发明名称 LIGHTWEIGHT AMPHIBIAN AIRCRAFT
摘要 FIELD: aviation. ^ SUBSTANCE: invention can be applied in amphibian and hydroplane aircraft design. Lightweight amphibian aircraft comprises a boat with lengthwise and transverse steps and shoulders, and engine with a pusher placed above the cockpit. Deflectors are attached between the boat steps. The aircraft has a water-rudder and empennage group with stabiliser at the keel, as well as retractable tricycle-equipped landing gear with a nose strut and a wing. Pylons with wing-tip floats are attached to at the end of the wing. Transverse shoulder of the boat comprises two levels, with possible installation of mounting fittings of main landing gear at the second level. The wing is attached at the boat top by a scheme similar to high-wing aurcraft. ^ EFFECT: improved flight, takeoff and landing performance of an aircraft. ^ 7 dwg
申请公布号 RU2328413(C1) 申请公布日期 2008.07.10
申请号 RU20060140325 申请日期 2006.11.15
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO TAGANROGSKIJ AVIATSIONNYJ NAUCHNO-TEKHNICHESKIJ KOMPLEKS IM. G.M.BERIEVA 发明人 KOBZEV VIKTOR ANATOL'EVICH;KRAVTSOV VALENTIN NIKOLAEVICH;SOKOLJANSKIJ VLADIMIR PETROVICH;PARFENOV ALEKSEJ ALEKSANDROVICH;OGOLEV JURIJ ANDREEVICH
分类号 B64C35/00 主分类号 B64C35/00
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