Transcription of 19. Case Study of Aircraft Wing Manufacture 1
{{id}} {{{paragraph}}}
Example: marketing
19. Case Study of Aircraft Wing Manufacture 1
9/ 22/ 031 Macintosh HD:Final book 16-19:Chapter 19 767 Case Case Study of Aircraft Wing Manufacture1 Yeah. If that alignment is off, engineering comes down and designs usa shim. We have to wait 24 hours while they do the calculations. When theline is supposed to move every three days, that s a disaster. A. IntroductionThis chapter brings together most of the knowledge contained in priorchapters and shows how it was applied to the design of a proposed newassembly technique for a wing subassembly for a commercial Aircraft . We willsee in this chapter the application of Key Characteristics, the Datum FlowChain, analysis of constraints and tolerances, and economic analysis.
tension loads. In the 1920s, metal began to be used for aircraft structure. A metal wing is a box structure with the skins comprising the top and bottom, with front and back formed by I-beams called spars, interior fore-aft stiffeners called ribs, and in-out stiffeners called stringers. In level flight, the lower skin is in
Tags:
Information
Domain:
Source:
Link to this page:
Please notify us if you found a problem with this document: