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Download e-book for kindle: Aircraft Landing Gear Design: Principles and Practices (AIAA by Norman S. Currey

By Norman S. Currey

This is often the single e-book on hand this day that covers army and advertisement airplane touchdown equipment layout. it's a finished textual content that may lead scholars and engineers from the preliminary techniques of touchdown equipment layout via ultimate element layout. The ebook presents an important hyperlink in touchdown equipment layout expertise from historic practices to fashionable layout traits, and it considers the mandatory airfield interface with touchdown equipment layout. The textual content is sponsored up by means of calculations, requirements, references, operating examples.

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At this point, no thought is given to kinematics, structural sizing, or brake requirements. " The following paragraphs represent a typical step-by-step approach that would be taken by the landing gear designer. Landing Gear Location Referring to Fig. 1, step I involves superimposing the M A C on an aircraft side and plan view. ) limits on the MAC. These limits arc obtained from the 25 26 AIRCRAFT LANDING GEAR DESIGN c. G,. (-) = _2, c . g. g. 55 MAC Frame a~ded and gear moved aft since abov location does not allow 15 deg angle with satisfactory tail-down angle e Use 12-15 deg initially -lr--'-" (LG at static) 15 d e g ~ STEP 6 Fig.

Among these characteristics are the maximum gross weight and the mean aerodynamic chord (MAC) location. At this point, no thought is given to kinematics, structural sizing, or brake requirements. " The following paragraphs represent a typical step-by-step approach that would be taken by the landing gear designer. Landing Gear Location Referring to Fig. 1, step I involves superimposing the M A C on an aircraft side and plan view. ) limits on the MAC. These limits arc obtained from the 25 26 AIRCRAFT LANDING GEAR DESIGN c.

The answer is controlled to some extent by the anticipated stowage concept. For instance, the C-130 uses two very large tires on each side of the aircraft; they are placed in tandem and the fuselage pod can be relatively slim. If a four-wheel bogie had been used, the pod would have been f a t t e r - e v e n though the tire sizes might have been smaller. As aircraft approach 500,000 lb, runway loading becomes more important, a factor that cannot always be sufficiently alleviated by merely increasing the tire size or number of tires per strut.

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