The invention relates to a structure having a panel, a stringer and a rib. The stringer has a stringer flange that is joined to an inner surface of the panel and a stringer web that extends away from the stringer flange. The rib has a rib web and a rib foot. The rib foot has a ...
the wing is a framework composed chiefly of spars, ribs, and (possibly) stringers(see figure 1-5). Spars are the main members of the wing. They extend lengthwise of the wing (crosswise of the fuselage). All the load carried by the wing...
Ribs arethe structural crosspieces that combine with spars and stringers to make up the framework of the wing. They usually extend from the wing leading edge to the rear spar or to the trailing edge of the wing. The ribs give the wing its cambered shape and transmit the load from the s...
Aluminum is the material of flight, as it poses excellent strength/weight and can be readily shaped into virtually any form for ideal streamlined shape and more durable than wood. It could also be easily mass produced with stamped forms into ribs and formers which could be covered in fabric ...
Very straight forward, formers, stringers and very light weight. 35, shows the fuselage completed with the rudder assembly being placed. 37, 39 show the wing construction. this was a little complicated as the wing is built upside down and the placement of the first three ribs and surrounding...
The obvious advantages of these materials lie in the structural weight savings over metals, possible through their higher ratios of strength and stiffness to weight. For compression panels and shear webs, which representprincipal componentsof the primary structure of wings, spars, and ribs, weight sa...
aFor the very repetitive Non-Specific Design components of aircraft,Fuselage Stringers, Frames, Panels, Wing Ribs, Skins, Spars etc. a lot of Certified and Test Validated Analytical Methods are used. 为航空器、机体纵梁、框架、盘区、翼肋骨、皮肤,晶石等非常反复未指明的设计组分。 使用很多被证明的...
aFor the very repetitive Non-Specific Design components of aircraft, Fuselage Stringers, Frames, Panels, Wing Ribs, Skins, Spars etc. a lot of Certified and Test Validated Analytical Methods are used. 为航空器、机体纵梁、框架、盘区、翼肋骨、皮肤,晶石等非常反复未指明的设计组分。 使用很多被证明...
The numerical procedure implemented obtains the optimal number of ribs per wing box (main and trailing), the optimal number of stringers per rib bay, and optimal sizing of all structural components (skin, spars, ribs and stringers). This procedure guarantees that acceptable margins of safety and...
wing bearing components: skin, spars, stringers and longitudinal wall ribs. 27. the force forms of wing: beam type: single beam structure; double beam structure; multi beam whole type; single block type; multi abdominal wing 28. wing lift devices: plain flaps, split flaps, leading edge ...