Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Raiders and lightweight simulation methods and preparation methods of the boat capsule of the flat straton airship

A technology of stratospheric airship and simulation method, which is applied in the field of large stratospheric airships, can solve problems such as the difficulty of taking into account the light weight of the airship structure, achieve the goal of light weight, reduce technical difficulty, and achieve good results in precise positioning

Active Publication Date: 2020-05-22
北京天恒长鹰科技股份有限公司
View PDF7 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For example, the prior art CN106240844A is a method for designing the strength of a stratospheric airship capsule. This invention accurately determines the thickness of the airship capsule according to the design formula of the stratospheric airship capsule strength, effectively reducing the design in the design theory of the stratospheric airship capsule strength. error, improve the reliability of the airship design, but this invention is to strengthen the entire area of ​​the surface of the airship, and it is difficult to take into account the light weight of the airship structure

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
  • Raiders and lightweight simulation methods and preparation methods of the boat capsule of the flat straton airship
  • Raiders and lightweight simulation methods and preparation methods of the boat capsule of the flat straton airship
  • Raiders and lightweight simulation methods and preparation methods of the boat capsule of the flat straton airship

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0032] Hereinafter, exemplary embodiments of the present disclosure will be described in more detail with reference to the accompanying drawings. Although the drawings show exemplary embodiments of the present disclosure, it should be understood that the present disclosure may be implemented in various forms and should not be limited by the embodiments set forth herein. On the contrary, these embodiments are provided to enable a more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.

[0033] According to the embodiment of the present invention, a simulation method that takes into account the strengthening and lightening of the stratospheric airship capsule is proposed, such as figure 2 , Including the following steps:

[0034] (1) Modeling the basic shape of the airship: the basic shape of the stratospheric airship is a typical oblong spiral body structure, select a certain spiral body contour curv...

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 provides a simulation method for strengthening and lightening an airship gasbag of a stratospheric airship, the stratospheric airship and a manufacturing method for the stratospheric airship. The simulation method comprises the following steps of (1), determining a basic shape of the stratospheric airship needed to be researched, and performing modeling on the shape; (2) performing simulation calculation to obtain airship gasbag surface stress distribution of the airship under a maximum overpressure condition; (3) according to related characteristics and a safety coefficient of an airship gasbag material, defining that an airship gasbag surface stress of the airship under the maximum overpressure condition is greater than a maximum safety stress, and serving as a reinforcement rib strengthening region; (4) selecting and using a proper reinforcement rib material to meet a lightweight requirement; arranging a plurality of reinforcement fiber ribs in circumferential and longitudinal directions in a simulated manner in the reinforcement rib strengthening region to strengthen the airship gasbag; and (5) after the airship gasbag is strengthened, performing simulation calculation again to obtain the airship gasbag surface stress distribution, and according to the maximum stress, selecting a proper low-density material to be applied to the airship gasbag.

Description

Technical field [0001] The invention relates to the technical field of a stratospheric airship, in particular to a simulation method for strengthening and lightweighting of a stratospheric airship capsule, a stratospheric airship and a preparation method thereof. Background technique [0002] A stratospheric airship is a lighter than air aerostat. It relies on air buoyancy to stay in the air, provides energy power for it through solar energy, and has a propulsion system. It can achieve vertical take-off and landing without relying on airports or runways, and can hover in the air. Over any geographical location, the operating altitude exceeds the air traffic control range, and is not affected by severe tropospheric weather. It can work continuously all day and all day, with strong load capacity, high cost-effectiveness ratio, and wide detection range. It has a wide range of national defense and civil applications. Application prospects. [0003] At present, stratospheric airships a...

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 Patents(China)
IPC IPC(8): G06F30/15G06F30/20G06F119/14
CPCG06F30/15G06F30/20Y02A90/10
Inventor 赵磊
Owner 北京天恒长鹰科技股份有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products