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

Flap rudder layout for enhancing rolling-control capability of hypersonic aircraft

A hypersonic, flap rudder technology, applied in the directions of aircraft, supersonic aircraft, aircraft control, etc., can solve the problems of flight control defects in the roll channel, unable to realize the roll control of the aircraft, etc., to improve the roll stability, The effect of improving the ability to avoid risk and the ability to maneuver

Inactive Publication Date: 2020-09-25
北京星途探索科技有限公司
View PDF3 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Theoretical studies have shown that when an axisymmetric aircraft adopts conventional symmetrically distributed flap rudders, since the normal force of the flap rudder surfaces passes through the aircraft axis, there are defects in the flight control of the roll channel, and the conventional symmetrically distributed flap rudder surfaces cannot achieve alignment. aircraft roll control

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
  • Flap rudder layout for enhancing rolling-control capability of hypersonic aircraft
  • Flap rudder layout for enhancing rolling-control capability of hypersonic aircraft
  • Flap rudder layout for enhancing rolling-control capability of hypersonic aircraft

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment approach

[0020] For the axisymmetric hypersonic vehicle with ball-cone-column configuration, a new flap-controlled rudder surface layout shape is invented. This layout not only has the characteristics of small aerodynamic interference, low thermal protection pressure, and high space utilization, but also can realize effective control of the three channels, especially the rolling channel. The features of the aircraft include: a spherical-cone-cylindrical axisymmetric fuselage; a flat flap rudder at the bottom of the fuselage; the flap rudder is connected to the bottom of the fuselage through the rudder shaft, There are different distances and installation angles. Outline diagram such as figure 1 shown. The specific implementation is as follows:

[0021] Firstly, the shape of spherical-cone-cylindrical axisymmetric fuselage is designed. By adjusting the length and angle of the cone section and the length of the column section, the stability and maneuverability of the axisymmetric air...

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 flap rudder layout for enhancing the rolling-control capability of a hypersonic aircraft is a layout form applied to a spherical-conical-cylindrical axisymmetric hypersonic aircraft, and the aircraft obtains a control moment through flap rudder deflection so as to control the flight attitude. The flap rudder is designed into a flat plate structure and is mounted at the bottom of the aircraft through a rudder shaft. The designed installation angle of the flap type rudder remarkably improves the rolling-control capacity of the aircraft, and effective distribution of pitching, yawing and rolling control efficiency of the aircraft is achieved.

Description

technical field [0001] The invention is applied to the aerodynamic shape design of hypersonic aircraft, and belongs to the field of aerodynamic layout design of hypersonic aircraft. Background technique [0002] Hypersonic aircraft has the characteristics of fast speed, strong defense penetration capability, and strong strike timeliness, and has become the focus of the development of major military powers in the world. In recent years, with the increasing maturity of missile defense technology, new requirements have been put forward for the maneuverability and rapid risk avoidance capabilities of high-speed sonic aircraft. Countries are actively developing new types of high-speed maneuverable hypersonic aircraft. [0003] For ball-cone-cylindrical hypersonic reentry vehicles, maneuvering flight is generally achieved by installing air rudders. The air rudder mostly adopts the empennage rudder or flap rudder scheme. Flap rudder has the advantages of small aerodynamic interfe...

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): B64C9/00B64C30/00B64F5/00G06F30/15
CPCB64C9/00B64C30/00B64F5/00G06F30/15Y02T90/00
Inventor 刘强梁建军赵新强孙永丰谢雪明陈景鹏
Owner 北京星途探索科技有限公司
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

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