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

Heat returning closed cooling recirculation system of Brighton scramjet

A technology of engine cooling and scramjet, which is applied to ramjet engines, machines/engines, rocket engine devices, etc., and can solve the problems of scramjet cooling difficulties, fuel supply system gas intake difficulties, and large cooling fuel flow, etc. problems, to achieve the effect of improving energy utilization, good component matching performance, and good heat absorption performance

Inactive Publication Date: 2009-11-11
HARBIN INST OF TECH
View PDF1 Cites 20 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to solve the problems of the existing hypersonic vehicle scramjet cooling difficulties, large cooling fuel flow, insufficient heat sink and difficulty in getting gas from the fuel supply system, and proposes a regenerative closed layout Layton scramjet cooling cycle system

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
  • Heat returning closed cooling recirculation system of Brighton scramjet
  • Heat returning closed cooling recirculation system of Brighton scramjet

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment approach 1

[0009] Specific implementation mode one: combine figure 1 To illustrate this embodiment, the cooling cycle system includes a compressor 1, an engine 3, a cooling passage 4, a turbine 5, a fuel tank 7, a fuel pump 8 and a central shaft 10, and the cooling cycle system also includes a regenerator 2, a heat exchanger Heater 6 and generator 9, one end of described central shaft 10 is connected with generator 9, and the other end of described central shaft 10 is connected with air compressor 1 and fuel pump 8 respectively, and described turbine 5 is contained in generator 9 and On the central axis 10 between the compressors 1, the cooling channel 4 is arranged on the outer wall surface of the upper part of the engine 3; the output end of the compressor 1 is connected to the cold side input end of the regenerator 2 through a pipeline, The output end of the cold side of the regenerator 2 is connected to the input end of the cooling passage 4 through a pipeline, the output end of the ...

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 discloses a heating returning closed cooling recirculation system of a Brighton scramjet, which relates to a cooling recirculation system of a scramjet. The invention aims at solving the problems of cooling difficulty, a large amount of cooling fuel flow, insufficient heat sink and gas-fetching difficulty of the fuel supply system of the scramjet of a prior hypersonic aerial vehicle. One end of a central axis is connected with a generator and another end thereof is respectively connected with a gas compressor and a fuel pump. A turbine is arranged on the central axis between the generator and the gas compressor. A cooling channel is arranged on the external wall at the upper part of the scramjet. The cooling recirculation system is provided with a primary cooling loop and a secondary cooling loop. The cooling recirculation system of the scramjet is applicable to the thermal protection of the hypersonic aerial vehicle and the cooling of the scramjet.

Description

technical field [0001] The invention relates to a cooling cycle system of a scramjet engine. Background technique [0002] Hypersonic vehicles with a flying Mach number greater than 5 are a hot topic in current research, including the development of single-stage or two-stage orbital space planes, space-to-ground transport vehicles, and hypersonic cruise missiles. One of the key technologies of the air-breathing hypersonic vehicle with the scramjet engine as the propulsion system is the thermal protection of the vehicle, in which the cooling of the engine is the most difficult part, because even if composite materials are used, it is difficult to withstand the huge heat generated inside the engine. heat load. It is generally believed that fuel is the best coolant, but theoretical analysis and practice show that the coolant flow rate will be greater than the propulsion fuel flow rate after reaching a certain flight Mach number, so extra fuel has to be carried, and the excess ...

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
IPC IPC(8): F02K7/10F02K9/64
Inventor 鲍文秦江于达仁周伟星
Owner HARBIN INST OF TECH
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com