Презентация на тему: «ANSAT Helicopter»
«ANSAT Helicopter»
Key dates 1995 – development star 17 августа 1999 года – first flight 2002 – certification test flights 2004 – type certificate 2005 – type certificate for two pilot helicopter 2005 – supplementary certificate for emergency splashdown system Aerazur 2005 – serial production start
Key dates
Main technical characteristics
Main flight performance
Power plant Comprises of two PW-207K engines with single-stage centrifugal compressor and single-stage axial turbine of gas generators Digital electronic regulators (FADEC) ensures continuous rotation speed of main rotor Emergency mechanical system of manual control is available Electric start-up in automatic or manual modes
Cockpit
Control system – hydromechanical control system СВА Flexball control linkage Applied by: Eurocopter (EC120, Ecureuil, Dauphin, Super Puma, EC155, EC175 , EC135, EC145, NH90), Airbus (A320, A330, A380), Dassault Aviation (Falcon family)
Control system – hydromechanical control system Main and tail rotor mechanical control system with the use of CBA Flexball flexible control linkage is developed
Fly-by-wire Control system
Main rotor
Onboard information check system
Operational features Features of Ansat operation by Forestry Aviation of South Korea Monitoring of forests, fire-fighting and pest control Most of the sorties performed at economical speed Performs terrain following flights in mountainous areas
Operational experience
Ansat - U
Operation of Ansat - U
Total flight hours
Assigned service life
Ground support facilities
Training Complex - Structure
Training complex visual aid
Training complex – training computer class
Procedural simulator
Flight simulator
ILS. Development prospects
Configurations
Functionality
Why Ansat
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