Unlock instant, AI-driven research and patent intelligence for your innovation.

Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element

A technology for installing fixtures and fuselage frames, applied to fuselage frames, aircraft parts, fuselages, etc., can solve the problems of unfavorable manufacturing time and cost, and difficulty in completing other assembly tasks at the same time, so as to achieve low total manufacturing costs and reduce machine costs. The effect of creating time and reducing quantity by itself

Inactive Publication Date: 2015-02-11
AIRBUS OPERATIONS (SAS)
View PDF4 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Then, when the operator installs and attaches these clamps, it can prove difficult to simultaneously complete other assembly tasks from inside the section, which constitutes another factor that is detrimental to manufacturing time and cost

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
  • Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element
  • Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element
  • Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0043] First refer to figure 1 , shows a commercial airliner 1 with a fuselage 2 part of which is at figure 2 is shown in more detail in , where the fuselage section 2 is viewed from the inside of the passenger aircraft.

[0044] The fuselage 2 generally includes a skin 3 and a fuselage frame 4, the inner surface 3a of the skin 3 supports the fuselage frame 4 in a fixed manner, and a single fuselage frame in the fuselage frame 4 is figure 2shown in . This frame 4 extends over all or part of the periphery of the fuselage in a transverse plane of the aircraft, ie a plane orthogonal to the direction 6 corresponding to the longitudinal and axial direction of the passenger aircraft. Each frame may be made in one piece or formed using several frame elements / sections each of which forms only a single corner sector of the frame, wherein these elements are then end-to-end Assemble end-to-end. The frame elements generally extend over an angular sector of the order of 30° to 120°. ...

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

To reduce the time and cost of manufacture of an aircraft fuselage, the subject matter disclosed herein provides a tool for positioning mounting clamps to attach a fuselage frame element on to a fuselage skin and / or on to stiffeners. According to the subject matter disclosed herein, the tool includes a ramp and several systems for holding clamps in position distributed along the ramp, where each system includes a mobile device for applying pressure to the clamp, together with an adjustment device coupled to the mobile device such that its separation from the ramp is adjustable.

Description

technical field [0001] The present invention relates to the field of aircraft fuselages and in particular to the field of positioning mounting fixtures for attaching aircraft fuselage frame elements to fuselage skins and / or to attachments fitted to the fuselage skins. Leather stiffeners. [0002] The invention finds particular, but not exclusive application in the field of commercial airliners. Background technique [0003] Aircraft fuselages are designed to withstand the loads caused by pressurization as well as the loads transmitted by the engines. [0004] To achieve this, the fuselage usually consists of a circumferential frame, also called a "ring frame", and an aerodynamic skin, sometimes called a "self-stiffening skin", attached to these circumferential frames And fitted with generally longitudinally extending stiffeners attached to the inner surface of the skin and commonly referred to as "stringers". [0005] The stringers can have different types of sections, fo...

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): B25B11/00
CPCB64C1/06B64F5/0009B64F5/10B64C1/061B64C1/12Y10T29/49826Y10T29/53978
Inventor 扬妮克·马林达米安·吉约托
Owner AIRBUS OPERATIONS (SAS)