Pressure regulation and control method and system for stratospheric airship

A stratospheric airship and control system technology, applied in the field of aircraft, can solve the problems of large buoyancy day-night cycle loss, buoyancy loss, buoyancy gas leakage loss, etc., to solve structural safety problems, reduce strength requirements, and improve performance Effect

Inactive Publication Date: 2017-05-10
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

[0005] However, during the long-term resident period of the stratospheric airship, the solar radiation during the day will cause the temperature of the capsule body and the internal buoyant gas to rise continuously, which will cause a large increase in the air pressure inside the stratospheric airship capsule. Under the condition of certain pressure capacity, the oversized size will reduce the compressive capacity of the main capsule, which puts forward very stringent requirements for the skin material; the decrease of the surface temperature of the capsule at night will lead to a large decrease in the pressure inside the capsule of the stratospheric airship , not only is it difficult to guarantee the shape of the airship, but it will also cause buoyancy loss and cause the airship to descend; if the overpressure conformal state is set according to the night, the pressure will

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  • Pressure regulation and control method and system for stratospheric airship

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Embodiment Construction

[0024] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0025] The present invention provides a method for regulating the pressure of a stratospheric airship. A pressure regulating capsule 2 is arranged in the inner cavity of the main capsule 1 of the stratospheric airship, and the inside of the main capsule is buoyant due to temperature changes during day and night operation. When the gas pressure increases or decreases, the pressure sensor 5 is installed on the main capsule 1 to detect the pressure change inside the main capsule 1 or the pressure inside and outside the main capsule 1 in real time. Part of the buoyant gas is pressed into or released from the pressure regulating capsule 2 to realize pressure regulation, so that the pressure of the main capsule remains stable.

[0026] When the pressure of the main capsule rises, part of the buoyant gas in the main capsule is pressed into the pressur...

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Abstract

The invention provides a pressure regulation and control method and system for a stratospheric airship. A pressure regulation and control capsule body is arranged in a main capsule body of the stratospheric airship. The pressure of buoyancy lift gas in the main capsule body is increased or decreased due to the temperature change in the day and night operation process in the main capsule body. A part of buoyancy lift gas in the main capsule body is pressed into the pressure regulation and control capsule body or the gas in the pressure regulation and control capsule body is released to enter the main capsule body so as to achieve pressure regulation, so that the pressure of the main capsule body remains stable. According to the pressure regulation and control method and system for the stratospheric airship, the problem that a pressure regulation and control mode is irreversible due to the day and night state change in the long-term operation process of a current stratospheric airship can be solved, and the stratospheric airship is promoted to be practical as soon as possible.

Description

technical field [0001] The invention mainly relates to the field of aircraft technology, in particular to a pressure control method and a control system for a stratospheric airship working for a long time. Background technique [0002] The stratospheric airship is a controllable aircraft that is lighter than air. It mainly relies on the buoyancy generated by the buoyant gas in the capsule structure to achieve weight balance. It mainly relies on solar cells and energy storage batteries to form a closed-loop energy system to achieve long-term stability. Flying, this type of aircraft works in the stratosphere altitude area near 20 kilometers from the ground, taking advantage of the stable atmospheric environment in this area, taking advantage of the characteristics of the low-speed wind field in this area, resisting wind with less propulsion energy, combined with closed-loop energy The system can realize the airborne flight capability over an area of ​​the annual level. [000...

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Application Information

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IPC IPC(8): B64B1/62
CPCB64B1/62
Inventor 侯中喜邓小龙杨希祥麻震宇朱炳杰
Owner NAT UNIV OF DEFENSE TECH
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