阅读说明：本技术 一种风能发电能力短期预测设备 (Short-term prediction equipment for wind power generation capacity ) 是由 区志华 于 2021-07-16 设计创作，主要内容包括：本发明公开了一种风能发电能力短期预测设备,其结构包括：发动机壳槽、小旋桨轴座槽、轴套环框、旋桨轴罩帽、柱筒支座,本发明实现了运用小旋桨轴座槽与轴套环框相配合,通过旋桨轴罩帽对接小旋桨板与转轴杆支座形成小型风动短期预测和风能发电能力的续航转子微转连续减速操作,使整体环框槽的捕捉风向和隔振效率形成微调和防晃动操作效果,让后续的风力发电机械触发和设备停转形成一个缓冲养护轴动的操作效果,提升预测短防护度和检测效率。(The invention discloses a short-term prediction device for wind power generation capacity, which structurally comprises: the invention realizes the micro continuous speed reduction operation of a small-sized pneumatic short-term prediction and a cruising rotor with wind energy generating capacity by matching the small propeller shaft seat groove and the shaft sleeve ring frame and butting the small propeller plate and the rotating shaft rod support through the propeller shaft hood, so that the wind direction capturing and vibration isolating efficiency of the whole ring frame groove form fine adjustment and anti-shaking operation effects, the subsequent mechanical triggering of wind power generation and equipment stopping form an operation effect of buffering the maintenance shaft movement, and the prediction short protection degree and the detection efficiency are improved.)

1. A short-term prediction device for wind power generation capacity structurally comprises: engine housing groove (1), little oar axle seat groove (2), axle sleeve ring frame (3), oar axle hood (4), column casing support (5), its characterized in that revolve:

the small propeller shaft seat groove (2) is inserted and embedded at the right side of the shaft sleeve ring frame (3), the engine shell groove (1) and the small propeller shaft seat groove (2) are embedded into a whole, the propeller shaft hood cap (4) is installed at the left side of the shaft sleeve ring frame (3), the column casing support (5) is inserted and embedded under the bottom of the engine shell groove (1), and the small propeller shaft seat groove (2) is mechanically connected with the propeller shaft hood cap (4) through the shaft sleeve ring frame (3);

the small propeller shaft seat groove (2) is provided with a small propeller plate (2A), a rotating shaft rod support seat (2B) and a shell cover groove (2C);

the two small propeller plates (2A) are respectively arranged at the upper end and the lower end of the right side of the rotating shaft rod support (2B), the rotating shaft rod support (2B) is inserted and embedded in the shell cover groove (2C), and the shell cover groove (2C) is inserted and embedded at the right side of the shaft sleeve ring frame (3).

2. The wind power generation capability short term prediction device of claim 1, wherein: the small propeller plate (2A) is composed of a grating hub plate (2A1) and an ellipsoid wing plate (2A2), the grating hub plate (2A1) is installed on the top of the ellipsoid wing plate (2A2), and the grating hub plate (2A1) and the ellipsoid wing plate (2A2) are buckled together.

3. The wind power generation capability short-term prediction device of claim 2, wherein: the grille wheel hub plate (2A1) is composed of a grille arc lath (2A11) and a cross plate frame (2A12), the grille arc lath (2A11) is installed inside the cross plate frame (2A12), and the grille arc lath (2A11) is tightly attached to the cross plate frame (2A 12).

4. The wind power generation capability short term prediction device of claim 1, wherein: the rotating shaft rod support (2B) is composed of a trapezoidal shifting block (2B1) and a supporting rod bearing seat (2B2), the trapezoidal shifting block (2B1) is installed on the left side of the supporting rod bearing seat (2B2), and the trapezoidal shifting block (2B1) and the supporting rod bearing seat (2B2) are nested into a whole.

5. The wind power generation capability short-term prediction device of claim 4, wherein: trapezoidal piece (2B1) is dialled by trapezoidal groove piece (2B11), slot joint and is dialled a board (2B12) and constitute, slot joint is dialled a board (2B12) and is equipped with more than two and insert respectively and inlay in the upper and lower both sides of trapezoidal groove piece (2B11) inside, slot joint is dialled a board (2B12) and trapezoidal groove piece (2B11) and is inserted and inlays together.

6. The wind power generation capability short term prediction device of claim 1, wherein: the engine shell groove (1) is composed of sliding cushion blocks (11) and a shell groove body (12), the sliding cushion blocks (11) are arranged on the upper side and the lower side of the interior of the shell groove body (12) and are installed on the upper side and the lower side of the interior of the shell groove body (12) respectively, and the sliding cushion blocks (11) are matched with the shell groove body (12).

7. The wind power generation capability short-term prediction device of claim 6, wherein: the sliding cushion block (11) is composed of a sliding block groove (111) and a spring plate frame (112), the spring plate frame (112) is installed inside the sliding block groove (111), and the sliding block groove (111) and the spring plate frame (112) are nested into a whole.

8. The wind power generation capability short term prediction device of claim 1, wherein: the shaft sleeve ring frame (3) is composed of two pull rod buckling blocks (31) and a ring frame groove (32), the two pull rod buckling blocks (31) are arranged on the right side of the ring frame groove (32), and the pull rod buckling blocks (31) are buckled with the ring frame groove (32) together.

9. The wind power generation capability short term prediction device of claim 8, wherein: the pull rod buckling block (31) is composed of a ball rod frame (311) and a buckling groove (312), the ball rod frame (311) is installed inside the buckling groove (312), and the ball rod frame (311) is inserted into the buckling groove (312) in an embedded mode.

Technical Field

The invention discloses short-term prediction equipment for wind power generation capacity, and belongs to the field of wind power machinery.

Background

Wind power generation is to the axle movable motor drive and the wind-force drive linking operation make the stability and the electric current protection degree of equipment butt joint need promote, guarantees the promotion of wind power generation mechanical linkage efficiency promotion and the promotion of security of large-scale equipment, and the public shortcoming of treating the optimization of prior art has:

the endurance of wind power generation to the electric power and the short-term wind direction prediction need synchronous operation, but a propeller and a shaft moving rack of the device are large, the control degree of a micro wind direction operation handle is insufficient, the wind direction actual force is easy to operate and predict, the linkage operation efficiency of strong wind power generation is missed, and the integrated electric control precision and mechanical regulation of a swinging end and a tailstock end are insufficient, so that the power generation prediction efficiency is low.

Disclosure of Invention

Aiming at the defects in the prior art, the invention aims to provide short-term prediction equipment for wind power generation capacity, which aims to solve the problems that the endurance of wind power generation to the power capacity and the short-term wind direction prediction need synchronous operation, but a propeller and a shaft moving rack of the equipment are large, the control degree of a micro-motion wind direction operation handle is insufficient, the wind direction actual force is easy to operate and predict, the linkage operation efficiency of strong wind power generation is missed, and the integrated electric control precision and mechanical adjustment of a swing end and a tailstock end are insufficient, so that the power generation prediction efficiency is low.

In order to achieve the purpose, the invention is realized by the following technical scheme: a short-term prediction device for wind power generation capacity structurally comprises: the engine comprises an engine shell groove, a small propeller shaft seat groove, a shaft sleeve ring frame, a propeller shaft hood and a cylindrical support seat, wherein the small propeller shaft seat groove is inserted and embedded at the right side of the shaft sleeve ring frame, the axes of the small propeller shaft seat groove are collinear, the engine shell groove and the small propeller shaft seat groove are nested into a whole and are positioned on the same horizontal plane, the propeller shaft hood cap is arranged on the left side of the shaft sleeve ring frame, the axes of the propeller shaft hood cap are collinear, the column casing support is inserted and embedded under the bottom of the engine casing groove and is vertical to each other, the small propeller shaft seat groove is mechanically connected with the propeller shaft cover cap through a shaft sleeve ring frame, the axes of the small propeller shaft seat groove and the propeller shaft cover cap are collinear, the small propeller shaft seat groove is provided with two small propeller plates, a rotating shaft rod support and a shell cover groove, the two small propeller plates are respectively arranged at the upper end and the lower end of the right side of the rotating shaft rod support, the rotating shaft rod support is inserted and embedded in the shell cover groove, the axis of the rotating shaft rod support is collinear, and the shell cover groove is inserted and embedded on the right side of the shaft sleeve ring frame, and the axis of the shell cover groove is collinear.

In order to optimize the technical scheme, the method further comprises the following steps:

as a further improvement of the invention, the small rotor plate consists of a grid hub plate and an ellipsoidal wing plate, the grid hub plate is installed on the top of the ellipsoidal wing plate, and the grid hub plate and the ellipsoidal wing plate are buckled together and are positioned on the same vertical plane.

As a further improvement of the invention, the grating hub plate is composed of a grating arc lath and a cross plate frame, the grating arc lath is installed inside the cross plate frame, and the grating arc lath and the cross plate frame are tightly attached together and are positioned on the same vertical surface.

As a further improvement of the invention, the rotating shaft rod support is composed of a trapezoidal shifting block and a supporting rod bearing seat, the trapezoidal shifting block is arranged on the left side of the supporting rod bearing seat, and the trapezoidal shifting block and the supporting rod bearing seat are nested into a whole and the axes of the trapezoidal shifting block and the supporting rod bearing seat are collinear.

As a further improvement of the invention, the trapezoidal shifting block consists of a trapezoidal groove block and a slot-opening shifting plate, the slot-opening shifting plate is provided with more than two slots and is respectively inserted and embedded in the upper side and the lower side of the inner part of the trapezoidal groove block, and the slot-opening shifting plate and the trapezoidal groove block are inserted and embedded together and are positioned on the same vertical surface.

As a further improvement of the invention, the engine shell groove consists of two sliding cushion blocks and a shell groove body, the two sliding cushion blocks are respectively arranged at the upper side and the lower side inside the shell groove body, and the sliding cushion blocks and the shell groove body are in interference fit.

As a further improvement of the invention, the sliding cushion block consists of a slider groove and a spring plate frame, wherein the spring plate frame is arranged inside the slider groove, and the slider groove and the spring plate frame are nested into a whole and are positioned on the same horizontal plane.

As a further improvement of the invention, the shaft sleeve ring frame is composed of two pull rod buckling blocks and a ring frame groove, the two pull rod buckling blocks are arranged on the right side of the ring frame groove, and the pull rod buckling blocks and the ring frame groove are buckled together and are mutually vertical.

As a further improvement of the invention, the pull rod buckle block consists of a ball rod frame and a buckle groove, wherein the ball rod frame is arranged inside the buckle groove, and the ball rod frame and the buckle groove are inserted and embedded together and are positioned on the same horizontal plane.

As a further improvement of the invention, the grid arc slat is of a composite plate groove structure with arc strips overlapped with a four-position air gap cover cap, so that the wind pressure sensing is facilitated, and breeze storage is facilitated to ensure the short-term wind direction prediction linkage deflection operation effect.

As a further improvement of the invention, the slot-seam plectrum plate is of a composite plectrum structure with a fin plate at the top and a narrow frame opening at the bottom, so that the row plate can be conveniently slammed to form the sensing operation effect of an electric plate in the vibrating screen.

As a further improvement of the invention, the spring plate frame is of a plate frame structure with double transverse plates and spring wire seats, so that the operation of upper and lower transverse supports is facilitated, the whole cushion operation is subsequently promoted, the collision of the shell is prevented, and the whole assembly attaching degree is ensured.

As a further improvement of the invention, the buckle groove is a composite buckle block structure with buckle jump grooves in the left and right arc buckle plates, so that the double shells are conveniently pressed to form the operation effect of penetrating the pull buckle.

Advantageous effects

The invention relates to short-term prediction equipment for wind power generation capacity.A worker sleeves a shell groove body of an engine shell groove with a shell cover groove of a small propeller shaft seat groove, so that a gap between a sliding block groove of a sliding cushion block and a spring plate frame is filled in the shell groove body, and grid hub pull buckle ellipsoid wing plates of a small propeller plate are turned over at a support rod bearing seat of a rotating shaft rod support to form a small rotor absorption wind pressure matched and butted trapezoid groove blocks of a trapezoid shifting block and a slot opening shifting plate to predict wind direction and wind power operation effects, so that a shaft sleeve ring frame butted propeller shaft cover cap is matched with a predicted swing angle fine adjustment operation effect at the top of a cylindrical support to match with the operation effect of short-term prediction and maintenance of the end of a bearing generator set for wind power generation capacity.

The invention has the following advantages after operation:

the small propeller shaft seat slot is matched with the shaft sleeve ring frame, the small propeller plate and the rotating shaft rod support are butted through the propeller shaft hood to form small pneumatic short-term prediction and continuous speed reduction operation of continuous rotation of a endurance rotor of wind power generation capacity, the wind direction capturing and vibration isolation efficiency of the whole ring frame slot forms fine adjustment and anti-shaking operation effects, the subsequent wind power generation machinery is triggered and the equipment stops to form an operation effect of buffering maintenance shaft movement, and the prediction short protection degree and the detection efficiency are improved.

Drawings

Other features, objects, and advantages of the present invention will become more apparent from the following detailed description of the embodiments of the invention when taken in conjunction with the accompanying drawings, in which:

fig. 1 is a schematic structural diagram of a short-term wind power generation capacity prediction device according to the present invention.

FIG. 2 is a detailed sectional structure diagram of the engine casing slot and the small propeller shaft seat slot of the present invention.

Fig. 3 is a detailed cross-sectional structural diagram of the shaft seat groove and the shaft collar frame of the small propeller of the present invention.

Fig. 4 is a detailed sectional structure diagram of the small rotor shaft seat groove, the small rotor plate and the rotating shaft rod seat of the invention.

FIG. 5 is an enlarged cross-sectional view of the sliding pad of the present invention in an operating state.

Fig. 6 is an enlarged cross-sectional structural view of the pull rod buckle block in the working state of the present invention.

Fig. 7 is an enlarged sectional view of the hub plate of the grill of the present invention in an operating state.

FIG. 8 is an enlarged cross-sectional view of the trapezoidal pick block according to the present invention.

Description of reference numerals: the engine comprises an engine shell groove-1, a small propeller shaft seat groove-2, a shaft sleeve ring frame-3, a propeller shaft cover cap-4, a cylinder support-5, a small propeller plate-2A, a rotating shaft rod support-2B, a shell cover groove-2C, a grid hub disc-2A 1, an ellipsoid wing plate-2A 2, a grid arc strip plate-2A 11, a cross disc frame-2A 12, a trapezoid shifting block-2B 1, a support rod bearing seat-2B 2, a trapezoid groove block-2B 11, a slot shifting plate-2B 12, a sliding pad block-11, a shell groove body-12, a sliding block groove-111, a reed plate frame-112, a pull rod buckle block-31, a ring frame groove-32, a ball rod frame-311 and a buckle groove-312.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.

The first embodiment is as follows:

referring to fig. 1 to 8, the present invention provides a short-term prediction apparatus for wind power generation capability, which comprises: the engine comprises an engine shell groove 1, a small propeller shaft seat groove 2, a shaft sleeve ring frame 3, a propeller shaft cover cap 4 and a cylindrical support 5, wherein the small propeller shaft seat groove 2 is inserted and embedded at the right side of the shaft sleeve ring frame 3 and the axes of the small propeller shaft seat groove 2 are collinear, the engine shell groove 1 and the small propeller shaft seat groove 2 are nested into a whole and are positioned on the same horizontal plane, the propeller shaft cover cap 4 is installed at the left side of the shaft sleeve ring frame 3 and the axes of the small propeller shaft cover cap are collinear, the cylindrical support 5 is inserted and embedded at the bottom of the engine shell groove 1 and are vertical to each other, the small propeller shaft seat groove 2 is mechanically connected with the propeller shaft cover cap 4 through the shaft sleeve ring frame 3 and the axes of the small propeller shaft seat groove 2 are collinear, the small propeller plate 2A, a rotating shaft rod support 2B and a shell cover groove 2C are arranged, the small propeller plates 2A are provided with two small propeller plates and are respectively installed at the upper end and the lower end of the right side of a rotating shaft rod support 2B, the rotating shaft rod support 2B is inserted and embedded in the shell cover groove 2C and the axes of the same are collinear, the housing cover groove 2C is inserted and embedded at the right side of the shaft sleeve ring frame 3, and the axes are collinear.

Referring to fig. 4, the small rotor plate 2A is composed of a grid hub plate 2A1 and an ellipsoidal wing plate 2A2, the grid hub plate 2A1 is installed on the top of the ellipsoidal wing plate 2A2, the grid hub plate 2A1 and the ellipsoidal wing plate 2A2 are buckled together and are located on the same vertical plane, the rotating shaft support 2B is composed of a trapezoidal dial block 2B1 and a support rod bearing seat 2B2, the trapezoidal dial block 2B1 is installed on the left side of the support rod bearing seat 2B2, the trapezoidal dial block 2B1 and the support rod bearing seat 2B2 are nested into a whole and have collinear axes, and the grid hub plate 2A1 and the support rod bearing seat 2B2 form an operation effect of rotating the rotor, so that the operation efficiency of the small rotor is realized.

Referring to fig. 7, the grille hub 2a1 is composed of a grille arc slat 2a11 and a cross plate frame 2a12, the grille arc slat 2a11 is installed inside the cross plate frame 2a12, the grille arc slat 2a11 and the cross plate frame 2a12 are tightly attached together and located on the same vertical plane, the grille arc slat 2a11 is a composite plate slot structure with arc strips overlapping with a four-position air gap cover, wind pressure sensing is facilitated, breeze storage is guaranteed to guarantee a short-term prediction linkage deflection operation effect of wind direction, and the operation effect of slot air leakage pouring and adjustment of wind direction deflection pulling is formed by attaching the grille arc slat 2a11 and the cross plate frame 2a 12.

Referring to fig. 8, the trapezoidal tab shifting block 2B1 is composed of a trapezoidal groove block 2B11 and a slot tab shifting plate 2B12, the slot tab shifting plate 2B12 is provided with more than two slots and is respectively inserted and embedded in the upper side and the lower side of the inside of the trapezoidal groove block 2B11, the slot tab shifting plate 2B12 and the trapezoidal groove block 2B11 are inserted and embedded together and are located on the same vertical plane, the slot tab shifting plate 2B12 is a composite tab structure with a narrow frame opening at the bottom of a fin plate at the top, so that a flap can be conveniently moved to form an inner electric plate sensing operation effect of the vibrating screen, and a tab disturbing wind direction is formed by the trapezoidal groove block 2B11 and the slot tab shifting plate 2B12 to accommodate and realize an operation effect of short-term wind pressure prediction.

Referring to fig. 2, the engine casing groove 1 is composed of two sliding pad blocks 11 and a casing groove body 12, the two sliding pad blocks 11 are respectively installed at the upper side and the lower side inside the casing groove body 12, the sliding pad blocks 11 and the casing groove body 12 are in interference fit, and the casing groove body 12 is formed with an operation effect that the casing is filled with anti-skidding materials from the upper side and the lower side.

Referring to fig. 5, the sliding pad 11 is composed of a slider groove 111 and a spring plate frame 112, the spring plate frame 112 is installed inside the slider groove 111, the slider groove 111 and the spring plate frame 112 are nested into a whole and are located on the same horizontal plane, the spring plate frame 112 is a plate frame structure with a spring wire seat on two transverse plates, so that the operation of upper and lower cross braces is facilitated, the subsequent lifting of the whole cushion operation is facilitated, the case collision is prevented, the whole assembling fitting degree is ensured, the sliding damping sliding is performed by the lateral movement of the spring plate frame 112 wrapped by the slider groove 111, and the operation effect of tension wrapping cushion protection is formed by the cooperation of the elastic pressure.

The working process is as follows: the working personnel cup joint the shell groove 12 of the engine shell groove 1 with the shell cover groove 2C of the small propeller shaft seat groove 2, so that the sliding block groove 111 of the sliding cushion block 11 and the spring plate frame 112 cushion the shell gap, and ensure that the grid hub disc 2A1 pull buckle ellipsoid wing plate 2A2 of the small propeller plate 2A overturns the grid arc slat 2A11 and the cross disc frame 2A12 at the support rod bearing seat 2B2 of the rotating shaft rod support 2B to form the trapezoidal groove block 2B11 and the slot seam deflector 2B12 of the small rotor absorption wind pressure matching butting trapezoidal deflector block 2B1 to predict the wind direction and wind force operation effect, so that the shaft sleeve ring frame 3 butting the propeller shaft cover cap 4 is matched with the predicted swing direction angle fine adjustment operation effect at the top of the cylindrical support 5 to match the operation effect of the wind power generation capacity short-period prediction maintenance bearing generator set end.

Example two:

referring to fig. 1 to 8, the present invention provides a short-term prediction apparatus for wind power generation capability, which is otherwise the same as embodiment 1 except that:

referring to fig. 3, the collar ring frame 3 is composed of two pull rod fastening blocks 31 and a ring frame groove 32, the two pull rod fastening blocks 31 are installed on the right side of the ring frame groove 32, the pull rod fastening blocks 31 are fastened with the ring frame groove 32 and are perpendicular to each other, and the pull rod fastening blocks 31 are matched with the pull fasteners on the ring frame groove 32-side to form the stability effect of the integral rotation operation.

Referring to fig. 6, the pull rod buckle block 31 is composed of a ball rod frame 311 and a buckle groove 312, the ball rod frame 311 is installed inside the buckle groove 312, the ball rod frame 311 and the buckle groove 312 are inserted and embedded together and are located on the same horizontal plane, the buckle groove 312 is a composite buckle block structure with buckle jump grooves in left and right arc buckle plates, so that a double-shell body can be conveniently pressed and installed to form an operation effect of penetrating through the buckle, the ball rod frame 311 assists a top support in the buckle groove 312 to form an operation effect of preventing repeated impact and damage, and the operation effect of preventing the buckle from being released is improved.

The overall transverse and longitudinal wind stress short-term prediction operation is formed through the tailstock of the early-stage wind power generation equipment, so that the pull rod buckle block 31 of the shaft sleeve ring frame 3 is assisted in clamping and shaft movement tripping prevention at the right side of the ring frame groove 32 through the ball rod frame 311 and the buckle groove 312 to form a linkage stable operation effect of the rotor propeller and the large-wing-plate propeller.

The invention achieves the purposes of utilizing the small propeller shaft seat slot 2 to be matched with the shaft sleeve ring frame 3, forming the micro continuous speed reduction operation of the endurance rotor with small pneumatic short-term prediction and wind power generation capacity by butting the small propeller plate 2A with the rotating shaft rod support 2B through the propeller shaft cover cap 4, forming the fine adjustment and anti-shaking operation effects of the wind capturing direction and the vibration isolation efficiency of the integral ring frame slot 32, forming the operation effect of buffering and maintaining the shaft motion by the subsequent mechanical triggering and the equipment stopping of the wind power generation, improving the prediction short protection degree and the detection efficiency, solving the problems that the endurance and the short-term wind direction prediction of the wind power generation need synchronous operation, but the propeller and the shaft motion frame of the equipment are large, the control degree of the micro wind direction operation is insufficient, the linkage operation efficiency of easily operating and predicting the wind direction actual force missing strong wind power generation is high, and the electric control precision and the mechanical adjustment of the swing end and the tail seat end are insufficient, the power generation prediction efficiency is low.

The specific embodiments described herein are merely illustrative of the invention. Various modifications or additions may be made to the described embodiments or alternatives may be employed by those skilled in the art without departing from the scope of the invention or exceeding the scope of the claims appended hereto.