The way to perform vertical take-off speed aircraft

 

(57) Abstract:

The invention relates to aviation and relates to a technology of performing vertical take-off speed aircraft. The essence of the invention lies in the fact that the parachute output on the cable in the vertical direction and, according to the invention, the chute is fixed on the means of its output, for example, the rocket, the second end of the cable chute is fixed on the pulley with the drive to pull the parachute in the aircraft. Another cable connects the tail of the aircraft from take-off, start the engine and remove the parachute tension to the cable, and after the engine thrust, enough for the flight, retract the said actuator above the chute at a rate that ensures the rise of the aircraft above the ground take-off, and release the torso of the connection tail section. The torso of the parachute can connect to the aircraft between the center of mass and the nasal part of it. The technical result from implementation of the described invention is the extension of the scope of implementation of the method of performing vertical take-off aircraft. 1 C.p. f-crystals.

The invention otnositelnosti aircraft.

A known method of performing vertical take-off speed aircraft, including the conclusion of a parachute rope in a vertical direction (US patent N 3721408, IPC B 64 I 17/38, published. 20.03.73).

However, the known method is characterized by the narrowness of the range of its implementation.

The technical result from implementation of the described invention is the extension of the scope of implementation of the method of performing vertical take-off aircraft.

This technical result is achieved that, when implementing the method for performing vertical take-off speed aircraft, including the conclusion of a parachute rope in a vertical direction, according to the invention, the chute is fixed on the means of its input, for example, the rocket, the second end of the cable chute is fixed on the pulley with the drive for retracting parachute in the aircraft, connect the other wire of the tail portion of the aircraft from take-off, start the engine and remove the parachute tension to the cable, and after the engine thrust, sufficient for the flight, retract the said actuator above the chute at a speed which pulls up the flyer is EcoObraz during the implementation of the method described above rope parachute to connect with aircraft between center of mass and the nasal part of it.

When implementing the method for performing vertical take-off speed aircraft parachute fixed on the means of its output in the vertical direction, for example, rocket or inflatable balloon, and the other end of this cable is connected with the drive pulley, while the aircraft is equipped with a second rope, which is fixed on the Playground and in the area of the tail section of the aircraft, then start the engine and remove the parachute tension to the cable and when reaching a traction engine, rated in terms of its significance for the flight, pull the parachute by means of the driven pulley in the aircraft with speed, which is due to the aerodynamic interaction of the dome of a parachute with a forced flow raises an aircraft above the ground, then let go of the rope tail mounts so that the cable chute fitted between the nose of the aircraft and its center of mass.

When explaining the method should note the following.

1. As a means of conclusion of the parachute in the vertical direction may be used either rocket or inflatable balloon that can completely bring a parachute with a rope to his tension. More C the segments, and can prevent the wind. Rocket, because she quickly fires require strict compliance with time steps of following commands. Indeed, if the parachute display a balloon, the latter will hold the parachute in working condition for a long time and after engine starting apparatus can be started the motor of the drive cable chute for retracting after reaching the desired thrust. When using rockets to start it proactively to achieve the necessary traction, which is not always smoothly increases.

2. The sequence of operations thus the following. Secure the tail of the rope with their ends on the ground and on aircraft. On the last take-off shall mount on a folding hook that is retained by the actuator. Letting go of the rope produced by the attainment of the specified thrust after retracting parachute. Force (thrust) is measured by a sensor, for example, strain gage, and the time of retracting parachute registered emphasis on the rope parachute, so as to disconnect the cable tail should be proactive, so that the aircraft was raised on the site. Because mount a flying machine made rope parachute closer to wear, and the angle sensor to determine the state of recovery of the aircraft. When the cable tail mounting and axis aircraft will be close to the same. If the angular position is not available, then the retraction speed of the parachute is small, and the cable tail attachment is released. If the rise and thrust achieved by its value, released the rope tail mounting, and the aircraft flies at an angle. The parachute can get to the end, and after takeoff.

3. If you used a rocket to output a parachute, it must connect with him destructible from shock loads when the hood cable until it stops. If you are using an inflatable balloon, he or destroyed by pulling it in the aircraft, or detached.

4. For landing aircraft cable tail mounting at the free end must have an anchor (marine type), and the second end of the cable should be attached to the pulley with the drive. The process of descent should be next. To reset the anchor. After coupling with the roughness of the terrain begins to release the rope, performing a gradual decrease of the horizontal component of velocity. After reaching the speed begins falling off when the engine is tigalda all of the objectives, namely, not only the vertical take-off aircraft, but its descent in a limited space.

1. The way to perform vertical take-off speed aircraft, including the conclusion of a parachute rope in a vertical direction, characterized in that the chute is fixed by means of its output, for example, the rocket, the second end of the cable chute is fixed on the pulley with the drive for retracting parachute in the aircraft, connect the other wire of the tail portion of the aircraft from take-off, start the engine and remove the parachute tension to the cable, and after the engine thrust, sufficient for the flight, retract the said actuator above the chute at a rate that ensures the rise of the aircraft above the ground takeoff, and release the cable connection tail section.

2. The method according to p. 1, characterized in that the rope parachute connected to the aircraft between the center of mass and the nasal part of it.

 

Same patents:

The plane // 2120394
The invention relates to aviation and can be used to create aircraft with improved characteristics

The invention relates to a device for creating aerodynamic lift

Helicopter // 2118272
The invention relates to aircraft vertical takeoff and landing

The invention relates to Aeronautics and relates to a method of creating a lifting force for aircraft, lowering the resistance forces

The invention relates to marine aviation industry and for the construction of multipurpose rescue amphibious aircraft

The invention relates to the field of propulsion systems, and in particular, to the motor systems briefly and vertically taking off and prizemlilsa aircraft type OF┴GDP

The invention relates to the propulsion of vehicles that do not interact with the support surface using the aerodynamic properties of a rotating propeller rotor wing aircraft, the centrifugal force of the rotating air stream, and the atmospheric pressure difference in front of and behind the facility, with the propeller

The invention relates to coaxial sub-node transmission/Central sleeve node bearing screws unmanned aerial aircraft

The invention relates to a toroidal fuselage of an unmanned aerial vehicle, having an optimized design

The invention relates to the field of air and gastouni machines

The invention relates to the field of aviation, in particular to the stabilization systems of aircraft, and can be used in the autopilot guided missiles

The invention relates to rocket and space technology and can be used to bring the exhaust accelerator first-stage space rocket "proton-M" in a limited area of impact to reduce the effect of ILV on the ecological state of the area of operation

The invention relates to an aircraft, and relates to a method of determining the position of the point of application of external forces helicopter

The invention relates to aviation, namely the means of braking LA after landing on the runway

The invention relates to a control system aircraft, namely vasoreactive systems, and can be used to control missiles and rockets

The invention relates to control systems of the aircraft by changing the thrust vector

The invention relates to rocket technology, and in particular to systems start and orientation of the missile, and can find primary use in small missiles surface-to-air and air-to-air

Passenger jet // 2068377
The invention relates to aircraft and, in particular for aircraft

The invention relates to an aircraft, namely the supersonic or hypersonic aircraft with air-breathing engines
Up!