Transport helicopter U-100

piston enginesingle-rotor0 - 100km

The U-100 helicopter uses a high-performance horizontally opposed twin-cylinder two-stroke piston liquid-cooled gasoline engine for aviation . The engine cam is imported from Germany , and the ignition control part is all independently developed . The carburetor and power characteristics are customized for this model . It has low vibration, high power, low fuel consumption, high reliability and long service life. After 418 hours of single-machine flight , the maximum take-off weight can still be greater than 105 kg, which is no different from a new aircraft . The following is a photo of the actual time recorded by the console timer : The engine has its own starting system, which can be started with one button, eliminating the trouble of carrying a starter with you. Remote start can also be installed as needed. The start button has anti-foolproof and speed limit protection to prevent accidental start and sudden rotation of the rotor . The engine has its own power generation system with a maximum power of 230W . In addition to meeting the power supply needs of the aircraft itself , it can also meet the power supply needs of most mission loads, eliminating the need for charging and maintenance of the onboard power supply. The aircraft power supply uses the current advanced and highly safe lithium iron phosphate battery and dual redundant power supply system, eliminating the need to worry about the safety of power use and storage. 2. Aircraft consistency and reliability The aircraft has undergone durability testing, and the longest cumulative flight time of a single aircraft is 418 hours . .