JP2013501675A - Stabilized and safe gyroplane - Google Patents

Abstract

  This application is a collection of the latter in a specific way using various well-known processes and eliminates potentially dangerous anti-torque propellers for the integration of double rotors connected to the starting engine. it can. The device is arranged so that the self-containment natural effect has sufficient time. The new technology gathered for the first time by special compilation is introduced into the principle of gyroplane technology, which is an eCRT technology that brings further safety. An aircraft with a rotating wing is supported by a “wirelessly controlled” eCRT performed by an eCRT sensor, which prevents the effect of fluctuating electromagnetic incompatibility caused by mechanical components under stress, thereby preventing flight Improve performance and liberate available power from stress, parasitics and fluctuating reaction forces.

Description

  The ideal form of transportation for all future travelers is still unknown when considering consumption, pollution and safety issues. We have studied this issue for a long time and examined various solutions that encourage us to prefer faster, more efficient but more safety-sensitive solutions along with traffic restrictions I have done it. Travel is essential for active people involved in trading real services as well as virtual services. Such services require some degree of responsiveness, but delays in transactions and decision making due to speed limitations. The gyroplane is a special type of aircraft, but generally speaking, further development is needed for flight safety and environmental protection. Depending on various factors related to noise and pollution, we choose land travel and cheap transportation. Safety is a major factor that makes us think about the problem of aircraft landing at a particular point at high speed. Helicopters are very expensive and noisy, and their safety rating is a concern because each set of cranks adds a different slope to the rotor blades depending on the set of cranks.

  This application takes into account a number of different known processes. We combine these multiple processes in a special way provided in this application, with the integration of double rotors connected to the starting engine, so that the anti-torque rotor that creates high risk can be omitted. This device is used until the natural levitation effect is sufficient. In a special arrangement, the new technology gathered for the first time is combined with the principles of gyroplane technology represented by eCRT technology that provides additional safety.

2 illustrates a gyroplane having two rotors.

  FIG. 1 illustrates a gyroplane having two rotors (1, 2). These rotors (1, 2) are rotor blades whose blades rotate in opposite directions so that lift balance is obtained without the need for an active anti-torque rotor. To start the aircraft, the engine (5) is used to activate the rotable plate (1, 2) before lift is generated. This can greatly improve the safety at takeoff. The device also allows for virtually vertical take-off at low wind speeds of less than 20 knots without losing or losing balance or extra distance taxing. A torque converter operated from the fuselage by the pilot operates the rotors (1, 2) with mechanical rotations (6) in opposite directions until the aircraft is levitated by autorotation. The converter minimizes the effective energy of the engine (5) that is transmitted to obtain lift. The engine (5) transmits its power to a horizontal thrust propeller (4) to create a moving speed and allow the gyroplane to move forward and its rotor (1,2) to naturally support the aircraft Receiving the lift without having to supply energy. The blade pitch is constant and tends to create resistance that slows the flight speed, but provides very high safety. The pitch can be changed, but is the same for both blades constituting the dynamic wing structure. This is similar to a fixed wing aircraft propeller with a variable pitch propeller. Obviously, this relates to both rotors (1, 2). Due to the control provided in the airframe (3), it is possible to execute the driving for accurate flight with high visibility. This stability, which is improved by integrating the two rotors that form the rotor blades, provides high stability and, together with a relatively slow driving forward engine, increases the lift without putting the aircraft into autorotation mode. provide.

  This device provides reliable safety through automatic stabilization of the aircraft during its flight. This feature is not a driving condition or function, but an immediate solution for temporary flight safety. This solution currently has no gyroplane and definitely requires energy input.

  In addition, mechanical noise and rotor noise are reduced by the contribution of eCRT technology. eCRT technology is one of the claimed applications applied to mechanical components. Here, the mechanical component is in the form of a mechanical flight member that connects the power converter to the blade, and the engine that is controlled when the aircraft is launched, the fuselage structure, the rotor shaft of the rotor blade, and the power converter. is there. The noise gain is at least 5 dB, and the useful power from conventional piston engines, Wankel engines, turbine engines or other types of engines is very effective at 110 in horsepower evaluation, and runs a set of rotors without difficulty Can be made. Considering this mechanical arrangement using multiple axes supported by intelligent eCRT technology that controls the tension and stress of the mechanical components because mechanical friction is greatly reduced, reliability and utilization High gain in possible power is provided. We claim priority with respect to patent application PCT / FR2009 / 001006, filed on August 14, 2009. The technology disclosed in this patent provides noiseless operation and significant reliability while releasing engine torque, reduces fuel consumption by 15-20%, and reduces NOx by at least 35-40%. Remove. An eCRT sensor is placed on the gyroplane shaft and airframe (3), for example in the form of eCRT (7; 8; 9). eCRT (7; 8; 9) is an adhesive-attached automatic radio controller that detects all of the relative positions, by “automatic radio control” of the movement of mechanical components under the stress that contributes to the movement of the aircraft Automatically controlled. The maneuvering of the machine in the air is very delicate and thanks to the implementation of eCRT, the dynamic wing provides “additional lift”. The eCRT implementation mandates the polarity and electromagnetic current to be controlled or removed, thereby preventing the disadvantages of electromagnetic incompatibility arising from mechanical stress, improving flight performance and generating mechanical power without generating stress. Liberalize. Thus, the eCRT sensor, in this non-limiting exemplary embodiment, in a stable ideal condition without interference or fluctuating reaction forces for the flight of an aircraft provided with at least one dynamic rotor. The fluctuation of the opposing electromagnetic load that occurs accidentally can be eliminated.

Claims (4)

  By mechanically integrating double wings connected to the starting engine and rotating in opposite directions until natural lift is generated, it is possible to eliminate the need for a half-torque rotor and to achieve vertical at low wind speeds. A method of providing safety and stability to the gyroplane that enables take-off.   The method of claim 1, comprising adding a thrust propeller that allows the gyroplane to advance and provides lift due to movement of the gyroplane along a horizontal axis.   It consists of double wings connected by a mechanical converter and rotating in opposite directions to a power converter that transmits the power of the engine of the gyroplane for start-up, said mechanical converter providing lift energy and from the fuselage This is a rotary wing aircraft based on the principle of gyroplane that converts the power into a horizontal thrust propeller under the command of, and enters the natural levitation mode by its moving speed, and without establishing autorotation by this operating principle A rotorcraft that can take off at low wind speeds.   Provided by an eCRT sensor that improves flight performance by smoothing out electromagnetic incompatibility effects generated by mechanical components under stress and frees available power from stress, interference, and reaction forces The rotary wing aircraft of claim 3, supported by an eCRT “radio control”.

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