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Shandong coax heli China Coaxial Single Seater [18] Guo Leiting's Coax China Yuncheng Farmer's Chopper Shantou Copters China Homebuilt Helis by Farmer Chen Ruihua Jiangsu China Coaxial Single Seater [19] Coaxial heli Zhuzhou China Coaxial Single Seater [20] Agricultural coaxial heli China [21] Red Coaxial Helicopter China Coaxial Single Seater [22]
A coaxial-rotor aircraft is an aircraft whose rotors are mounted one above the other on concentric shafts, with the same axis of rotation, but turning in opposite directions (contra-rotating). This rotor configuration is a feature of helicopters produced by the Russian Kamov helicopter design bureau .
The Livella Uno was designed to comply with the US FAR 103 Ultralight Vehicles and the European 120 kg class ultralight aircraft rules. It features a dual coaxial main rotors, with an inverted V-tail, a single open-air pilot's seat without a windshield, tricycle landing gear and a 40 hp (30 kW) Wankel Aixro XH40 engine.
Climb and descent is controlled by increasing and decreasing the throttle. The aircraft lacks a tail rotor, as the coaxial, contra-rotating main rotors produce zero net torque. Yawing motion is produced and controlled by electronic gyroscopically-controlled differential electric braking of the main rotors. With its empty weight of 70 kg (154 lb ...
The VA115 features dual, coaxial main rotors with NACA 23012 airfoils, a single-seat open cockpit without a windshield, tricycle landing gear and a two-cylinder, air-cooled, two stroke, fuel-injected 50 hp (37 kW) Hirth F23 engine. [1] The aircraft fuselage is made from metal tubing, with a small cockpit fairing. Its dual two-bladed rotors each ...
The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).
Single seat helicopters are helicopters have one place. A commonly known type of the helicopter that must be single seat, is the FAA Ultralight Helicopter, though single place helicopters existed before this classification (See Ultralight aircraft (United States))
The single-engine aircraft has twin three-blade coaxial rotors. [2] The most likely western powerplant is the Safran Arrius . [ 8 ] It features shaped carbon fiber main blades to cut noise emissions, composite construction, a glass cockpit and sliding rear cabin doors, and will compete with the Bell 505 and Robinson R66 . [ 9 ]