Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Hydrodynamic force catapulting device of carrier-borne aircraft

A technology of catapult device and carrier-based aircraft, which is applied in the direction of launch/tow transmission device, etc., can solve the problems of high energy consumption, low utilization rate, large energy consumption, etc., and achieve the effects of high energy utilization rate, compact size and simple structure

Active Publication Date: 2018-10-16
BEIJING INST OF SPECIALIZED MACHINERY
View PDF6 Cites 13 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, carrier-based aircraft mainly adopt two methods of steam ejection and electromagnetic ejection. Among them, steam ejection needs to convert seawater into fresh water first, and then convert fresh water into high-pressure steam. In this process, energy consumption is large and the utilization rate is low. The volume of the device is huge, and the system structure is extremely complex. At present, only a few countries can master its core technology
Although electromagnetic ejection has the advantages of large thrust, low energy consumption, and high efficiency, it has irreparable shortcomings, that is, it will generate strong electromagnetic interference, which not only seriously affects the electromagnetic environment and working reliability of the electromechanical equipment on the aircraft carrier, but also is not conducive to the The maneuverability and stealth of the ship formation restrict its combat effectiveness to a certain extent
Therefore, how to develop a new type of carrier-based aircraft ejection device to overcome the shortcomings of steam ejection devices such as high energy consumption and complex systems, and to avoid problems such as strong electromagnetic interference generated by electromagnetic ejection devices, is of great importance to improving the take-off capability of carrier-based aircraft and The combat effectiveness of the aircraft carrier is of great significance

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
  • Hydrodynamic force catapulting device of carrier-borne aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0023] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0024] The invention provides a hydrodynamic ejection device for a carrier-based aircraft, such as figure 1 As shown, the device includes a hydraulic power source, a pressure storage tank, a traction system and a buffering and blocking system.

[0025] Wherein, the hydraulic power source includes a water tank 1, a filter 2, a first motor 3, a hydraulic pump 4, a first one-way valve 5, a second motor 6, a centrifugal pump 7, a first stop valve 8, a hydraulic pressure Relief valve 9 , first pressure gauge 10 , water pressure electromagnetic switch valve 11 , second stop valve 13 and pressure sensor 14 . Wherein, the hydraulic pump 4 is driven by the first motor 3, and the centrifugal pump 7 is driven by the second motor...

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 hydrodynamic force catapulting device of a carrier-borne aircraft and relates to the technical field of weapon launching. The medium state and energy conversion processes from seawater to fresh water and then from fresh water to high-pressure steam are not need for achieving the catapulting device, and a seawater medium in the ocean is directly used for transmitting energy and acting, so that the device is simple in structure, compact in size, low in energy consumption in the catapulting process and high in energy use rate. In addition, the catapulting device uses high-pressure seawater as catapulting power, no electromagnetic interference is generated, and invisibility of a naval ship and reliable and stable work of mechanical and electrical equipment on the naval ship are facilitated.

Description

technical field [0001] The invention relates to the technical field of weapon launching, in particular to a hydrodynamic ejection device for a carrier-based aircraft. Background technique [0002] Ejection devices (catapults) are widely used in the launching process of aircraft, especially for carrier-based aircraft based on aircraft carriers, the use of catapult devices can greatly shorten the running distance, increase the load and efficiency of take-off, and significantly improve the aircraft carrier. The maneuver reaction time and combat effectiveness of the carrier aircraft. [0003] At present, carrier-based aircraft mainly adopt two methods of steam ejection and electromagnetic ejection. Among them, steam ejection needs to convert seawater into fresh water first, and then convert fresh water into high-pressure steam. In this process, energy consumption is large and the utilization rate is low. The volume of the device is huge, and the system structure is extremely co...

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): B64F1/06
Inventor 张振华王海岳吴向阳李春萍王飞
Owner BEIJING INST OF SPECIALIZED MACHINERY
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
Eureka Blog
Learn More
PatSnap group products