Aeroscout UAV Rotor Blade
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Aero oscout GmbH H Technikum mstrasse 21 1 6048 Horw w Switzerland S d pho one: +41 41 349 33 85 1 5 f fax: +41 41 349 36 37 1 7 emai il: info@ae eroscout.ch h w web: www.ae eroscout.ch h Scout B 00 UAV B1-10 High Ef hly fficien Carbon Main Roto Bla nt n or ades GENERAL T autono The omous indu ustrial unm manned hel licopter Sco B1-100 has been developed out d for profess sional airborne applic cations suc as aeria mapping, airborne broadcasti ch al ing, search h & rescue, surveillanc and insp ce pection as w as law enforceme well ent. HIGHLY EF FFICIENT CA ARBON MAIN ROTOR B BLADES The new carbo main rot blades developed e on tor d by Aeroscout GmbH are highly efficient a s they are reducing the average power consumption e n during the flight by m e minimum 10% compa ared to the standard main rotor b m blades. The decrease e e of power c consumptio is directly indicate on the power/carb on ed buretor ind dicator on the ground t d control sta ation. SAFTEY Th state-of he f-the-art carbon main rotor blad are pr n des roduced in dustrially with latest w t carbon mu ulti-cross-la ayer techno ology using autoclave fabrication The static tensile st g n. c trength has s been verif fied by a fa actor of thr relative to the nominal oper ree e ration for th Scout B1-100 UAV he B V helicopter r. DESIGN Th highly e he efficient car rbon main rotor blade have been designe specifically for the es ed e operation on the Sco B1-100 UAV helico out opter considering tak ke-off weigh main ro speed, ht, otor , main rotor diameter and physical operati modes of the Sco B1-100 UAV helico r ion out opter while e optimizing lift efficie g ency, aerod dynamic d rag, and continuousn c ness of the angle of attack. In e f n addition, t these blade have sup es perior beha avior under extreme maneuvers. r m UPGRADIN Due to t industr product NG the rial tion proces the new carbon ma rotor bl ss ain lades have e long-life e endurance a can be used imm and e mediately with the same main r w rotor speed controller d r settings. F Furthermore, only small mechan nical modif fications are required when mo d ounting the e new carbo rotor blades. on DEMONST TRATION System demo onstrations are availab on requ in Luce ble uest erne, Switzerland. Subject to change witho out notice. © Aeroscout GmbH 2013, Switzerland

High Ef ent C on Main R r hly fficie Carbo Rotor Blad f th Sc des for he cout B1-10 U 00 UAV TECHNICAL DATA Main rotor diameter r Weight per blade (ap pprox.) Material Nominal m main rotor s speed Performan increase (reduced power con nce nsumptioni) Tensile str rength testi ing 3. m .2 1.5kg Ca arbon (mullti-layer) 86 rpm 60 >1 10% Zw Z150 k wick kN FEATURES  No modification for the rpm control settings required r ller s g  Hig ghly efficien and effec nt ctive movem ments of th helicopter including extreme maneuvers he m s  Increased saf fety margins for custom s mers with heavy and/or...