PROBLEM TO BE SOLVED: To provide an assembling method of an aircraft wing which does not require a large amount of tooling, can cope with an increase in tolerance due to application of composite materials, and is adaptable to horizontal assembling.SOLUTION: Tooling components 11, 12 include: ...
At least some of the ribs are joined to the cover at their end regions so that the wing can be assembled and dismantled by sliding the cover along the longitudinal axis (10) of the spar. Independent claims are also included for the following: (A) a hang glider, ultra light aircraft, ...
In this case, I used 1/8" aircraft plywood. Take your time shaping the templates to make them as accurate as possible. Depending on how you do things, it may or may not be important that the centerlines of the ribs are aligned to one another as they will ...
The double decker or biplane wing is for an aircraft. The upper and lower surfaces of the wing form part of a common aerofoil contour. The two surface (2,3) are connected to each other by a number of vertical ribs which extend from the leading edge to the trailing edge. The leading ...
Fuselage frames and wing ribs 来自 Elsevier 喜欢 0 阅读量: 58 作者: THG Megson 摘要: Aircraft are constructed primarily from thin metal skins which are capable of resisting in-plane tension and shear loads but buckle under comparatively low values of in-plane compressive loads. The skins are,...
Fuselage Frames and Wing Ribs 来自 ResearchGate 喜欢 0 阅读量: 48 作者: THG Megson 出版社: Elsevier Ltd 摘要: Aircraft are constructed primarily from thin metal skins which are capable of resisting in-plane tension and shear loads but buckle under comparatively low values of in-plane compressive...
Various multi-disciplinary analysis optimization (MDAO) tools have been developed by the aeronautical industry to enhance the aircraft design process. These tools usually function as stand alone applications and encompass the analysis tools needed for evaluating the structural responses, the constraints, ...
The air is distributed on a whole length of a front edge by the air distribution window. The air is blown with high speed from the drain system through the gaps over an upper surface of the wing to produce a hyper-buoyancy force using a coanda-effect....
Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs This dissertation investigates the advantages of using curvilinear spars and ribs, termed SpaRibs, to design supersonic aircraft wing-box in comparison to the use of classic design concepts that employ straight spars and ribs. The...
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