TWM526626U - Hydraulic blade apparatus - Google Patents

Description

Fluid blade equipment

The present invention relates to a blade device, and more particularly to a fluid blade device that can be driven by a fluid to be applied to a fluid power generation device.

Referring to Fig. 1, a wind blade device of the Taiwan Patent No. M485960 patent, the wind blade device mainly comprises: a rotating shaft 81, and a plurality of blade modules 82 connected to the rotating shaft 81 and angularly spaced from each other. Each of the blade modules 82 includes a grille 821 that connects the rotating shaft 81, and a plurality of blades 822 that are pivotally suspended from the grille 821.

When used, the wind blade device is mounted on a horizontally rotatable rotating seat, and a baffle is mounted on the rotating seat. When the wind is blown in a flow direction, the baffle is driven by the wind to drive the rotating seat to rotate to drive the blade 822 device to turn the blade module 82 perpendicular to the flow direction. The wind power generating device can receive the wind on the front side, but the wind power generating device drives the rotating seat to rotate due to the force exerted by the wind on the blade module 82, thereby driving the blade 822 device to turn the blade module. 82 is a position parallel to the flow direction of each other.

It can be seen from the above that the rotating seat is pushed by the opposing force of the deflector and the blade modules 82. Therefore, the size of the deflector must be designed corresponding to the size of the blade module 82 to provide appropriate The deflection force forces the wind blade device to maintain the position of the wind receiving device. If the user increases the size of the blade module 82 in order to increase the torque, it is necessary to increase the size of the deflector and increase the size of the deflector. The size of the baffle increases the material cost of the wind blade device, so the existing wind blade device still needs to be improved.

Accordingly, it is an object of the present invention to provide a fluid blade apparatus that reduces material costs.

Thus, the novel fluid blade apparatus can be driven by fluid flowing in a flow direction and includes a rotating seat and a vane device. The rotating seat is rotatable about a vertical axis. The blade device is mounted on the rotating seat and can drive the rotating seat to rotate, and includes a rotating shaft and a plurality of blade units.

The rotating shaft extends along a horizontal axis and is pivotally connected to the rotating base along the horizontal axis, the rotating shaft has a fulcrum portion located in the middle and pivoted to the rotating base, and two locating points located along the horizontal axis The mounting part on the opposite side of the part. The blade units are respectively connected to the mounting portions of the rotating shaft, each blade unit has a plurality of blade modules spaced around the horizontal axis and angularly spaced from each other, each blade module having a grille connecting the rotating shafts. And a plurality of blades mounted to the grille, the grille having at least one airfoil grid extending in an axial direction of the rotating shaft, the airfoil grid extending in a wing-like cross section, and When the fluid passes, a biasing force is generated which deflects the respective mounting portions in a direction opposite to the flow direction.

When the blade modules are driven by the fluid, the rotating shaft is rotated in a running direction, and the biasing force is generated to drive the rotating seat to rotate to a wind receiving position for receiving the wind on the front side of the blade device.

The effect of the novel is that, through the shape design of the airfoil grid bars, a biasing force toward the opposite flow direction can be generated when the fluid passes to drive the blade device to rotate to the wind receiving position, thus The size of the baffle used to drive the rotation of the rotating seat can be reduced to save the material cost of the set of fluid blade devices.

Before the present invention is described in detail, it should be noted that in the following description, similar elements are denoted by the same reference numerals.

Referring to Figures 2 and 3, an embodiment of the novel fluid blade apparatus includes a rotating base 1, a deflector 2, and a vane assembly 3.

The rotating base 1 can be raised by a erecting device 9. The erecting device 9 can be fixed to a ground. The rotating base 1 is pivotally connected to the erecting device 9 and is rotatable relative to the erecting device 9 about a vertical axis V perpendicular to the ground.

The deflector 2 includes an extending arm 21 extending horizontally from the rotating base 1 and a deflector 22 disposed at one end of the extending arm 21 away from the rotating base 1. The deflector 22 is fluidly driven. A deflection force is generated which causes the rotating base 1 to rotate horizontally about the vertical axis V.

The blade device 3 is mounted on the rotating base 1 and can rotate the rotating base 1 and can be driven by the fluid to rotate in a running direction T. The blade device 3 includes a rotating shaft 31 extending along a horizontal axis H, and two A vane unit 32 connected to the rotating shaft 31.

The rotating shaft 31 is pivotally connected to the rotating base 1 along the horizontal axis H. The rotating shaft 31 of the present embodiment is a laterally extending elongated hollow rod body, and has a fulcrum portion 311 located at the middle and pivotally connected to the rotating base 1, and two of the two fulcrum portions 311 along the horizontal axis H. The mounting portion 312 on the opposite side. The mounting portions 312 are elastically bendable relative to the fulcrum portion 311. Since the embodiment is applied to medium and large-scale hydropower generating equipment, the length of the rotating shaft 31 is quite long, even up to several tens to hundreds of meters. Generally, the rotating shaft 31 can be made of metal material under a certain length. The mounting portion 312 can be elastically bent relative to the fulcrum portion 311, but the material of the rotating shaft 31 is not limited to the metal material.

Each of the vane units 32 is coupled to a respective mounting portion 312 and has a plurality of vane modules 33 spaced angularly about the horizontal axis H. Each of the blade modules 33 extends substantially in a radial direction of the rotating shaft 31, and has a grille 34 connecting the rotating shaft 31, and a plurality of blades 35 mounted to the grille 34. The number of the blade modules 33 of the present embodiment is three, and the grids 34 of the blade modules 33 are angularly spaced from each other by 120 degrees. However, the number of the blade modules 33 may be two or four. Or five or more. In addition, the number of the blade units 32 may be an even number of four or more, and is symmetrically disposed on the mounting portions 312, respectively, and is not limited to the embodiment.

Each of the gratings 34 has a plurality of airfoil grids 36 spaced along a radial direction of the one of the rotating shafts 31 and extending in an axial direction of the rotating shaft 31, and a plurality of spaced-apart gates are arranged along the axial direction. Auxiliary grid bars 37 extending in the radial direction, the airfoil grid bars 36 interlacing with the rack bars to collectively define a plurality of matrix-arranged blade spaces 38.

Each airfoil grid 36 extends in a wing-like cross section 361. The cross section 361 includes an inner end 362 and an outer end 363 spaced apart in the radial direction, a flat side 364 extending linearly from the inner end 362 to the outer end 363, and a smoothing by the inner end 362 The ground curve extends to the outer end 363 and projects toward the arcuate side 365 in the running direction T. The arcuate side 365 has an outer arc segment 366 that is gradually curved from the outer end 363 toward the running direction T to a turning point 367, and an inner arc segment that is gradually curved from the turning point 367 to the inner end 362. 368. The turning point 367 is the farthest point of the arcuate side 365 relative to the flat side 364. The extension length L1 of the inner arc segment 368 in the radial direction is greater than the extension length L2 of the outer arc segment 366.

The blades 35 are arranged in a matrix and respectively correspond to the equal blade spaces 38. Each of the blades 35 has a connecting end 351 which is away from the rotating shaft 31 and connected to the grating 34, and a swinging end 352 adjacent to the rotating shaft 31, and each The vanes 35 are movable between a closed position that covers the vane space 38 and the swing end 352 against the grill 34, and an open position that moves the swivel end 352 away from the grill 34.

Referring to FIG. 2, FIG. 4 and FIG. 5, the novel flow blade device is used to demarcate through the horizontal axis H of the rotating shaft 31, and the two blade modules 33 below the rotating shaft 31 are located on the opposite side of the leeward surface. At the same time, the blade module 33 above the rotating shaft 31 is on the forward wind pressure side of the windward surface wind pressure. When the upper blade module 33 is pushed by the fluid in a flow direction F1, since the blades 35 of the blade module 33 are located on the windward side of the grill 34, they are blown to abut against the grill 34. And in the closed position and covering the blade space 38, the blades 35 are further matched with the grating 34 to form a complete windward surface on the windward side, and the two blade modules 33 located below Being pushed away from the grille 34 by the fluid, and in the open position, the fluid can pass through the vane spaces 38, and through the opening and closing of the vanes 35, a large torque rotation can be generated, so that the novel can be subjected to The wind is pushed together with the shaft 31 to rotate in the running direction T.

At the same time, the airfoil grids 36 of each of the blade units 32, when subjected to fluid flow at a particular location, produce a biasing force that deflects the respective mounting portions 312 toward the flow direction F1, as shown in the figure. As shown in FIG. 5, when the airfoil grid 36 is in the lower left position, the blades 35 of the blade module 33 are moved to the open position, and the shape of the airfoil grid 36 is transmitted through the wing. The fluid flow velocity of the arcuate side 365 of the grid bar 36 is relatively fast, and the fluid flow rate through the flat side 364 of the airfoil grid 36 is slow. According to the law of Bernoulli, the faster the fluid flow rate, the lower the pressure. Therefore, the airfoil grid 36 generates a lift force toward the upper left, and a biasing force P toward the opposite flow direction F1 can also be formed.

Referring to FIG. 5 and FIG. 6 , when the airfoil grids 36 generate the biasing force P, the mounting portions 312 on both sides of the rotating shaft 31 are bent relative to the fulcrum portion 311 opposite to the flow direction F1, so that the The rotating shaft 31 has a curved shape, and through the above shape, the blade device 3 can be stably maintained at the wind receiving position.

Referring to FIGS. 5, 6, and 7, when the fluid is changed from the flow direction F1 to the flow direction F2, the baffle 22 is pushed by the fluid to generate a rotating seat 1 to drive the blade device 3 to turn. The deflection force R of the wind receiving position causes the blade device 3 to be steered from the imaginary line position of FIG. 7 in the direction of the arrow A toward the solid line position of FIG. 7. As the blade device 3 is turned, the blade modules 33 and the fluid are The contact area is increased and is subjected to the resistance in the opposite direction to the deflection force R. Then, the airfoil grid 36 is also biased toward the opposite flow direction F2 due to an increase in the contact area with the fluid. And the deflection force R of the baffle 22 is assisted by the biasing force P, and the resistance caused by the fluid can be overcome to drive the rotating base 1 to rotate, so that the blade device 3 is rotated to the wind receiving line as shown in FIG. The position, in this way, assists the rotation of the blade device 3 to the wind receiving position by the assistance of the biasing force P.

It should be noted that, in this embodiment, the number of the airfoil grids 36 of each of the grilles 34 is three, but the number of the airfoil grids 36 may be two, four or more. Each of the grids 34 may also have only one airfoil grid 36, which is not limited to this embodiment.

In summary, the novel flow blade device, through the shape design of the airfoil grids 36, can generate a biasing force P toward the opposite flow direction F1 when the fluid passes, whereby the flow guide The deflection force R provided by the plate 22 can be reduced, and the deflection force R cooperates with the biasing force P to rotate the blade device 3 to the wind receiving position, so that the diversion can be reduced. The size of the plates 22 is to save material costs for the set of flow blade devices.

In addition, since the airfoil grid 36 is originally the grille 34 of the blade module 33, the dimension length of the airfoil grids 36 increases as the size of the blade module 33 increases, and thus, when the user In order to increase the torque and increase the size of the blade modules 33, the size of the airfoil grids 36 is also increased, and a large offset force can be provided to assist the deflection force of the deflector 22, Thereby, the material cost required for increasing the deflector 22 can be reduced, and the object of the present invention can be achieved.

However, the above is only the embodiment of the present invention, and when it is not possible to limit the scope of the present invention, all the simple equivalent changes and modifications according to the scope of the patent application and the contents of the patent specification are still This new patent covers the scope.

1‧‧‧ rotating seat
2‧‧‧Guided rudder
21‧‧‧Extension arm
22‧‧‧Baffle
3‧‧‧blade device
31‧‧‧ shaft
311‧‧‧ fulcrum department
312‧‧‧Installation Department
32‧‧‧blade unit
33‧‧‧ Blade Module
34‧‧‧ Grille
35‧‧‧ blades
351‧‧‧Connecting end
352‧‧‧Swing end
36‧‧‧Airfoil grid
361‧‧‧ cross section
362‧‧‧Inside
363‧‧‧Outside
364‧‧‧ Straight side
365‧‧‧ arc side
366‧‧‧outer arc
367‧‧‧ turning point
368‧‧‧ inner arc
37‧‧‧Auxiliary grid
38‧‧‧Leaf space
9‧‧‧ Erecting device
V‧‧‧vertical axis
H‧‧‧ horizontal axis
F1‧‧‧flow direction
F2‧‧‧flow direction
A‧‧‧ arrow
L1‧‧‧ extended length
L2‧‧‧ extended length
P‧‧‧Offset force
R‧‧‧ deflection force
T‧‧‧direction of operation

Other features and effects of the present invention will be apparent from the following description of the drawings, wherein: FIG. 1 is a perspective view showing a conventional wind blade device; FIG. 2 is a perspective view showing the novel flow blade device Figure 3 is an incomplete cross-sectional side view showing one of the blade modules of the embodiment in an upper position; Figure 4 is a cross-sectional side elevational view showing the embodiment being fluid-driven; 5 is an incomplete cross-sectional side view showing one of the blade modules of the embodiment is located at the lower left position; FIG. 6 is a top plan view illustrating the embodiment in a direction of flow; and FIG. 7 is a top plan view, This embodiment is illustrated as welcoming another flow direction.

1‧‧‧ rotating seat

2‧‧‧Guided rudder

21‧‧‧Extension arm

22‧‧‧Baffle

3‧‧‧blade device

31‧‧‧ shaft

311‧‧‧ fulcrum department

312‧‧‧Installation Department

34‧‧‧ Grille

35‧‧‧ blades

36‧‧‧Airfoil grid

37‧‧‧Auxiliary grid

38‧‧‧Leaf space

9‧‧‧ Erecting device

V‧‧‧vertical axis

H‧‧‧ horizontal axis

32‧‧‧blade unit

33‧‧‧ Blade Module

F1‧‧‧flow direction

T‧‧‧direction of operation

Claims (7)

A fluid blade device that is driven by a fluid flowing in a flow direction and includes: a rotating seat rotatable about a vertical axis; and a vane device mounted to the rotating seat and capable of rotating the rotating seat, and The utility model comprises: a rotating shaft extending along a horizontal axis and pivotably connected to the rotating seat along the horizontal axis, the rotating shaft has a fulcrum portion located in the middle and pivoted to the rotating seat, and two along the horizontal axis a mounting portion on opposite sides of the fulcrum portion, and a plurality of vane units respectively connected to the mounting portions of the rotating shaft, each vane unit having a plurality of vane modules angularly spaced around the horizontal axis Each blade module has a grille connecting the rotating shaft, and a plurality of blades mounted on the grille, the grille having at least one airfoil grid extending in an axial direction of the rotating shaft, the airfoil grid The rod extends in a wing-like cross section and, when the fluid passes therethrough, creates a biasing force that deflects the respective mounting portions against the flow direction, When the blade module driven by a fluid, it will drive the spindle is rotated in one direction of operation and generate the biasing force to drive the rotation of the rotary base to a receiving device that the front of the blade position of the wind by the wind. The fluid blade apparatus of claim 1, wherein the mounting portions are elastically bendable relative to the fulcrum portion, and the biasing force generated by the airfoil grid rod can drive the respective mounting portions relative to the fulcrum The part is bent in the opposite direction to the flow direction. The fluid blade apparatus of claim 2, wherein the airfoil grid has a cross section having an inner end and an outer end spaced apart in a radial direction of the rotating shaft, and a straight line extending from the inner end to a flat side of the outer end, and an arcuate side that smoothly curves from the inner end to the outer end and projects toward the running direction. The fluid blade device of claim 3, wherein the arcuate side has an outer arc segment that is gradually curved from the outer end toward the running direction to a turning point, and a curve is gradually curved from the turning point to An inner arc segment of the inner end, the inflection point being the farthest point of the arc convex side relative to the straight side, the inner arc segment extending in the radial direction being greater than the outer arc segment. The fluid blade device of claim 4, further comprising a flow guiding rudder fixed to the rotating seat, the guiding rudder including an extending arm horizontally extending from the rotating seat, and a extending arm disposed at the extending arm A baffle that rotates one end of the seat, and when the baffle is pushed by the fluid, a deflection force is generated that causes the rotating seat to rotate to drive the blade device to the wind receiving position. The fluid blade apparatus of claim 1, wherein the grid comprises a plurality of matrix-arranged blade spaces, the blades are arranged in a matrix and respectively correspond to the blade space, each blade having a distance from the rotation axis and connecting a connecting end of the grille, and a swinging end adjacent to the rotating shaft, each vane being in a closed position covering the vane space and abutting the swinging end against the grille, and a swinging end away from the grille Move between open positions. The fluid blade apparatus of claim 6, wherein the grid of each blade module comprises a plurality of airfoil grids spaced along the radial direction, and a plurality of spaced along the axial direction An auxiliary grid extending in the radial direction, the airfoil grids and the auxiliary grids together define the blade spaces.