The present invention relates to a horizontal shaft rotor and a watercraft having the rotor, and more particularly, to a horizontal shaft rotor in which a flow receiving surface of a lift-type blade is largely bulged and a blade tip is inclined to the direction of the flow receiving surface and a watercraft having the rotor.
A blade in which the blade tip is inclined to the direction of the flow receiving surface is disclosed for example, in Patent Literature 1.
Patent Literature 1: JP2007-125914A
In the rotor blade disclosed in the above-mentioned Patent Literature 1, for example, when it is used for a ship propulsion machine, water is pushed out by the force of the blade, so that a large power torque for overcoming the resistance of water is required.
It is an object of the present invention to provide a rotor in which a fluid traveling along a circumferential surface of the blade produces a propulsion flow due to a water pressure difference caused by a high-speed flow according to the Coanda effect naturally occurring depended on the shape of the blade by rotating the blade rather than pushing out a fluid with the blade.
Special features of the present invention are as follows.
(1) A horizontal shaft rotor comprising a lift-type blade, in the lift-type blade, a front face in a flow receiving direction is a large arcuate bulging face in a string direction, a rear face in a discharge direction is made smaller than the bulge of the front face, when the blade rotates, a high speed flow caused according to the Coanda effect passing along the string direction of the front face from a rear edge portion to a back face direction generates propulsive force.
(2) The horizontal shaft rotor according to (1) above, wherein, in the lift type blade, the back face in the discharge direction at the blade root portion is linear in the string direction and parallel to the rotation direction, the back face is gradually increased inclination to a front face direction from the blade root portion to the maximum string length portion, and from the rear edge portion to a front edge portion.
(3) The horizontal shaft rotor according to (1) or (2) above, wherein, in the lift-type blade, in a side view, a thickness gradually decreases from the blade root portion to a blade tip portion, and the front face gradually inclines to the back face direction from the blade root portion to the blade tip portion.
(4) A watercraft comprising the horizontal shaft rotor according to any one of claims 1 to 3, wherein the horizontal shaft rotor is mounted on a rotor shaft of a rotor housing disposed in the watercraft so that a tip of an inclined portion of a blade is oriented in a bow direction.
According to the present invention, the following effects can be obtained.
In the invention described in the above (1), since the back face is flat and the front face bulges out like a blade cross-section shape, a high speed flow according to the Coanda effect occurs on the front face in the rotor shaft direction due to the rotation, and this high speed flow passes from the rear edge in the string direction to the back face direction, the propulsive force is generated in the rotor shaft direction as a reaction.
Due to the rotation, the fluid along the front face gathers in the direction of the inclined portion, and gets even faster according to the Coanda effect occurring at the bulging face of the front face in the inclined portion, and passes to the back face direction, the propulsive force in the rotor shaft direction is generated as a reaction.
In the invention described in the above (2), since the back face of the blade root portion of the lift-type blade is straight in the string direction and an angle of attack gradually increases from the blade root portion with the zero angle of attack to the maximum string length portion, a blade tip portion pushes the fluid to make the propulsive force, but since the amount of fluid flowing with high speed along the front face is larger than the amount of fluid to be pushed, the power can be made small.
In the lift-type blade of the invention described in the above (3), in a side view, the thickness gradually decreases from the blade root portion to the blade tip portion, and the front face gradually inclines toward the back face direction from the blade root portion to the blade tip portion, so that the resistance during rotation is small and the fluid along the front face is easy to move to the blade tip direction, the fluid gathered at the inclined portion of the blade tip becomes high speed according to the Coanda effect and flows from the rear edge to the back face direction, the propulsive force is generated as a reaction.
In the invention described in the above (4), since a rotor oriented the tip of the inclined portion of the blade in the bow direction is mounted on the rotor shaft of the rotor housing disposed in the watercraft, when the rotor rotates, the high speed flow moving according to the Coanda effect in the string direction at the front face being the flow receiving surface of the blade passes from the rear edge to the back surface being the discharge direction, the propulsive force is generated as a reaction.
An embodiment of the present invention will be described below with reference to the drawings.
In the rotor 1, a plurality (five in
The blade 3 gradually increases the string length from the blade root portion 3A to the blade tip portion, and the maximum string length portion 3B is set to be as wide as 45 to 50% of a turning radius.
As shown in
The tip from the maximum string length portion 3B is an inclined portion 3C, and as shown in
The back face 3E on the downstream side of the blade 3 is a flat face, as shown in
As shown in
In the blade root portion 3A in
The thickness gradually becomes thinner towards the blade tip portion. In the maximum string length portion 3B in
When the blade 3 rotates, the fluid passing to the string direction passes through the large bulged front face 3D at a high speed according to the Coanda effect. The fluid passing through the front face 3D is faster than the velocity of the fluid passing through the back face 3E without bulge, and for the fluid that the flow velocity is faster than the surroundings, its density becomes lower density and the pressure drops lower than the ambient.
A fluid of normal pressure flows into the fluid of reduced pressure from the surroundings, as a result, the fluid pressure increases and the fluid moves to the direction of the blade tip portion, then, the fluid gathers at the inclined portion 3C and strikes it, as a result, the fluid passes through the bulged front face 3D in the inclined portion 3C to the direction of the rear edge portion 3G of the string, the propulsive force is generated as a reaction.
In
In
In
Since the amount of the fluid in a certain period of time gathered in the maximum string length portion 3B is a fluid which gathers from the direction of the blade root portion 3A by centrifugal force and other fluid pressure change due to the rotation, as a quite large reaction, that is, the rotational speed of the rotor 1 is increased, and a large propulsive force is generated to the direction of the rotor shaft 4.
As being apparent from
That is, as shown in
At the blade tip portion with a high rotating circumferential speed, since the front edge portion 3F and the rear edge portion 3G are pointed and the thickness gradually increases toward the middle of the front face 3D like the half meat of a fish, the relative flow with respect to the front edge portion 3F during rotation passes at high speed according to the Coanda effect and the resistance does not occur when it passes through the largest thickness portion of the front face 3D to the string direction.
In this way, the rotor 1 does not push out water to the downstream direction by the blade 3, due to the rotation of the blade 3, the relative flow generated in the string direction becomes the high speed water flow according to the Coanda effect at the front face 3D, and passes from the rear edge portion 3G to the back face 3E direction, the propulsive force is generated as a reaction.
As a result, the blade 3 does not push out water by force, so that large power is not required. Since Coanda effect naturally occurring due to the rotation of the blade 3 is utilized, when the blade 3 rotates, the Coanda effect naturally occurs, and when the flow velocity of the fluid along the front face 3D is faster than the fluid along the back surface 3E, the high speed flow naturally passes to the direction of the back face 3E.
The front end portion of the rotor shaft 4 is connected to the motor 8 via the clutch 9 so that the rotor 1 can be rotated by the motor 8, but when the clutch 9 is disconnected, the rotor 1 can be rotated by wind power. Number of blades 3 is arbitrarily set within the range of 2 to 6 sheets.
A rotation number of the rotor shaft 4 is measured by a measuring instrument 10 provided in the rotor housing 7, and the measured value is inputted to an automatic controller 11. When the motor 8 is started and the clutch 9 is connected, the rotor 1 is rotated by the motor 8.
Due to the rotation of the rotor 1, when the air current generated by the blade 3 is discharged in the directions indicated by arrows F and F in
That is, since the air current concentrates to the direction of the axial center in the direction of the back face 3E, the propulsive force becomes large.
When the rotational speed of the rotor 1 is increased, the propulsive force is further increased. As a result, by adding a small auxiliary motor, a strong propulsive force can be obtained. The rotor 1 may be used as a screw under water.
By rotating with a small power, a high speed flow caused according to the Coanda effect occurring in the string direction of the flow receiving surface of the blade passes from the rear edge portion to the back face direction, and the propulsive force can be obtained as a reaction, so that the rotor 1 is used as a propulsion machine such as a small watercraft.
Number | Date | Country | Kind |
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2016-038817 | Mar 2016 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2017/006592 | 2/22/2017 | WO | 00 |