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Airborne elevator apparatus

一种升降机、空用的技术，应用在刚性飞船、气球飞行器等方向

Inactive Publication Date: 2013-02-20
丹尼尔·S.·瑞德福特
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0017] A search of the prior art did not reveal any patents disclosing the present invention, and none of the prior art dealing with tethered aerostats could claim to be load neutral, or deploy multiple service loads simultaneously in the Earth's atmosphere on different altitudes

Method used

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Embodiment Construction

[0067] Those skilled in the art will better understand the novelty and advantages of this invention by referring to the following description of the best mode for carrying out the invention together with the accompanying drawings.

[0068] exist Figure 1 to Figure 5 In , a preferred embodiment of the invention is shown.

[0069] figure 1A preferred embodiment of the present invention is shown, comprising an aerial device 10 for locating aerial lift equipment in the Earth's atmosphere, for simultaneously deploying a plurality of service loads in the Earth's atmosphere along different The aerial device 50 for altitude, and the device 120 for controlling the operation of the aerial lift equipment.

[0070] figure 1 Further shown is the vacant lift installation secured to a service area 100 , which in the figure is an on-road service area 102 .

[0071] figure 1 Still further shown is an aerial apparatus 10 for positioning aerial elevator installations in the earth's atmosph...

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Abstract

An Airborne Elevator Apparatus capable of deploying at the same time multiple service loads at different altitudes in the Earth's atmosphere by physically separating tether weight carrier function from the service load weight carrier function of a common aerostat. The tether weight carrier function is performed by at least one airborne canopy assembly (20) filled with lighter than air gas, which has enough lifting power to support its own weight and the weight of the attached airborne cables (30). The service load carrier function is performed by several airborne booster assemblies (51). Designed to glide on the apparatus's airborne cables (30), an airborne booster assembly (51) filled with lighter than air gas has enough lifting power to carry its own weight and the weight of a service load at altitudes below the uppermost canopy. For stability purposes, the apparatus is designed to rotate around its vertical axis.

Description

technical field [0001] The present invention generally relates to the field of hybrid moored aerostats, in particular to an aerial elevator. Background technique [0002] Modern interest in the use of tethered aerostats for carrying and performing various surveillance and communication tasks is growing. Unlike fixed-wing aircraft or helicopters, these aerostats use helium or hydrogen to stay in the air. Tethered aerostats are unmanned, inexpensive, and secured to the ground by a tethering system that also provides power and communications. [0003] Webster's Dictionary defines the term "service load" as "the load that a structure is expected to support under normal use". [0004] The purpose of the tethered aerostat is to lift in the Earth's atmosphere and maintain the service load at a predetermined deployment altitude. Its lifting capacity should be sufficient to support its own weight, the weight of its tether, and the weight of the service load. Because the weight of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/06
CPCB64B1/50B64B1/30B64B1/06B64B1/66B64F1/14
Inventor 丹尼尔·S.·瑞德福特
Owner 丹尼尔·S.·瑞德福特
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