval and release system (4), a mooring system (5) and a bracket command chamber (6). The retrieval and release system (4), the mooring system (5) and the bracket command chamber (6) are arranged on the rotary platform (2). Through optimal design of an anchoring vehicle moving system, maneuverability of the whole system is improved. By adopting atraveling device with a hub motor and a steering device with a steering motor, turning and moving of the anchoring vehicle in any direction are realized, a wind following function of the system is improved; structural form of a mooring tower is improved, structural efficiency is improved by adopting a plate-column structure, and convenience is brought to automatic retracting and releasing. The hub motor type anchoring vehicle is high in maneuverability and flexible in release and arrangement and can be widely used for release and retrieval of small-and-medium captive balloons.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to the field of moored balloons, in particular to a hub motor type anchor vehicle. Background technique [0002] As an ideal aerial platform, tethered balloon has been favored by people since its birth. It has the advantages of long blanking time, large coverage area, low energy consumption, easy disassembly and collection, and strong mobility. Since ordinary aircraft cannot stay in the air for a long time, tethered balloons can stay in the air for several weeks or even months, and can be used for weather observation, forecasting, and monitoring of aircraft, etc., so it has attracted attention from all parties. In addition to being used for weather forecasting, aircraft monitoring, broadcast communication, and topographic mapping, tethered balloons can also be used for low-altitude early warning, especially for air monitoring of border defense and coastal defense, and anti-terrori...

Claims

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Application Information

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IPC IPC(8): B64B1/66B64B1/50B60P3/00B60K7/00
CPCB64B1/50B64B1/66B60K7/00B60P3/00
Inventor 郑杨涛施志强
Owner 丹阳昊天飞行器技术有限公司
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