Torsion type aircraft control human sensing mechanism with adjustable starting torque and adjusting method

A technology of aircraft control and starting torque, which is applied in the design field of aircraft control human-sensing system, can solve the problems of increasing the volume and weight of the mechanism, complicated adjustment of the starting force, and difficult to adjust accurately, so as to reduce the volume and weight of the mechanism, use fewer parts, cost reduction effect

Pending Publication Date: 2020-05-05
LANZHOU FLIGHT CONTROL
View PDF13 Cites 1 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is: aiming at the deficiencies in the adjustment of the force-sensing actuation force of the existing aircraft control twisting body type, a twisting-type aircraft control human-sensing mechanism and adjustment method with adjustable starting torque are proposed to solve the problem of the existing torsion body force. The actuation for

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
  • Torsion type aircraft control human sensing mechanism with adjustable starting torque and adjusting method
  • Torsion type aircraft control human sensing mechanism with adjustable starting torque and adjusting method
  • Torsion type aircraft control human sensing mechanism with adjustable starting torque and adjusting method

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0026] See attached Figure 1 to Figure 6 , Provide a specific embodiment: a torsion-type aircraft manipulation human-sensing mechanism with adjustable starting torque and an adjustment method, including a rotating shaft 1, a first adjustment disc 2, a torsion body 3, a second adjustment disc 4, and an anchor disc 5.

[0027] The circular peripheries of the first adjustment disc 2 and the second adjustment disc 4 respectively have first circular arc protrusions 1a and second circular arc protrusions 2a along the axial direction on the side surfaces, and first counterbores 2c on the other side surfaces. And the second counterbore 4c, the first adjustment disc 2 and the second adjustment disc 4 have 3 counterbore groups, each counterbore group is evenly distributed on the circumference with an interval of 120°, each group has 5 The torsion body 3 is formed by machining a spiral groove on the cylindrical surface of the annular structure by machining to form the torsion body 3, and t...

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 belongs to the technical field of airplane control human sensing system design and particularly relates to a torsion type airplane control human sensing mechanism with the adjustable starting torque and an adjusting method. At present, the torsion body type force sensing starting force is not easy to accurately adjust, the number of machined parts is large, a large number of materials are consumed, moreover, the size and the weight of the mechanism are increased, and starting force adjustment is complex. The mechanism is characterized in that a plurality of counterbores are formed in the circumferential direction of a first adjusting disc and the circumferential direction of a second adjusting disc, and the first adjusting disc and the second adjusting disc are respectively provided with a second arc protrusion and a third arc protrusion; the torsion body has torsion elasticity, and a plurality of threaded holes are formed on end faces of two sides of the torsion body; and a rotating shaft sequentially penetrates through the first adjusting disc, the torsion body, the second adjusting disc and an anchoring disc. The mechanism is advantaged in that by adjusting different installation angle positions of the first adjusting disc and the second adjusting disc on the torsion body, adjustment of the force sense starting force of the aircraft control torsion body is completed accurately, easily, conveniently and efficiently, the number of used parts is small, reliability is high, consumed materials are small, the size and weight of the mechanism are reduced, and costis reduced.

Description

technical field [0001] The invention belongs to the technical field of aircraft control human-sensing system design, and in particular relates to a torsion-type aircraft control human-sensing mechanism and an adjustment method with adjustable starting torque. Background technique [0002] The artificial sensory force system is set in the control system of the modern aircraft cockpit to provide control force simulation, so that the pilot can intuitively feel the state of the aircraft, and avoid the pilot's misoperation affecting the safety of the aircraft and the quality of flight control. The artificial sensory force system needs to have a centering function, so it is necessary to set a certain preload force, that is, the starting force, for the spring of the artificial sensory force system. When the pilot's control force on the control stick is greater than the starting force, the control signal is output. In order to ensure the accuracy of the starting force, it is necess...

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): B64F5/00B64C13/04
CPCB64F5/00B64C13/042Y02T50/40
Inventor 李建黄志毅任省伟孙自军
Owner LANZHOU FLIGHT CONTROL
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
Try Eureka
PatSnap group products