PATENTS

 
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15926841

FLYING VEHICLE EMERGENCY PROCEDURES

Electronic emergency landing system. Provides safe landing of aircraft in case of failure of one of the propellers. It differs from analogs in that the system is fully automated and does not require human participation.

15945682

FLYING VEHICLE ARCHITECTURE

The layout of the aircraft differs from analogs in that it has a higher speed and comfort of flight compared to a multicopter and a greater reliability and efficiency compared to an aircraft with rotary thrusters (convertiplanes). A dynamic wing unlike a classic wing, the angle of attack and profile are completely computer controlled. Automatically folds down when planted to reduce footprint.

15926890

FLYING VEHICLE HYBRID POWER PLANT

The system for increasing the duration and range of flight is a generator consisting of an internal combustion engine with a free piston, which does not have a single bearing, connecting rod, or crankshaft, in contrast to classic internal combustion engines. Windings are integrated into the generator housing, thus, it is possible to reduce the weight and dimensions of the power plant.

15945667

FLYING VEHICLE THRUST DEVICE

The Venturi engine with the same thrust is 3 times smaller and safer than an open propeller. Eco friendly.

2017138560/11(067302)

Small-sized vertical take-off / landing aircraft
with increased flight range

The layout of the aircraft differs from analogs in that it has a higher speed and comfort of flight compared to a multicopter and a greater reliability and efficiency compared to an aircraft with rotary thrusters (convertiplanes). A dynamic wing unlike a classic wing, the angle of attack and profile are completely computer controlled. Automatically folds down when planted to reduce footprint. The Venturi engine with the same thrust is 3 times smaller and safer than an open propeller. Environmentally friendly.

2017105473/11(009845)

Quadcopter emergency landing method

Flight software. Electronic emergency landing system. Provides safe landing of aircraft in case of failure of one of the propellers. It differs from analogs in that the system is fully automated and does not require human participation.

2017107692/11(013298)

System for increasing the duration and range of the multicopter flight

The system for increasing the duration and range of flight is a generator consisting of an internal combustion engine with a free piston, which does not have a single bearing, connecting rod, or crankshaft, in contrast to classic internal combustion engines. Windings are integrated into the generator housing, thus, it is possible to reduce the weight and dimensions of the power plant.

2017111894/11(021022)

Multicopter frame (options)

The hybrid frame differs from the classic solutions in that the propeller bracket and landing gear are combined into one component, which reduces the weight and dimensions of the aircraft.

2019120954

A way to increase speed, flight maneuverability and reduce energy costs
for straight flight of a multicopter

The layout of the aircraft differs from analogs in that it has a higher speed and comfort of flight compared to a multicopter and a greater reliability and efficiency compared to an aircraft with rotary thrusters (convertiplanes).

2019128525

The system for combining the rotor and the shock-absorbing landing gear of the aircraft into a single airborne propulsion system

The system of combining the rotary wing and the aircraft landing gear to increase active and passive protection in the event of a fall, for movement on the ground and in the air. In contrast to the known solutions, it combines the chassis and the propeller into one element.

2019139825

Security system for vertical take-off and landing aircraft

Flight software. Takeoff and landing assistance system. A computer system for limiting dangerous modes of aircraft during takeoff and landing. It differs from analogs in that the system is fully automated and does not require human participation.

2019131525

Aircraft balance control system

Balanced control system for a manned drone. Differs from analogs in intuitiveness and convenience of control method.

2019139829

Item Device for controlling a manned aircraft for vertical take-off and landing

A type of control to increase the stability of the pilot's position during the flight with the possibility of using a wide grip, increasing the safety of piloting, the ability to resist overloads. Allows you to control all axes of the copters with a fixed pilot's arm.

2019139828

System of electrical energy carriers built into the aircraft body

Energy delivery system along the aircraft beams using a special battery. Reduced conductors, increased rigidity, increased payload space.

2019139827

Aircraft cabin gyro stabilization system

A closed cockpit that does not change the angle of inclination when the angle of the aircraft itself changes. For passenger comfort and the possibility of using it on various aircraft layouts.

 
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