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

Method for docking framework with airplane

A frame and rigid frame technology, used in aircraft parts, ground installations, transportation and packaging, etc., can solve the problems of poor flexibility and sealing, hidden dangers, damage to the fuselage shell, etc., and achieve good sealing and overload prevention. Effect

Active Publication Date: 2013-03-27
LIYANG TECH DEV CENT
View PDF10 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The above two documents are still relatively single for the use of laser rangefinders
[0006] Therefore, the method for deploying the canopy device in the prior art generally has the following defects: due to the single force point of the energy storage device or the actuator, the flexible frame is difficult to adapt to various aircraft surface curvatures, and the flexibility and sealing performance are relatively poor; Fitting the flexible frame tightly to the fuselage shell usually requires a relatively large force, which is easy to damage the fuselage shell. In addition, since the energy storage device or actuator usually starts to work after the awning device touches the fuselage shell, it is easy to Due to its own failure or system error, the overload caused serious damage to the fuselage shell; the lack of real-time detection and alarm devices during the passenger boarding process has potential safety hazards

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
  • Method for docking framework with airplane
  • Method for docking framework with airplane
  • Method for docking framework with airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0015] Refer to attached figure 1 , which shows an awning device 1 according to the present invention, the awning device 1 includes a door frame 2 and a docking frame 3, the docking frame 3 is directly used to realize the docking of the awning device 1 and the aircraft fuselage shell. The docking frame 3 includes a rigid frame 4 and a flexible frame 5 that will be in direct contact with the fuselage shell. The flexible frame 5 is made of flexible material, but the material has poor ductility, such as plastic. The flexible frame may further include cushioning materials, air cushions or elastically deformable tubes, etc. around the flexible frame. The canopy device further comprises a floor 6, wherein the floor is a retractable floor comprising a telescoping portion 11 by means of, for example, an actuator inside the floor, such as a hydraulic actuator. 12 to realize telescopic movement, the hydraulic actuator 12 may be one that is arranged in the middle of the floor, or two th...

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 method for docking a framework with an airplane and provides an unfolding method of an awning device. The method comprises the following steps of: starting laser range finders to measure distances from a flexible framework to an airplane body, and when a boarding bridge advances towards the airplane vertically and approaches the airplane to be docked by a certain distance, temporarily stopping the motion of the boarding bridge approaching the airplane; controlling the deformation of the flexible framework by using the distances measured by the plurality of laser range finders and by actuators so as to make the deformed flexible framework achieve the same surface curvature as that of a casing of the airplane body to be docked; continuously controlling the boarding bridge to advance, braking the boarding bridge when the distance measured by the laser range finder at the front end of a floor reaches a preset value; and controlling a winding mechanism to release an energy storage device by a controller so as to tightly press a docking framework to fit the casing of the airplane body. By utilization of the unfolding method of the awning device, disclosed by the invention, the tightness and safety are improved.

Description

technical field [0001] The present invention relates to a method for docking a frame with an aircraft, in particular to a method for deploying an awning device, in particular to an awning including a docking frame that can adaptively have a shape conforming to the curvature of the surface of the aircraft before docking with the aircraft. How to deploy the canopy. Background technique [0002] Airplane boarding bridge is a piece of airport equipment commonly used by modern passenger aircraft. They are used as the entrance for boarding, allowing passengers to enter the interior of the passenger aircraft from the terminal building. This type of boarding bridge usually has a canopy device at its end, which bridges the space between the boarding bridge and the aircraft, so as to protect the boarding personnel from the influence of bad weather conditions. [0003] Patent document CN100355628C discloses a sealing device for aircraft passenger ladders or aircraft boarding bridges, ...

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): B64F1/305
Inventor 狄睿狄春保
Owner LIYANG TECH DEV CENT
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