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

Mechanical-pneumatic composite vectoring nozzle with short distance/vertical take-off and landing function

A vector nozzle, vertical take-off and landing technology, applied in the direction of machines/engines, jet propulsion devices, etc., can solve the problems of complex nozzle structure, difficult maintenance, difficult control, etc., to reduce the number of parts and adjust the complexity, response The effect of high speed and less mechanical structure

Active Publication Date: 2021-12-14
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF8 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The structure of the traditional STOL / VTOL nozzle is complex, and the mode switching process is difficult to control and difficult to maintain

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
  • Mechanical-pneumatic composite vectoring nozzle with short distance/vertical take-off and landing function
  • Mechanical-pneumatic composite vectoring nozzle with short distance/vertical take-off and landing function
  • Mechanical-pneumatic composite vectoring nozzle with short distance/vertical take-off and landing function

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0056] The calculation is carried out for a mechanical-pneumatic composite vectoring nozzle with vertical take-off and landing function in a typical configuration.

[0057] Figure 6 , Figure 7 What is shown is a specific embodiment of using a mechanical disturbance type throat offset type aerodynamic vectoring nozzle. in, Figure 6 Shown is the internal flow field of a nozzle with no disturbance applied near the throat. It can be seen that the present invention cannot realize the turning of the airflow beyond 95° at this time, thus vertical take-off and landing cannot be realized. But when the spoiler that controls the bowing direction is stretched out, so that the vector nozzle produces the airflow deflection in the bowing direction, the present invention obviously produces a deflection of more than 95°, specifically as Figure 7 As shown, the vertical take-off and landing function is realized. Therefore, for the present invention, it is necessary to generate a real-ti...

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 mechanical-pneumatic composite vectoring nozzle with short-distance / vertical take-off and landing functions, which includes an aerodynamic steering section and a mechanical steering section; Nozzle and transition section; mechanical steering section includes cylinder A, cylinder B, bearing A, bearing B; along the fluid flow direction, cylinder A, bearing A, cylinder B, bearing B, transition section, axisymmetric / quasi The inlets of the axisymmetric throat offset aerodynamic vectoring nozzles are sequentially connected. Through the relative rotation of the two bearing mechanisms and the aerodynamic steering of the throat offset pneumatic vectoring nozzle, the function of airflow deflection exceeding 90° is realized without the mechanical structure deflecting by 90°, and the pneumatic vectoring nozzle can be used in the suspension Attitude control is carried out in the stopped state, which assists the continuous change of key parameters such as lift, thrust and vector angle of the entire exhaust system. It has many characteristics such as simple structure and relatively few motion mechanisms.

Description

technical field [0001] The invention relates to a mechanical-pneumatic composite vectoring nozzle with short-distance / vertical take-off and landing functions, and belongs to the technical field of advanced thrust vectoring nozzles of aero-engines. Background technique [0002] With the development of science and technology and the urgent needs of practical applications, short-distance / vertical take-off and landing aircraft have once again entered people's field of vision. The structure of the traditional ST / VTOL nozzle is complex, and the mode switching process is difficult to control and difficult to maintain. Therefore, it is necessary to develop a STOL / VTOL exhaust system with simple structure, light weight, good performance, and meeting the needs of high-speed flight. [0003] At present, the fluid thrust vectoring nozzle has gradually become the research focus and research focus of various countries due to its simple structure and light weight, and will enter engineeri...

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): F02K1/00F02K1/78
CPCF02K1/004F02K1/78
Inventor 黄帅徐惊雷潘睿丰张玉琪宋光韬陈匡世曹明磊成前
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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

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