WO2012039249A1 - Mécanisme à pale rotative et dispositif de production d'énergie l'utilisant - Google Patents

Mécanisme à pale rotative et dispositif de production d'énergie l'utilisant Download PDF

Info

Publication number
WO2012039249A1
WO2012039249A1 PCT/JP2011/069812 JP2011069812W WO2012039249A1 WO 2012039249 A1 WO2012039249 A1 WO 2012039249A1 JP 2011069812 W JP2011069812 W JP 2011069812W WO 2012039249 A1 WO2012039249 A1 WO 2012039249A1
Authority
WO
WIPO (PCT)
Prior art keywords
sprocket
blade
rotating
wind direction
wind
Prior art date
Application number
PCT/JP2011/069812
Other languages
English (en)
Japanese (ja)
Inventor
宮本　啓一
純 堤田
Original Assignee
有限会社グローバルリング
株式会社セルフ
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 有限会社グローバルリング, 株式会社セルフ filed Critical 有限会社グローバルリング
Publication of WO2012039249A1 publication Critical patent/WO2012039249A1/fr

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F03D7/06—Controlling wind motors  the wind motors having rotation axis substantially perpendicular to the air flow entering the rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/06—Rotors
    • F03D3/062—Rotors characterised by their construction elements
    • F03D3/066—Rotors characterised by their construction elements the wind engaging parts being movable relative to the rotor
    • F03D3/067—Cyclic movements
    • F03D3/068—Cyclic movements mechanically controlled by the rotor structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/50—Kinematic linkage, i.e. transmission of position
    • F05B2260/503—Kinematic linkage, i.e. transmission of position using gears
    • F05B2260/5032—Kinematic linkage, i.e. transmission of position using gears of the bevel or angled type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the present invention relates to a rotating blade for generating a rotational force by using a fluid motion.
  • the present invention relates to a so-called vertical axis type rotary blade mechanism and a power generation apparatus using the same.
  • wind turbines having a rotation axis parallel to the wind direction have been put to practical use for wind power generation.
  • this windmill basically, huge blades rotate in a virtual plane orthogonal to the wind direction.
  • the following problems have been pointed out.
  • -Birds have the habit of flying toward the downstream of the wind in order to search for updrafts. Then, it is easy to collide with the blade
  • a parallel axis type windmill has a height of about 100 meters from the ground surface to the upper end of the blade in order to improve power generation efficiency.
  • a main object of the present invention is to provide a technique capable of making a rotor blade and a fluid flow direction parallel by utilizing a fluid flow when the fluid velocity is excessive.
  • the present invention can be expressed as the contents described in the following items.
  • (Item 1) Revolving shaft, rotating body, first rotating blade, second rotating blade, wind direction shaft, fixed sprocket, first movable sprocket, rotational force transmission mechanism, first key member, and second key member And a key drive mechanism,
  • the rotating body is rotatable around the revolution axis
  • the first rotating blade and the second rotating blade are attached to the rotating body, and thereby, each of these rotating blades is configured to revolve around the revolution axis
  • the first rotor blade includes a first rotating sprocket
  • the second rotor blade includes a second rotating sprocket
  • the wind direction axis is provided with a wind direction plate for receiving wind force, and the wind direction axis is rotatable with respect to the revolution axis according to the direction of the wind force to the wind direction plate
  • the fixed sprocket is fixed to the wind direction axis and is rotatable according to the rotation of the wind direction axis
  • the first movable sprocket is
  • the first movable sprocket includes a first engagement portion and a second engagement portion
  • the rotational force transmission mechanism is configured to transmit rotational force in the same direction between the fixed sprocket and the first rotating sprocket of the first rotating blade.
  • the first rotating sprocket is configured to rotate in the direction opposite to the revolution
  • the rotational force transmission mechanism is configured to transmit rotational force in the same direction between the first movable sprocket and the second rotating sprocket of the second rotary blade, whereby the second By the revolution of the rotation sprocket, the second rotation sprocket is rotated in the direction opposite to the revolution
  • the first key member is configured to be able to detachably engage with the first engagement portion to fix the first movable sprocket and the wind direction shaft, In the state where the first hook member is engaged with the first engaging portion, when the second rotating blade reaches the same revolution angle as the first rotating blade, the second rotating blade rotates.
  • the angle is substantially equal to the rotation angle of the first rotor blade
  • the second hook member is configured to be able to detachably engage with the second engagement portion to fix the first movable sprocket and the wind direction shaft, And in the state where the second key member is engaged with the second engagement portion, the second rotary blade is substantially parallel to the first rotary blade,
  • the key drive mechanism is configured to engage the first key member with the first engaging portion in a normal state and to engage the second key member with the second engaging portion in a strong wind. Characteristic rotary blade mechanism.
  • Item 2 In a state where the first key member is detached from the first engaging portion and the second key member is not engaged with the second engaging portion, the first movable sprocket is rotated in the second rotation.
  • Item 1 is configured to rotate by receiving the rotational force generated by the rotation of the blade through the rotational force transmission mechanism, whereby the second engagement portion reaches the position of the second key member.
  • the rotor blade mechanism according to 1.
  • a power generator that generates electric power by using the revolution force of the rotating body in the rotary blade mechanism according to any one of items 1 to 5 as a rotational force for power generation.
  • FIG. 1 is an overall cross-sectional view of a rotary blade mechanism according to a first embodiment of the present invention.
  • only two rotor blades are shown.
  • It is an enlarged view of the revolution shaft in a rotary blade mechanism.
  • It is a schematic explanatory drawing of the rotary body in a rotary blade mechanism.
  • only two rotor blades are shown.
  • It is a schematic top view for demonstrating the rotation angle of a rotary blade.
  • It is a cross-sectional view of a rotary blade. It is an enlarged view of a wind direction axis. It is an expanded sectional view about the principal part of a wind direction axis.
  • FIG. 10A shows a state in which the first key member is fitted into the first engagement portion.
  • FIG. 10B shows a state in which the second key member is fitted into the second engaging portion.
  • FIG. 3C shows a state in which the second key member is fitted into the second engaging portion of the first movable sprocket and subsequently fitted into the second engaging portion of the second movable sprocket. It is explanatory drawing for demonstrating schematically the state in which each rotary blade became parallel. It is explanatory drawing for demonstrating the rotary blade mechanism which concerns on 2nd Embodiment using planar view and longitudinal cross-sectional view.
  • Fig. (A) shows the use of 8 blades
  • Fig. (B) shows the use of 4 blades
  • Fig. (C) shows the use of 2 blades
  • Fig. (D) shows the state of not using all the blades.
  • FIG. 4A is an explanatory diagram for explaining the positional relationship between the first engagement portion and the second engagement portion in the fixed sprocket.
  • FIG. 5B is a schematic explanatory diagram for explaining the mutual positional relationship (angular relationship) between the first engaging portion and the second engaging portion in the seven movable sprockets and the one fixed sprocket. is there. It is explanatory drawing for demonstrating the rotary blade mechanism which concerns on 3rd Embodiment. It is explanatory drawing for demonstrating the rotary blade mechanism which concerns on 4th Embodiment.
  • FIG. 19A is a view corresponding to the plan view of FIG. Fig. (B) is an arrow view of the main part of the B direction in Fig. (A). It is a figure equivalent to the side view which fractured
  • the rotary blade mechanism of the present embodiment has a so-called vertical axis type structure.
  • gas ie, a wind force
  • a rotational force is used as an example of the fluid for obtaining a rotational force.
  • the rotating blade mechanism of the present embodiment includes a revolution shaft 1, a rotating body 2, a first rotating blade 3, a second rotating blade 4, a third rotating blade 5, a wind direction shaft 6, a fixed sprocket 7, A first movable sprocket 8, a second movable sprocket 9, a rotational force transmission mechanism 10, a first key member 11, a second key member 12, and a key drive mechanism 13 are provided (FIGS. 1 and 4). And FIG. 7).
  • the revolution shaft 1 is erected on a plane (for example, the ground) as shown in FIGS. 1 and 2. Inside the revolution shaft 1, a space 1a extending in the direction of the axis is formed.
  • Rotating body 2 is rotatable around the revolution axis 1. Specifically, the rotating body 2 is attached to the revolution shaft 1 via a bearing 2a (see FIG. 1), and thereby, rotation about the revolution shaft 1 is possible.
  • the rotating body 2 includes a lower support 2b and an upper support 2c for supporting each wind receiving blade (see FIG. 3).
  • the first to third rotor blades 3 to 5 are attached to the rotating body 2 so as to be able to rotate (see FIGS. 1 and 4).
  • FIG. 1 and FIG. 3 only two rotor blades are shown for simplicity of explanation.
  • the lower end of each rotor blade is rotatably supported by the lower support 2b, and the upper end of each rotor blade is rotatably supported by the upper support 2c.
  • a bearing can be used, for example.
  • each of these rotor blades can revolve around the revolution shaft 1.
  • the first to third rotating blades 3 to 5 are provided with first to third rotating sprockets 31 to 51 (see FIG. 4).
  • the rotating sprockets 31 to 51 are connected to the sprockets 7 to 9 (see FIG. 7) attached to the wind direction shaft 6 via the rotational force transmission mechanism 10 (described later).
  • Each rotor blade has a substantially flat plate shape as shown in FIG. Further, in the present embodiment, each rotor blade has a rising portion 32 or 42 that rises in the opposite direction to the rotation direction at both ends in the radial direction during rotation of each rotor blade (the ends in the left-right direction in FIG. 5). 52 (not shown in FIG. 4) are provided.
  • the wind direction shaft 6 includes a wind direction plate 61 for receiving wind force (see FIG. 6). Further, the wind direction axis 6 is rotatable with respect to the revolution axis 1 according to the direction of the wind force toward the wind direction plate 61. Specifically, the wind direction shaft 6 is inserted into a space 1a formed inside the revolution shaft 1, and is attached to the revolution shaft 1 via a bearing. Thereby, the wind direction axis
  • the fixed sprocket 7 is fixed to the outer surface of the wind direction shaft 6 and can be rotated according to the rotation of the wind direction shaft 6 (see FIG. 7).
  • the first movable sprocket 8 and the second movable sprocket 9 are attached to the outer surface of the wind direction shaft 6 and are rotatable about the wind direction shaft 6. As will be described later, at the normal time, the first and second movable sprockets 8 and 9 are fixed by the first hook member 11 so as to maintain a predetermined rotation angle with respect to the wind direction shaft 6.
  • Stoppers 14a and 14b for preventing the movement of these sprockets in the axial direction are arranged above the first movable sprocket 8 and below the second movable sprocket 9. These stoppers 14a and 14b are both fixed to the outer surface of the wind direction shaft 6 with screws. However, the means for fixing these stoppers is not particularly limited, and for example, an adhesive may be used. Note that these stoppers 14a and 14b themselves do not prevent the first and second movable sprockets 8 and 9 from rotating about the axis.
  • the first movable sprocket 8 includes a first engagement portion 81 and a second engagement portion 82 (see FIG. 7).
  • the positional relationship between the first engagement portion 81 and the second engagement portion 82 is shown in FIG.
  • the distance from the axis of the revolution shaft 1 to the second engagement portion 82 is different from the distance from the axis of the revolution shaft 1 to the first engagement portion 81.
  • the second engaging portion 82 is formed at a position of about 120 ° clockwise from the first engaging portion 81 in the drawing.
  • Grooves 81a and 82a are formed in the first engaging portion 81 and the second engaging portion 82 for smooth insertion operation of the first and second key members 11 and 12, which will be described later (see FIG. 10). ).
  • FIG. 10 schematically shows a state transition when the first and second hook members engage with the first and second engaging portions.
  • the second movable sprocket 9 also includes a first engagement portion 91 and a second engagement portion 92 (see FIG. 7). As will be described later, the second engaging portion 92 of the second movable sprocket 9 is disposed at a position (phase angle) different from the second engaging portion 82 of the first movable sprocket 8 in the initial state. However, in order to facilitate understanding, both are shown in FIG. The distance from the axis of the revolution shaft 1 to the second engagement portion 92 of the second movable sprocket 9 is substantially equal to the distance from the axis of the revolution shaft 1 to the second engagement portion 82 of the first movable sprocket 8. (See FIG.
  • FIG. 9 is for explaining the positional relationship between the respective engaging portions, the engaging portion that should be hidden behind the first movable sprocket 8 is also illustrated.
  • the second engaging portion 92 of the second movable sprocket 9 is formed at a position of about 240 ° clockwise from the first engaging portion 91 in the drawing. That is, in the state where the first engaging portion 81 and the first engaging portion 91 are matched (the state shown in FIG. 7), the first engaging portions 81 and 91, the second engaging portion 82, and the second engaging portion.
  • the intervals with the part 92 are all 120 ° (see FIG. 9).
  • the rotational force transmission mechanism 10 is constituted by chains 101, 102, and 103 (see FIG. 4) spanned between the fixed / movable sprockets 7, 8, and 9 and the respective rotating sprockets 31 to 51.
  • the chain 101 of the rotational force transmission mechanism 10 can transmit rotational force in the same direction (counterclockwise in FIG. 4) between the fixed sprocket 7 and the first rotating sprocket 31 of the first rotating blade 3. It has become a structure.
  • the rotational force transmission mechanism 10 causes the first rotation sprocket 31 to rotate in the opposite direction to the revolution (for example, clockwise in FIG. 4) by the revolution of the first rotation sprocket 31 (for example, counterclockwise rotation in FIG. 4). Is configured to rotate.
  • the chain 102 of the rotational force transmission mechanism 10 transmits rotational force in the same direction between the first movable sprocket 8 and the second rotating sprocket 41 of the second rotary blade 4. It has a configuration. Thereby, the rotational force transmission mechanism 10 is configured to rotate the second rotation sprocket 41 in the direction opposite to the rotation by the revolution of the second rotation sprocket 41.
  • the chain 103 of the rotational force transmission mechanism 10 also transmits rotational force in the same direction between the second movable sprocket 9 and the third rotating sprocket 51 of the third rotary blade 5 as in the case of the chain 101 described above. It has a configuration. Thereby, the rotational force transmission mechanism 10 is configured to rotate the third rotation sprocket 51 in the direction opposite to the rotation by the revolution of the third rotation sprocket 51. In FIG. 1, only one of the chains 102 and 103 is shown.
  • the first to third rotor blades 3 to 5 are configured to rotate by 1 ⁇ 2 rotation during one revolution around the wind direction axis 6. Specifically, the number of teeth of each of the rotating sprockets 31, 41, 51 is twice the number of teeth of the corresponding fixed sprocket 7 and movable sprocket 8, 9.
  • the first hook member 11 is detachably engaged with the first engaging portion 81 of the first movable sprocket 8 and the first engaging portion 91 of the second movable sprocket 9 so that the first and second movable sprockets are engaged.
  • the relative rotation angle between 8 and 9 and the wind direction axis 6 can be fixed.
  • the second hook member 12 is configured to be able to detachably engage with the second engaging portions 82 and 92 to fix the first and second movable sprockets 8 and 9 and the wind direction shaft 6.
  • the second and third rotor blades 4 and 5 are substantially parallel to the first rotor blade 3. It has become. This operation will be described later.
  • the key drive mechanism 13 has a configuration in which the first key member 11 is engaged with the first engaging portions 81 and 91 in a normal state and the second key member 12 is engaged with the second engaging portions 82 and 92 in a strong wind. ing.
  • the key drive mechanism 13 includes an operation unit 131 and a support unit 132 housed inside the wind direction shaft 6 (see FIG. 7).
  • the operation part 131 is extended below the wind direction axis 6 and can be moved up and down by appropriate drive means (not shown) or manually.
  • the support part 132 is attached to the tip (upper end in FIG. 7) of the operation part 131.
  • the first key member 11 and the second key member 12 are attached to the side surface of the support portion 132.
  • the first key member 11 and the second key member 12 fixed thereto are also lowered. Then, first, the first key member 11 is sequentially removed from the two first engaging portions 81 and 91. In a state where the first key member 11 is completely removed from the two first engaging portions 81 and 91, the first movable sprocket 8 and the second movable sprocket 9 can rotate about the axis relative to the wind direction axis 6. Become. On the other hand, since both the second rotor blade 4 and the third rotor blade 5 receive strong wind force, they rotate by this wind force, and the first and second movable sprockets 8 and 9 are connected via the chains 102 and 103. It rotates with respect to the wind direction axis 6.
  • the second key member 12 descends as the support portion 132 of the key drive mechanism 13 descends. And the front-end
  • the position of the second key member 12 eventually coincides with the position of the second engaging portion 92 in the second movable sprocket 9. . Then, the tip of the second key member 12 is fitted into the second engaging portion 92 (FIG. 10C).
  • the second hook member 12 can be engaged with the two second engaging portions 82 and 92, respectively.
  • the movable sprockets 8 and 9 are both fixed with respect to the wind direction shaft 6.
  • the second key member 12 is engaged with the two second engaging portions 82 and 92, respectively, as schematically shown in FIG. Is also parallel to the first rotor blade 3. This is because when the movable sprockets 8 and 9 rotate with respect to the wind direction axis 6, even if the revolution angles of the second and third rotor blades 4 and 5 remain unchanged, the rotation angles change.
  • the wind direction plate 61 of the wind direction axis 6 and each rotor blade are parallel to each other. That is, in the state where the wind direction plate 61 and the first rotary blade 3 are parallel, the second rotary blade 4 and the third rotary blade 5 are parallel to the first rotary blade 3 by the above-described operation.
  • the wind direction plate 61 and each rotary blade become parallel, the revolution force which each rotary blade receives at the time of a strong wind can be reduced. Thereby, the overrotation of the rotary body 2 can be prevented.
  • each rotary blade revolves along the direction of the wind direction plate 61. Further, if the rotor blades are installed at equal intervals, there is an advantage that the sum of the forces in the revolving direction acting on the rotor blades is almost zero even if there is an instantaneous change in the wind direction.
  • the reverse operation is performed. That is, the operation part 131 of the key drive mechanism 13 is operated to raise the support part 132. Then, the first hook member 11 can be sequentially engaged with the two first engaging portions 81 and 91 by utilizing the rotational force of the wind force by the reverse operation to the above. In this state, the rotation angle of each rotor blade returns to the initial state shown in FIG. When there is no wind power, each rotor blade is left as it is, but in this state, power generation is not possible in the first place, so this is not a problem in itself. Even if the rotary blades are parallel to each other, the initial position can be restored by a weak wind due to the effect of the rising portions (see FIG. 5) provided on the blades. Further, since the wind direction constantly fluctuates, it is considered that a rotational force can be applied to each blade along with the fluctuation.
  • the rotary blades can be made parallel only by moving the key drive mechanism 13 up and down, even when the key drive mechanism 13 is driven by electric power, power consumption can be reduced. For this reason, in the electric power generating apparatus using this rotary blade mechanism, there exists an advantage that there is little fall of power generation efficiency.
  • the rotary blade mechanism of the second embodiment includes first to eighth rotary blades 211 to 218, and these rotary blades rotate in the same manner as in the first embodiment.
  • a rotating sprocket (not shown) is attached.
  • a fixed sprocket and a movable sprocket are attached to the wind direction shaft 6 as in the first embodiment, but in the second embodiment, eight sprockets are used corresponding to the number of rotor blades. ing. That is, a fixed sprocket 220 and first to seventh movable sprockets 231 to 237 are attached to the wind direction shaft 6 in the second embodiment.
  • the fixed sprocket 220 is formed with a first engaging portion 221 and a second engaging portion 222 as in the case of the fixed sprocket 7 (see FIGS. 13 to 14).
  • first to seventh movable sprockets 231 to 237 are also formed with first engaging portions 2311 to 2371 and second engaging portions 2312 to 2372 (see FIGS. 13 to 14).
  • first engaging portions 2311 to 2371 and second engaging portions 2312 to 2372 see FIGS. 13 to 14.
  • FIG. 14 in order to show the positional relationship between the engaging portions, the engaging portions that should have been hidden are also shown by solid lines.
  • one key drive mechanism 13 is used.
  • this key drive mechanism is divided into a first key drive mechanism 3131 and a second key drive mechanism 3132. Use.
  • the first key drive mechanism 3131 is attached with the first key member 11
  • the second key drive mechanism 3132 is attached with the second key member 12 ( (See FIG. 12).
  • each rotor blade in this state is shown in FIG.
  • the first key member 11 of the first key driving mechanism 3131 is engaged with the first engaging portion 221 of the fixed sprocket 220 and the first engaging portions 2311 to 2371 of the first to seventh movable sprockets 231 to 237. It is inserted. Thereby, about each rotary blade, if it is the same revolution angle, it can be operated so that it may become the same autorotation angle.
  • the first to fourth rotor blades can be operated in parallel with the wind direction, and the other four rotor blades can be operated to have the same rotation angle at the same revolution angle (FIG. 12). (See (b)).
  • the operation in which the second key member 12 is fitted into the second engaging portion is the same as in the first embodiment described above, and a detailed description thereof will be omitted (see FIG. 13B). It is also possible to operate 5 to 7 rotating blades, but since the operation in that case can be understood from the above, detailed description thereof will be omitted.
  • the first to sixth rotor blades can be operated in parallel with the wind direction, and the other two rotor blades can be operated to have the same rotation angle if they have the same revolution angle (FIG. 12). (See (c)). Since the operation
  • the second key member 12 of the second key drive mechanism 3132 includes the second engaging portions 2312 to 2372 of the first to seventh movable sprockets 231 to 237 and the second engaging portion of the fixed sprocket 220. 222.
  • the first to eighth rotor blades can be in a state parallel to the wind direction (see FIG. 12D). Since the operation of fitting the second key member 12 into the second engaging portion is the same as that in the first embodiment described above, detailed description thereof will be omitted (see FIGS. 13A and 13C). Further, although it is possible to operate one rotary blade, the operation in that case can be understood from the above description, and detailed description thereof will be omitted.
  • the same reference numerals are used for members that are basically the same as those in the first embodiment described above, thereby simplifying the description.
  • the first key member 11 and the second key member 12 are driven by one key drive mechanism 13.
  • the first key member 11 is driven by the first key driving mechanism 3131 and the second key member 12 is driven by the second key driving mechanism 3132.
  • the second key member 12 is sequentially fitted into the second engaging portions 82 and 92. As a result, the same operation as in the first embodiment is possible.
  • the rotary blade mechanism of the fourth embodiment includes a support frame 400 for supporting the wind direction shaft 6.
  • the support frame 400 includes a base body 401 and a support column 402.
  • a bearing for supporting the wind direction shaft 6 so as to be rotatable is attached to a connection portion between the base body 401 and the wind direction shaft 6.
  • the rotary blade mechanism of the fifth embodiment includes an upper exhaust mechanism 500 for improving the discharge efficiency of the airflow that has passed through the rotary blade.
  • the upper exhaust mechanism 500 includes six struts 510, an upper rail 520, a guide plate 530, and a rotating frame 540.
  • the column 510 has a circular cross section (see FIG. 20), and is disposed outside the rotating body 2.
  • auxiliary struts 511 that support the struts 510 are also illustrated, but in FIG. 20, the description of the auxiliary struts is omitted.
  • the upper rail 520 has an annular shape and is attached to the upper end of the column 510 (see FIG. 18).
  • the guide plate 530 has a truncated cone shape that is convex downward, and its upper end is connected to the upper rail 520.
  • the rotation frame 540 is attached to the wind direction plate 61 of the wind direction shaft 6 and is configured to rotate together with the wind direction plate 61.
  • the rotating frame 540 is generally configured by an upper surface plate 541 and side surface plates 542 and 543.
  • a ventilation path 544 for allowing airflow to pass therethrough is formed inside the rotary frame 540.
  • the top plate 541 has a substantially fan shape and is fixed to the wind direction plate 61.
  • the upper surface plate 541 defines the upper surface of the ventilation path 544.
  • the side plates 542 and 543 are connected to the side portion of the top plate 541 and define the side surface of the ventilation path 544.
  • rollers 542a and 543a are attached to the lower portions of the side plates 542 and 543.
  • the rollers 542 a and 543 a can run on the upper surface of the upper rail 520, so that the rotating frame 540 can move together with the wind direction plate 61.
  • the airflow can flow in the direction of the wind direction plate 61 (that is, the direction toward the downstream side of the airflow).
  • the flow of the airflow around the rotor blade can be made smooth, and as a result, the airflow can be efficiently received by the rotor blade.
  • the fixed sprocket 220 and the first to seventh movable sprockets 231 to 237 are arranged around the wind direction axis 6.
  • these sprockets are arranged outside the wind direction shaft 6 and each sprocket is attached to the wind direction shaft 6 via a gear mechanism.
  • the fixed sprocket 220 and the first to seventh movable sprockets 231 to 237 are attached to the rotating shaft 600 so as to be able to rotate relative thereto.
  • the position of each sprocket is defined by the first key member 11 and the second key member 12.
  • the rotation shaft 600 is connected to the wind direction shaft 6 by a rotation transmission mechanism 650 using a bevel gear.
  • the same operation as in the second embodiment can be realized.
  • the fifth embodiment by adjusting the reduction ratio between the bevel gears, it is possible to realize a configuration in which each rotary blade rotates by half during one revolution. That is, in this embodiment, the fixed sprocket 220 and the first to seventh movable sprockets 231 to 237 can have the same pitch circle radius as that of the respective rotating sprockets. There is also an advantage that the 7 movable sprockets 231 to 237 can be downsized.
  • the rotary frame 2 is rotatably supported by a pedestal 100 erected on the ground, and each wing revolves around a virtual revolution shaft 1 (see FIGS. 21 and 22).
  • the rotary blade mechanism of the sixth embodiment includes a side exhaust mechanism 700 around the rotary body 2.
  • the side exhaust mechanism 700 includes six air guide blades 710 and a drive mechanism 720 (FIG. 26).
  • Each of the air guide blades 710 includes a thin plate-like main body 711 and a rotating shaft 712.
  • the main body 711 is attached at a position eccentric with respect to the rotation shaft 712 as shown in an enlarged view in FIG.
  • the upper end of the rotating shaft 712 is rotatably supported by a support frame 400 similar to that described in the fourth embodiment.
  • the lower end of the rotating shaft 712 is also rotatably supported by an appropriate base.
  • the drive mechanism 720 includes a motor 721, a transmission mechanism 722, a clutch mechanism 723, and a bevel gear 724 (see FIG. 26).
  • the motor 721 is controlled to rotate at a predetermined angle by a control means (not shown).
  • the transmission mechanism 722 is a mechanism for transmitting the rotational force of the motor 721 to the rotating shaft 712 of the wind guide blade 710 via the clutch mechanism 723 and the bevel gear 724.
  • the specific structure of the transmission mechanism 722 is not particularly limited, for example, a combination of a worm gear and a worm wheel can be used.
  • the clutch mechanism 723 is attached in the middle of the transmission mechanism 722.
  • the intermittent operation of the clutch mechanism 723 can be performed by an appropriate control mechanism.
  • the bevel gear 724 is meshed with a bevel gear attached to the rotation shaft 712 so that the rotation shaft 712 can be rotated.
  • the rotary blade mechanism of the sixth embodiment by controlling the air guide blade 710 to an appropriate angle by the motor 721, the airflow passing through the side of the rotating body 2 can be efficiently flowed. Thereby, in this embodiment, the wind receiving efficiency in each rotary blade can be improved.
  • the wind guide blade 710 can be freely rotated by setting the clutch mechanism 723 to the disconnected state. Since the main body 711 of the wind guide blade 710 is attached in an eccentric state with respect to the rotating shaft 712, when the clutch mechanism 723 is in a disconnected state, the main body 711 of the wind guide blade 710 is moved along the wind direction by wind force. Can be arranged. Therefore, in the present embodiment, it is possible to reduce the possibility of the wind guide blades 710 being damaged during a strong wind.
  • the present invention is not limited to the above-described embodiment, and various modifications can be made without departing from the gist of the present invention.
  • a specific number of rotor blades is used, but any other appropriate number can be used.
  • the number of movable sprockets is set according to the number of rotor blades.
  • the angular relationship of the second engaging portions formed on each movable sprocket is set so that the above-described operation is possible according to the arrangement state of each rotor blade.
  • wind power is exemplified as the fluid.
  • other fluid flows such as hydraulic power.

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

L'invention concerne une méthode permettant d'aligner une pale rotative avec la direction du vent grâce à celui-ci en cas de grand vent. Les trois premières pales rotatives (3 à 5) sont attachées à un corps rotatif pouvant tourner (2) de façon à être centrées sur un arbre de rotation (1). Un arbre de direction du vent (6) peut tourner par rapport à l'arbre de rotation (1) en fonction de la direction de la force du vent sur une plaque de détection de la direction du vent (61). Une roue dentée fixe (7) est fixée sur l'arbre de direction du vent (6). Un mécanisme d'entraînement de clavette (13) permet à un premier élément clavette (11) de s'engager dans les premières parties d'engagement respectives (81, 91) d'une première et d'une deuxième roue dentée mobile (8, 9) en temps normal. Dans cet état, le corps rotatif (2) peut tourner grâce à la force du vent sur les pales rotatives (3 à 5). En cas de grand vent, le premier élément clavette (11) est retiré des premières parties d'engagement respectives (81, 91). Un deuxième élément clavette (12) est ensuite engagé dans les deuxièmes parties d'engagement respectives (82, 92) des première et deuxième roues dentées mobiles (8, 9). Dans cet état, chacune des pales rotatives (3 à 5) se place parallèlement à la direction du vent.
PCT/JP2011/069812 2010-09-24 2011-08-31 Mécanisme à pale rotative et dispositif de production d'énergie l'utilisant WO2012039249A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2010-214020 2010-09-24
JP2010214020A JP2013253476A (ja) 2010-09-24 2010-09-24 回転翼機構及びこれを用いた発電装置

Publications (1)

Publication Number Publication Date
WO2012039249A1 true WO2012039249A1 (fr) 2012-03-29

Family

ID=45873739

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2011/069812 WO2012039249A1 (fr) 2010-09-24 2011-08-31 Mécanisme à pale rotative et dispositif de production d'énergie l'utilisant

Country Status (2)

Country Link
JP (1) JP2013253476A (fr)
WO (1) WO2012039249A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150147176A1 (en) * 2012-07-05 2015-05-28 Adv Tech Rotary machine comprising a rotor placed in a fluid and equipped with orientable blades

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55104774U (fr) * 1979-01-18 1980-07-22
JPS55131585A (en) * 1979-02-26 1980-10-13 Hideo Sakai Windmill with rotating blades
JPS5618076A (en) * 1979-07-11 1981-02-20 Voith Gmbh J M Device for utilizing fluid energy
JP2001107838A (ja) * 1999-08-02 2001-04-17 Hirai Sekkei Jimusho:Kk 風車およびその制御方法
JP2002339854A (ja) * 2001-03-15 2002-11-27 Toshiyuki Uchibayashi 風力発電装置

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55104774U (fr) * 1979-01-18 1980-07-22
JPS55131585A (en) * 1979-02-26 1980-10-13 Hideo Sakai Windmill with rotating blades
JPS5618076A (en) * 1979-07-11 1981-02-20 Voith Gmbh J M Device for utilizing fluid energy
JP2001107838A (ja) * 1999-08-02 2001-04-17 Hirai Sekkei Jimusho:Kk 風車およびその制御方法
JP2002339854A (ja) * 2001-03-15 2002-11-27 Toshiyuki Uchibayashi 風力発電装置

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150147176A1 (en) * 2012-07-05 2015-05-28 Adv Tech Rotary machine comprising a rotor placed in a fluid and equipped with orientable blades
US9841003B2 (en) * 2012-07-05 2017-12-12 Adv Tech Rotary machine comprising a rotor placed in a fluid and equipped with orientable blades

Also Published As

Publication number Publication date
JP2013253476A (ja) 2013-12-19

Similar Documents

Publication Publication Date Title
DK2306002T3 (en) Systems and methods for assembling a pitch control device for use in a wind turbine
KR101297887B1 (ko) 풍력 발전 장치, 기어 전달 기구 및 기어 맞물림 제어 방법
DK2416006T3 (en) Krøjningsanordning for use in wind turbines
WO2008022209A3 (fr) Générateur d'électricité éolien
CN102612797B (zh) 回转式电动机致动器及水平轴风车
JP2005516159A5 (fr)
CA2552297A1 (fr) Generateur d'energie eolienne de type magnus
CN102374114B (zh) 用于风力涡轮的轮毂和安装风力涡轮的方法
US8680705B2 (en) Vertical axis wind turbine
MX2012000008A (es) Turbina eolica de par motor compensado.
JP2009500562A (ja) ブレードピッチ制御機構
JP2010121518A (ja) 縦軸式マグナス型風力発電装置
CN102844565A (zh) 风车用驱动装置
RU2426005C1 (ru) Карусельный ветродвигатель
WO2012039249A1 (fr) Mécanisme à pale rotative et dispositif de production d'énergie l'utilisant
KR101525553B1 (ko) 수직 로터형 풍력발전 장치
JP2009085090A (ja) 風車装置
WO2009081438A3 (fr) Dispositif de moteur hydraulique rotatif avec un axe vertical pour la production d'énergie
WO2009006287A3 (fr) Moulin oscillant
CN104204512A (zh) 发电装置
JP2012112309A (ja) 風車ブレードの制御方法
CN101871431A (zh) 笼式风叶风力发电机
US20130343889A1 (en) Friction Wheel Drive Train for a Wind Turbine
TW201428180A (zh) 風力發電系統、風力發電系統的組裝方法以及風力發電系統的檢查方法
KR20130024330A (ko) 풍력발전기의 블레이드의 가변구조

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 11826695

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 11826695

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: JP