Patent Application
20150330304
This patent claims priority to Russian patent application Serial No. 2014119114/06 (030106) filed on May 13, 2014, currently issued as a patent. Decision on grant of Russian patent is issued on Jan. 13, 2015.
The invention relates to energy and transport, in particular to the universal power engine with thrust vector control, which can be used to move different, almost any object that you want to move from one place to another, for example, this power engine can find application in the transport machines both the land ones and air or above-water ones.
There is known an engine of a air-cushion vehicle which comprises a load-bearing structure with a platform, a flexible side fence, a source of pressure in the fenced zone and a wheeled mover (see the patent GB N0 1465382, cl. B60V 1/00, Feb. 23, 1977).
In this vehicle the source of high pressure is removed from the supporting surface. therefore, the formation of an air cushion is due to the static pressure increase in the area of the fence between the base of the vehicle and the supporting surface without the use of effect velocity head, which reduces the lifting force generated by an air cushion and requires increased airflow, sharply limiting the ability to use this power engine application such as vehicle in this case.
The engine equipped with the orthogonal turbines units with jet control of the media flow on the blades is the most similar to the invention from the view of the technical essence and the results achieved. Two cavities are in these blades to supply the media to control jet generated throw outlet slots located along the blades. Blades of the turbines have the aerofoil profile. Two cavities with outlet slots are formed inside the partition which divides the internal space of the blades. The outlet slots are directed to the corresponding surface of the blade behind the point of its profile maximum thickness.
The blades are installed on hollow shaft mounted for rotation using hollow cross arms with streamlined profile. These cross arms are perpendicular to the shaft and the cavities of the blades, of the crossed arms and of the shaft are interconnected. There is a stationary hollow gas-distribution pipeline with holes in its walls, used to ensure the connection between the gas-distribution pipeline cavity and the cross arm cavities, inside the hollow shaft (coaxial to it with annular gap). Herewith the distribution pipeline is connected to a source of continuous or pulse supply of gaseous media under pressure (see patent RU No. 2327059, CL F03G7/08, 20.062.008).
This engine allows to create a device that can move on the ground and in the air due to the interaction of the rotating blades of the rotors with the environment. However, the efficiency of this engine is relatively small due to its energy loss.
The object of this invention is to increase the interaction efficiency of the rotating rotors' blades of the engine.
This problem is solved and the technical result is achieved due to the fact that the engine with thrust vector control is equipped with at least one blade orthogonal turbine with jet circulation control flow of the blades; these blades have at least one cavity to supply the control media to jet generation outlet slots located along the blade; two cavities with outlet slots are formed inside the partition which divides the internal space of the blades; the blades of each turbine have the aerofoil profile; each output slot is displayed on the corresponding surface of the blade in the area behind the point the maximum thickness of the profile of the blade; the blades are installed on hollow shaft mounted for rotation using hollow cross anus made from streamlined profile; these cross arms are perpendicular to the shaft and the cavities of the blades of the crossed arms and of the shaft are interconnected; there is a stationary hollow gas-distribution pipeline with holes in its walls, used to ensure the connection between the gas-distribution pipeline cavity and the cross arm cavities, inside the hollow shaft (coaxial to it with annular gap); distribution pipeline is connected to a source of continuous or pulse supply of gaseous medium under pressure; each cavity of each blade is equipped with spark plugs burning, the fuel-air mixture connected to the induction coils of the ignition system.
The blades may be straight.
The blades can be made along a helical line.
The blades can be set multilevel.
The increasing the efficiency of the engine is due to the combination described above. A spark ignition of an air-fuel mixture in each cavity of each blade is installed, and spark plugs are connected to the induction coil of the ignition system and gas distribution pipe connected to the supply system of fuel-air mixture.
In
The engine with controlled thrust vector contains at least one orthogonal turbine 1 with jet circulation control of the blades 2. For this purpose these blades have at least one cavity 3 to supply the control media to jet generation outlet slots 4 located along the blades.
The blades 2 each turbine 1 have the aerofoil profile. Each output slot 4 is directed to the corresponding surface of the blade 2 behind, the point of its profile maximum thickness. The blades 2 are installed on a hollow shaft 5 mounted for rotation using hollow cross arms 6 made from streamlined profile. These cross arms are perpendicular to the shaft 5 and the cavities 3, 7, and 8 of the blades 2, of the crossed arms 6 and of the shaft 5 respectively are interconnected. Inside the hollow shaft 5 (coaxial to it with annular gap) there is a stationary hollow gas-distribution pipeline 9 with holes 12 in its walls used to ensure the connection between the gas-distribution pipeline 9 cavity and the cross arm 6 cavities 7.
Distribution pipe 9 is connected to a source of continuous or pulsed supply of gaseous medium under pressure (not shown in the drawings), each cavity 3 of each blade 2 is installed spark plugs 10 air-fuel mixture that is connected to the induction coil 11 system ignition and distribution pipe 9 is connected to the supply system of fuel-air mixture.
The blades 2 may be straight, helical and may be set multilevel.
To put in motion a vehicle equipped with the described engine fuel-air mixture is supplied to the cavity 3 of the blades 2 of the orthogonal turbine 1 through distribution pipeline 9 and further through the shaft 5 and crossed arms 6. This fuel-air mixture is burnt up in the cavity (or cavities) 3 of the blades 2 with spark plugs 10. As a result of the fuel-air mixture burning combustion products are generated; these products exit through the jet generation outlet slots 4 and form a jet stream rotating the blades 2 of the orthogonal turbine 1 and creating lifting force perpendicular to the axis of the turbine. The spatial orientation of this force is determined by the position of the holes 12 in the distribution pipeline 9.
The lifting force magnitude is regulated by the shaft 5 speed and consumption of the fuel-air mixture supplied to the blades 2. The direction of the force acting on the engine is determined by the position of the holes 12 in the distribution pipeline 9.
The present invention can be used in automotive, construction, oil and gas and other industries that need to be transported to lift or move a variety of goods. The test of model (
It will be understood that the system and method may be embodied in other specific forms without departing from the spirit or central characteristics thereof. The present examples and embodiments, therefore, are to be considered in all respects as illustrative and not restrictive, and the system method is not to be limited to the details given herein.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2014119114/06 | May 2014 | RU | national |
