Natural heat and sail driven aerostat system with controllable track

An aerostat and trajectory technology, applied in the field of aerostat systems, can solve the problems of short high-altitude flight time, small load, complex system, etc., and achieve the effects of easy acquisition and replacement, easy engineering implementation, and simple system

Inactive Publication Date: 2014-03-26
CHINA ACADEMY OF SPACE TECHNOLOGY
View PDF5 Cites 16 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] High-altitude balloons are currently the only mature stratospheric aerostats, but the commonly used zero-pressure balloons use the method of throwing sand and deflation to maintain altitude in order to cope with diurnal changes, and the high-altitude flight time is short (several days); Structural design issues, only dozens of days of flight in the Antarctic region; general hot air balloons consume a lot of fuel during the flight; the infrared hot air balloon (MIR) proposed by France has a long flight time (the average flight time is 3 weeks, the longest record 69 days), but can carry a smaller payload
More importantly, high-altitude balloons lack active control means and can only fly with the wind, unable to achieve cruise residence in a specific area
An ideal stratospheric airship can achieve fixed-point residence and cruising maneuvers at the height of the stratosphere, but the technology is difficult and the system is complex, and there is no successful application precedent.

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
  • Natural heat and sail driven aerostat system with controllable track
  • Natural heat and sail driven aerostat system with controllable track
  • Natural heat and sail driven aerostat system with controllable track

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0017] As shown in Figure 1, it is the overall composition of the system of the present invention, and it is made up of two modes, and the first mode is a normal working mode, including upper skin 1, lower skin 2, suspension rope 4, equipment load cabin 5 , a support arm 6, a pneumatic sail surface 7, a measurement control module 8, a vector thruster 9, a deflection control cable 10 and an air valve 11. Such as figure 2 As shown, it is composed of the equipment load compartment 5 system of the present invention, which is composed of solar cells 5-1, connecting wires 5-2, electronic control equipment 5-3, battery 5-4, payload 5-5, and rope retractable The control device 5-6, the buoyant gas cylinder 5-7, the control valve 5-8, and the gas pipeline 5-9 are composed. The second mode is the buoyancy supplement mode, and the auxiliary airbag 3 is introduced on the basis of the system composition of the first mode.

[0018] The main airbag is composed of an upper skin 1 and a low...

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 relates to a natural heat and sail driven aerostat system with a controllable track. An upper covering and a lower covering are welded to form a main air bag which is filled with the air. As the outer surface of the upper covering and the outer surface of the lower covering are coated with heat control coatings, solar radiant heat and infrared radiant heat of the surface of the earth are absorbed, so that the temperature of the air in the main air bag is raised and floating force is generated; an air valve is installed on the top of the main air bag and started and closed by receiving instructions of a device load cabin so as to control the height of the whole system; the device load cabin is connected to the lower portion of the main air bag by tying a rope in a hanging mode, the lower portion of the device load cabin is connected with a supporting arm through a deviation control cable, and a measurement control module, a pneumatic sail face and a vector thruster are arranged on the supporting arm. The stressed direction of the pneumatic sail face is crossed with the action direction of the vector thruster in an orthogonality mode. The measurement control module receives the instructions sent by the device load cabin and controls starting and closing of the vector thruster and the rotation angle of the supporting arm.

Description

technical field [0001] The invention relates to a new type of aerostat, in particular to an aerostat system utilizing natural heat energy to float in the air, with adjustable height and controllable trajectory, which can be used as an important means for flight detection of adjacent space and planetary atmosphere. Background technique [0002] Near space (Near space) generally refers to the airspace at an altitude of 20-100 km from sea level, and is a space field that is rarely involved in current human activities. With the advancement of modern science and technology, the unique resource advantages of adjacent space have become the focus of attention of all countries. Stratospheric aerostats are an important means for the development and utilization of adjacent space resources. As a near space information platform, it can realize long-term real-time, all-weather and all-weather high-resolution earth observation and high-speed mobile communication in a specific area by carr...

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): B64B1/62B64B1/64
Inventor 姚伟王超马蓉吕晓辰
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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