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Barry Hill Palmer
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Barry Hill Palmer : ウィキペディア英語版
Barry Hill Palmer

Barry Hill Palmer (born November 10, 1937) is an American aeronautical engineer (UC Berkeley, 1961), inventor, builder and pilot of the first hang glider based on the Rogallo wing or ''flexible wing''. Palmer also designed, built and flew the first weight-shift ultralight trike aircraft.
==Inventor of the first Flexible Wing hang glider==

On August 1961 Barry Palmer first saw a photo of the Rogallo wing mounted on the Fleep experimental aircraft published in the Aviation Week magazine and became interested in this flexible wing because of its light weight and simplicity.〔August 14, 1961 by Aviation Week & Space Technology magazine.〕
In October 1961 he completed construction and flew the first flexible wing hang glider; this took place near Latrobe, east of Sacramento, California.〔His first hang glider cost him only $10.89 USD. Article by Barry H. Palmer published in February 1969 by ''Sport Aviation'' magazine. Barry Palmer’s web site, dated photos:().〕 He used polyethylene sheet, aluminum tubing and no wires for construction as he did fear kinking during assembly and transport. Most flights were performed with just a set of inclined parallel bars that split his weight between his underarms and hands to experiment with the center of gravity and thus he demonstrated that the Rogallo wing, when used as a hang glider, could also be controlled by shifting weight alone. Palmer, who built the first modern-age foot launched hang glider, is not yet mentioned by the FAI.
Palmer experimented with about 8 different hang glider versions and their wings were mostly 90 degree swept back wings. His smallest glider weighed , and had a surface area of . The flexibility in the frame caused no performance problems. His first and largest hang glider was about 45 pounds and had a surface area of . Palmer explored control of his several versions of hang gliders by using different control frames: pilot in front of the control frame, pilot behind the control frame, and control frame in front of the pilot in a swing seat, which inadvertently approximated the George A. Spratt mechanism from 1929. NASA’s Paresev glider came to light after Palmer’s gliding flights, so it bore no influence on him.
During the period from 1961 to 1963 Barry Palmer made tens of flights using the Rogallo wing concept. His flights were usually long and his longest flight was about . He flew at altitudes up to . His best glider had an overall glide ratio of 4.5 to 1 at the speed of 29–32 km/h (18–20 miles/h). The last of Palmer’s hang gliders flew in the summer of 1963 and it had a single point suspension ski-lift type of seat mounted to the keel with a universal joint; the seat could be forced fore and aft, and laterally, but allowed for no twisting of the seat relative to the wing due to lateral stick movement. That is why a single control stick could be used to replace the control frame.
Palmer relates that he had a good paying aerospace job at the time and he was flying on a minimalist and inexpensive glider purely for curiosity and fun. He did not attempt to modernize or market the flexible wing hang glider; there was no attempt to publicize on the media, except for an 'accidental' report made by a small local newspaper.〔''San Juan Record'' newspaper, published out of Fair Oaks, California. Thursday March 15th, 1962. Scan: ()〕 In fact, Palmer concealed his efforts to the American aviation bureaucracy (FAA) of flying without credentials in a pre-ultralight era, but freely gave information about the wing to any person interested, including Francis Rogallo〔Interview with Gerard Farell on 1/23/2007 – 1/24/2007.〕〔(Letter from Francis Rogallo to Barry Palmer (October4/1962) )〕 and Richard Miller, who develop the famous ''Bamboo Butterfly'' Rogallo wing hang glider, the plans of which circulated in some American magazines in the mid 1960s; Tara Kiceniuk's followed with plans for the bamboo ''Batso'' Rogallo wing.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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