KR20120040713A - Stabilized safety gyroplane - Google Patents

Abstract

The present application takes a variety of known methods and combines them in a special way, the present application relates to the integration of a double rotor blade connected to a launching machine, and by this integration there is no risk of reverse torque propellers that can be dangerous. do. The device is designed to allow sufficient time for the natural effect of self-sufficiency. Special editorial introduces new technologies for the first time with the principle of gyroplane technology, an eCRT technology that provides additional safety. Aircraft with rotorcraft are helped by "radio controlled" eCRTs performed with eCRT sensors, which eliminate the effects of fluctuating electromagnetic incompatibility caused by stressed mechanical components, increasing flight performance. It also ensures that available power is not subject to stress, parasites or variable back forces.

Description

Stabilized Safety Gyroplane {STABILIZED SAFETY GYROPLANE}

In the future, the ideal mode of transport for all travelers in terms of consumption, pollution and stability is not known. Applicants have long considered this issue and have considered a variety of options that, along with the limitations of traffic, make them prefer faster and more efficient approaches that require greater attention to safety. Travel is important for active people who are involved in the marketing of real and virtual services that require a reaction and involve delays in distance and decision making due to speed constraints. Gyroplanes are a special type of aircraft, and generally require further development in terms of flight safety and environmental protection. Due to various factors about noise and pollution, people choose to travel by land or inexpensive transportation. Safety is a major contributor to the problem of aircraft landing at high speeds in certain locations. Helicopter safety is a source of concern because helicopters are very expensive and noisy, and because of the rotor blades that have different tilts by one set of cranks on each turn.

The present application contemplates different known methods which are combined in a special manner, in which the dual rotor blades are connected to the launching engine so that there is no need for a reverse torque rotor which can pose a great danger. Are integrated. This device is used until there is sufficient natural lift. In a particular configuration, the new technologies being combined for the first time are combined with the principles of gyroplane technology represented by eCRT technology providing additional safety.

1 shows a gyroplane consisting of two rotors, which are rotorcraft.

1 shows a gyroplane consisting of two rotors 1 and 2 which are rotor blades, the blades of which are rotated in opposite directions to balance the lift without the need for an active reverse torque rotor. In order to fly the plane, the engine 5 is used to start the rotor blades 1 and 2 before lift is applied, so that the safety of takeoff is greatly improved. The device also enables practical vertical takeoff at low wind speeds of less than 20 knots without moving distance due to balance damage, loss or excessive induction. Until the plane emerges in automatic rotation, a torque converter operated in the aviator's airframe will operate the rotors 1 and 2 with the opposite mechanical rotation 6. The torque converter can deliver the minimum available energy of the engine 5 to provide lift. The engine 5 transmits its output to the horizontal thrust propeller 4 so that it is naturally lifted up without the need to energize the rotors 1 and 2 supporting the plane, generating a translational speed and the gyroplane Allow you to move forward. The blades are at a constant pitch, which creates a drag that slows down the flight speed, but gives considerable safety. The pitch may vary, but is the same for both blades that make up the dynamic wing structure, as in the case of propellers in fixed wing aircraft with variable pitch propellers. Clearly, this relates to both rotors 1, 2. The control provided in the body 3 allows the manipulation for accurate flight to be performed with high visibility. This stability, which is enhanced by integrating two rotors that form a rotorcraft, achieves high stability and, when coupled with an engine for relatively slow sliding forward movement, lift is achieved without leaving the aircraft in automatic rotation mode.

The device provides reliable safety as the aircraft automatically stabilizes during flight. These features are not operating conditions or functions, but are momentary and temporary flight safety measures, which currently do not have a gyroplane and must also require energy input.

In addition, mechanical noise and rotor noise can be applied to eCRT technology (one of the claimed applications) in the form of a mechanical flight member that connects the engine, aircraft structure, rotor rotor shaft and power converter to the blades being adjusted when the aircraft is taken off. Reduced by applying to mechanical components. The noise gain is at least 5 decibels, and the available power of a conventional piston engine, Wankel or turbine or other type of engine is very effective at 110 horsepower, allowing the set of rotors to be started without difficulty. Mechanical friction is greatly reduced, thus achieving high gains and reliability in available power in terms of this multi-axis mechanical device backed by intelligent eCRT technology that regulates the tension and stress of mechanical components. The applicant claims priority to the PCT / FR2009 / 001006 patent on August 14, 2009. The technology disclosed in this patent provides silent operation and remarkable reliability while freely using engine torque, while also reducing fuel consumption by 15%? 20% reduction and at least 35% of NO _x ? Eliminate 40% The eCRT sensor is for example an eCRT (7; 8; 9) (adhesive automatic radio control device that detects all relative positions that are automatically controlled by "auto radio control" of the movement of mechanical components under stress acting on the aircraft's movement). In the form of the gyroplane gas 3. The aerial operation of the machine is very sensitive, and the dynamic vanes provide "extra lift" due to the eCRT implementation that manages the controlled and eliminated electromagnetic currents and polarity, thereby eliminating the disadvantages of electromagnetic incompatibility caused by mechanical stress, Performance is improved and mechanical power is freed without stress. Thus, the eCRT sensor can, in this non-limiting exemplary embodiment, eliminate these incidental and opposing variable electromagnetic loads in a stable and ideal state without interference and variable adverse forces for the flight of aircraft with at least one dynamic rotor blade. have.

Claims (4)

Mechanically integrated double wings that rotate in opposite directions connected to the launch engine until natural lift forces are applied, eliminating the need for reverse torque rotors and enabling vertical takeoff at low wind speeds, providing safety and stability to the gyroplane. Way. The method of claim 1,
How to add a thrust propeller that moves the gyroplane forward and also provides lift due to the translational movement of the gyroplane along the horizontal axis. A rotorcraft based on the principle of gyroplane, comprising a dual wing connected to a power converter and rotating in opposite directions, wherein the power converter transmits power of a gyroplane engine for launching by a mechanical converter. The conventional transducer provides lift and also receives command from the airframe to transmit power to the horizontal thrust propellers, which the aircraft switches to natural lift mode at its translational speed, and by this principle of operation, automatically rotates. Rotorcraft aircraft capable of taking off at low wind speeds. The method of claim 3, wherein
The rotorcraft is aided by an eCRT "radio control" provided by the eCRT sensor, which eliminates the effects of electromagnetic incompatibility caused by stressed mechanical components, improving flight performance and providing more available power. Rotorcraft aircraft that resist stress, interference and back forces.

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