JP2016156325A - Vertical shaft type windmill - Google Patents

Vertical shaft type windmill Download PDF

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JP2016156325A
JP2016156325A JP2015034911A JP2015034911A JP2016156325A JP 2016156325 A JP2016156325 A JP 2016156325A JP 2015034911 A JP2015034911 A JP 2015034911A JP 2015034911 A JP2015034911 A JP 2015034911A JP 2016156325 A JP2016156325 A JP 2016156325A
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wing
vertical axis
wing member
rotary shaft
rib
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JP6508971B2 (en
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強 笹原
Tsutomu Sasahara
強 笹原
和昌 久保田
Kazumasa Kubota
和昌 久保田
山田 裕介
Yusuke Yamada
裕介 山田
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Lixil Corp
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Lixil Corp
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction

Abstract

PROBLEM TO BE SOLVED: To provide a vertical shaft type windmill that is satisfactorily rotatable.SOLUTION: The vertical shaft type windmill comprises: a rotary shaft member which is coupled to a generator and erected in a freely rotatable manner in the state where a rotary shaft extends vertically; an arm 30 that extends from the rotary shaft member in a radiation direction of the rotary shaft; a coupling member 50 that is provided in a tip of the arm 30; and a blade member 70 that is coupled to the coupling member 50. The coupling member 50 includes: plate-like body parts 53A and 55A that are spread orthogonally to the radiation direction of the rotary shaft; and rib parts 53B and 55B that are bend from front edges and rear edges of the body parts 53A and 55A closer to the rotary shaft side. The blade member 70 includes a coupled part provided with a first fitting portion that is bonded to outer side faces of the body parts 53A and 55A of the coupling member 50, and a second fitting portion that is bonded to outer side faces of the rib parts 53B and 55B.SELECTED DRAWING: Figure 4

Description

本発明は垂直軸型風車に関するものである。   The present invention relates to a vertical axis wind turbine.

特許文献1は従来の垂直軸型風車を開示している。この垂直軸型風車は、回転軸部材、5本のアーム、及び各アームの先端に連結された翼部材を備えている。回転軸部材は発電機に連結されている。この回転軸部材は回転軸が垂直方向に伸びた状態に回転自在に立てられている。各アームは回転軸部材の周りを等間隔で回転軸の放射方向に伸びている。翼部材は薄板状の金属から形成された流線型の翼形である。この翼部材は内側面(回転軸側の側面)の前側を残して後ろ側を切り欠いている。この翼部材は、残された内側面の後端縁近傍と、外側面(回転軸と反対側の側面)とを連結したリブが形成されている。このため、この翼部材は、構成要素が少なく、軽量かつ強固に形成されている。また、この翼部材は、内側面、外側面、及びリブに囲まれた凹部にはめ込まれたブロック状のホルダを有している。アームは先端面から先端面に直交する方向に伸びる雌ねじ部が設けられている。このアームは、翼部材の外側面から翼部材及びホルダを貫通した螺子部材が雌ねじ部にねじ込まれ、先端面が翼部材の回転軸側の側面に当接して翼部材を連結している。このように、この垂直軸型風車はアームと翼部材とを正確に位置決めして連結することができる。   Patent Document 1 discloses a conventional vertical axis type windmill. This vertical axis type windmill includes a rotating shaft member, five arms, and a wing member connected to the tip of each arm. The rotating shaft member is connected to the generator. The rotary shaft member is erected so that the rotary shaft extends in the vertical direction. Each arm extends in the radial direction of the rotating shaft at equal intervals around the rotating shaft member. The wing member is a streamlined wing shape formed from a thin plate-like metal. This wing member is notched on the rear side, leaving the front side of the inner side surface (side surface on the rotating shaft side). The wing member is formed with a rib connecting the vicinity of the rear end edge of the remaining inner side surface and the outer side surface (side surface opposite to the rotation axis). For this reason, this wing member has few components and is light and strong. In addition, the wing member has a block-shaped holder fitted in a recess surrounded by an inner surface, an outer surface, and a rib. The arm is provided with an internal thread portion extending from the distal end surface in a direction orthogonal to the distal end surface. In this arm, a screw member penetrating the wing member and the holder from the outer surface of the wing member is screwed into the female screw portion, and the tip surface abuts on the side surface on the rotating shaft side of the wing member to connect the wing member. Thus, this vertical axis type wind turbine can accurately position and connect the arm and the wing member.

特許第4514502号公報Japanese Patent No. 4514502

しかし、特許文献1の垂直軸型風車は、翼部材及びホルダを貫通した1本の螺子部材でアームと翼部材とを連結している。このため、この垂直軸型風車は、回転した際に翼部材に対して生じる曲げ応力がアームと翼部材とを連結している螺子部材に集中する。よって、この垂直軸型風車は、回転数が高くなると、応力によって螺子部材の破損等を生じ、翼部材がアームから脱落するおそれがある。また、この垂直軸型風車は、回転した際に翼部材の受ける遠心力が螺子部材をアームの雌ねじ部から引き抜く方向に働く。この垂直軸型風車は、螺子部材とアームの雌ねじ部とはねじ結合されているだけであるため、風車の回転数が高くなると、遠心力によって螺子部材がアームのねじ部から引き抜かれ翼部材がアームから脱落するおそれがある。   However, the vertical axis type windmill disclosed in Patent Document 1 connects the arm and the blade member with a single screw member penetrating the blade member and the holder. For this reason, when this vertical axis type windmill rotates, the bending stress generated with respect to the blade member concentrates on the screw member connecting the arm and the blade member. Therefore, when the rotational speed of the vertical axis type wind turbine is increased, the screw member may be damaged due to stress, and the wing member may drop from the arm. Further, in this vertical axis type windmill, the centrifugal force received by the wing member when it rotates rotates in the direction of pulling out the screw member from the female screw portion of the arm. In this vertical shaft type windmill, since the screw member and the female threaded portion of the arm are only screwed together, when the rotational speed of the windmill increases, the screw member is pulled out from the threaded portion of the arm by centrifugal force, and the wing member is There is a risk of falling off the arm.

本発明は、上記従来の実情に鑑みてなされたものであって、良好に回転することができる垂直軸型風車を提供することを解決すべき課題としている。   The present invention has been made in view of the above-described conventional situation, and an object to be solved is to provide a vertical-axis type wind turbine that can rotate satisfactorily.

本発明の垂直軸型風車は、発電機に連結され、回転軸が垂直方向に伸びた状態に回転自在に立てられる回転軸部材と、
この回転軸部材から前記回転軸の放射方向に伸びるアームと、
このアームの先端部に設けられた連結部材と、
この連結部材に連結された翼部材と、
を備えた垂直軸型風車であって、
前記連結部材は、前記回転軸の放射方向に直交する方向に拡がるプレート状の本体部と、この本体部の前端縁及び後端縁から前記回転軸側へ屈曲したリブ部とを有しており、
前記翼部材は、前記連結部材の本体部の外側面に接合する第1取付部、及びリブ部の外側面に接合する第2取付部を具備した被連結部を有していることを特徴とする。
A vertical shaft type windmill of the present invention is connected to a generator, and a rotary shaft member that is rotatable and stands in a state where the rotary shaft extends in the vertical direction;
An arm extending in a radial direction of the rotary shaft from the rotary shaft member;
A connecting member provided at the tip of the arm;
A wing member connected to the connecting member;
A vertical axis wind turbine with
The connecting member has a plate-like main body that extends in a direction perpendicular to the radial direction of the rotary shaft, and a rib that is bent toward the rotary shaft from the front and rear edges of the main body. ,
The wing member has a connected portion including a first attachment portion that is joined to the outer surface of the main body portion of the connection member and a second attachment portion that is joined to the outer surface of the rib portion. To do.

この垂直軸型風車は、連結部材が回転軸の放射方向に直交する方向に拡がるプレート状の本体部の前端縁及び後端縁から回転軸側へ屈曲したリブ部を有し、リブ部の外側面が翼部材の第2取付部に接合されている。このため、この垂直軸型風車は、連結部材のリブ部が強度部材として働き、回転した際に翼部材及び連結部材に対して生じる曲げ応力を分散させることができる。よって、この垂直軸型風車は、回転数が高くなっても翼部材と連結部材との連結を良好に維持することができる。なお、回転軸の放射方向に直交する方向とは、回転軸の放射方向に厳密に直交する場合のみでなく、直交に対して多少角度がずれていてもよい。   This vertical shaft type windmill has rib portions bent from the front end edge and the rear end edge of the plate-like main body portion to the rotation shaft side in which the connecting member extends in a direction perpendicular to the radial direction of the rotation shaft. The side surface is joined to the second attachment portion of the wing member. For this reason, in this vertical axis type windmill, the rib portion of the connecting member functions as a strength member, and the bending stress generated on the blade member and the connecting member when rotating can be dispersed. Therefore, this vertical axis type windmill can maintain the connection between the blade member and the connecting member well even when the rotational speed increases. The direction orthogonal to the radial direction of the rotation axis is not limited to the case of being strictly orthogonal to the radial direction of the rotation axis, and the angle may be slightly deviated from the orthogonal direction.

したがって、本発明の垂直軸型風車は良好に回転することができる。   Therefore, the vertical axis type windmill of the present invention can rotate well.

実施例1の垂直軸型風車を示す斜視図である。It is a perspective view which shows the vertical axis type windmill of Example 1. FIG. 実施例1の垂直軸型風車を示す断面図である。It is sectional drawing which shows the vertical axis type windmill of Example 1. FIG. 実施例1の翼部材、連結部材、及びカバーを示す斜視図である。It is a perspective view which shows the wing | blade member of Example 1, a connection member, and a cover. 実施例1の翼部材、及び連結部材を示す断面図である。It is sectional drawing which shows the wing | blade member of Example 1, and a connection member. 実施例1の翼部材、連結部材、及びカバーを示す分解断面図である。FIG. 3 is an exploded cross-sectional view showing a wing member, a connecting member, and a cover of Example 1. 実施例1の連結部材を示す斜視図である。FIG. 3 is a perspective view showing a connecting member of Example 1. 他の実施例の連結部材を示す斜視図である。It is a perspective view which shows the connection member of another Example.

本発明における好ましい実施の形態を説明する。   A preferred embodiment of the present invention will be described.

本発明の垂直軸型風車において、前記連結部材のリブ部及び前記翼部材の第2取付部は、前記リブ部及び前記第2取付部を貫通する接合部材によって接合され得る。この場合、リブ部及び第2取付部を貫通する接合部材が、回転した際に翼部材に生じる遠心力に交差する方向(望ましくは直交する方向)に伸ばすことができる。このため、この垂直軸型風車は、リブ部と第2取付部の接合面に沿ってリブ部と第2取付部とがずれ難く、接合強度を高めることができる。   In the vertical axis wind turbine of the present invention, the rib portion of the connecting member and the second attachment portion of the wing member may be joined by a joining member that penetrates the rib portion and the second attachment portion. In this case, the joining member that penetrates the rib portion and the second attachment portion can be extended in a direction (desirably orthogonal) that intersects the centrifugal force generated in the wing member when rotated. For this reason, in this vertical axis type windmill, the rib portion and the second attachment portion are not easily displaced along the joint surface between the rib portion and the second attachment portion, and the joining strength can be increased.

本発明の垂直軸型風車の翼部材は回転軸側の側面を凹ませた凹部が前記被連結部を形成し得る。この場合、この翼部材は側面より外側に露出しないように凹部内で連結部材と翼部材とを連結することができる。このため、この垂直軸型風車は、翼部材の周りを流れる空気の流れが乱れにくく揚力の減少を抑えることができるため、良好に回転することができる。   In the blade member of the vertical axis type wind turbine according to the present invention, a recessed portion in which a side surface on the rotating shaft side is recessed may form the connected portion. In this case, the connecting member and the wing member can be connected in the recess so that the wing member is not exposed to the outside from the side surface. For this reason, this vertical axis type windmill can rotate satisfactorily because the flow of air flowing around the wing member is less likely to be disturbed and the decrease in lift can be suppressed.

本発明の垂直軸型風車の翼部材は、前記被連結部を形成する前記凹部の開口部を塞ぎ、前記被連結部の周囲の回転軸側の側面に段差無く連続するカバーを有し得る。この場合、この垂直軸型風車は、カバーによって、翼部材の周りを流れる空気の流れがスムーズになり揚力を良好に発揮することができるため、良好に回転することができる。   The wing member of the vertical axis type windmill of the present invention may have a cover that closes the opening of the concave portion forming the coupled portion and continues without a step on the side surface on the rotating shaft side around the coupled portion. In this case, the vertical axis wind turbine can rotate well because the cover allows the air flowing around the wing member to flow smoothly and exert a good lift.

本発明の垂直軸型風車の翼部材は、前記被連結部を有する中間翼部材と、この中間翼部材の前端部に連結される前側翼部材と、前記中間翼部材の後端部に連結される後側翼部材とを有し得る。この場合、この垂直軸型風車は、中間翼部材、前側翼部材、及び後側翼部材を組み付ける前に連結部材と中間翼部材とを連結することができる。このため、この垂直軸型風車は容易に組み立てることができる。   The blade member of the vertical axis wind turbine of the present invention is connected to the intermediate blade member having the connected portion, the front blade member connected to the front end portion of the intermediate blade member, and the rear end portion of the intermediate blade member. A rear wing member. In this case, the vertical axis wind turbine can connect the connecting member and the intermediate blade member before assembling the intermediate blade member, the front blade member, and the rear blade member. For this reason, this vertical axis type windmill can be easily assembled.

次に、本発明の垂直軸型風車を具体化した実施例1について、図面を参照しつつ説明する。   Next, a first embodiment in which the vertical axis wind turbine of the present invention is embodied will be described with reference to the drawings.

<実施例1>
実施例1の垂直軸型風車は、図1及び図2に示すように、回転軸部材10、アーム30、連結部材50、及び翼部材70を備えている。回転軸部材10は、円筒状であり、回転軸が垂直方向に伸びて立てられている。回転軸部材10は下方に配置された図示しない発電機の回転軸部に図示しない接続部品を介して連結されている。回転軸部材10は発電機の回転軸部とともに回転自在である。この回転軸部材10は外周面に等間隔で4個の円環状のフランジ15が固定されている。各フランジは4個の貫通孔を等間隔に離れた3か所に設けている。各4個の貫通孔は所定の四角形の頂点に設けられている。
<Example 1>
As shown in FIGS. 1 and 2, the vertical axis wind turbine according to the first embodiment includes a rotating shaft member 10, an arm 30, a connecting member 50, and a wing member 70. The rotating shaft member 10 has a cylindrical shape, and the rotating shaft extends in the vertical direction. The rotary shaft member 10 is coupled to a rotary shaft portion of a generator (not shown) disposed below via a connection component (not shown). The rotating shaft member 10 is rotatable together with the rotating shaft portion of the generator. The rotary shaft member 10 has four annular flanges 15 fixed to the outer peripheral surface at equal intervals. Each flange has four through-holes at three positions spaced at equal intervals. Each of the four through holes is provided at a vertex of a predetermined square.

アーム30はフランジ15に連結された状態で回転軸に平行な方向(上下方向)が薄い長方形状の平板材で形成されている。アーム30は各フランジ15から3本ずつ等角度(120度)間隔で回転軸の放射方向にまっすぐ伸びている。アーム30は基端部及び先端部の夫々に上下方向に貫通する4個の貫通孔を有している。これら4個の貫通孔はアーム30の長辺又は短辺に平行な辺からなる所定の四角形の頂点に設けられている。アーム30とフランジ15とは、アーム30の基端部の4個の貫通孔をフランジ15の4個の貫通孔に重ね合わせてボルトを挿通し、挿通したボルトにナットを締め付けることによって、連結されている。   The arm 30 is formed of a rectangular flat plate member that is connected to the flange 15 and has a thin direction (vertical direction) parallel to the rotation axis. Three arms 30 extend straight from the flange 15 in the radial direction of the rotation axis at equal angular intervals (120 degrees). The arm 30 has four through holes penetrating in the vertical direction in each of the proximal end portion and the distal end portion. These four through-holes are provided at the apexes of a predetermined quadrangle made of a side parallel to the long side or the short side of the arm 30. The arm 30 and the flange 15 are connected by overlapping the four through holes at the base end portion of the arm 30 with the four through holes of the flange 15 and inserting bolts, and tightening the nuts to the inserted bolts. ing.

連結部材50は、図3〜図6に示すように、連結部51、前接合部53、及び後接合部55を有している。連結部51は、アルミ合金製であり、アーム30に連結された状態で、回転軸に平行な方向(上下方向)が薄い平板材で形成されている。連結部51は中央部51Aの回転軸部材10側に4個の貫通孔51Xを上下方向に貫設している。連結部51とアーム30とは、連結部51の4個の貫通孔51Xをアーム30の先端部の4個の貫通孔に重ね合わせてボルトを挿通し、挿通したボルトにナットを締め付けることによって、連結されている。また、連結部51は、翼部材70を連結した状態で、アーム30が連結された中央部51Aから前方向(翼部材70の前端方向)に斜めに伸びる前傾斜部51B、及び後方向(翼部材70の後端方向)に斜めに伸びる後傾斜部51Cを有している。つまり、この連結部51は前傾斜部51Bと後傾斜部51Cとの間に空間が形成されている。前傾斜部51Bの先端部及び後傾斜部51Cの先端部は、回転軸から放射方向に伸びているアーム30に直交する第1辺部52Aと、第1辺部52Aの外側端部から第1辺部52Aに直交し回転軸側へ伸びる第2辺部52Bとを形成している。   The connection member 50 has the connection part 51, the front junction part 53, and the back junction part 55, as shown in FIGS. The connecting portion 51 is made of an aluminum alloy, and is formed of a flat plate material that is connected to the arm 30 and has a thin direction (vertical direction) parallel to the rotation axis. The connecting portion 51 has four through holes 51X extending in the vertical direction on the rotating shaft member 10 side of the central portion 51A. By connecting the four through holes 51X of the connecting part 51 to the four through holes at the tip of the arm 30 and inserting the bolts, and tightening the nuts to the inserted bolts, the connecting part 51 and the arm 30 are It is connected. In addition, the connecting portion 51 includes a front inclined portion 51B extending obliquely in the forward direction (front end direction of the wing member 70) from the central portion 51A to which the arm 30 is connected, and a rear direction (wing A rear inclined portion 51C extending obliquely in the rear end direction of the member 70 is provided. That is, the connecting portion 51 has a space between the front inclined portion 51B and the rear inclined portion 51C. The front end portion of the front inclined portion 51B and the front end portion of the rear inclined portion 51C are first from the first side portion 52A orthogonal to the arm 30 extending in the radial direction from the rotation axis and from the outer end portion of the first side portion 52A. A second side portion 52B that is orthogonal to the side portion 52A and extends toward the rotation axis is formed.

前接合部53及び後接合部55は、アルミ合金製であり、L型アングル材で形成されている。前接合部53と連結部51とは、前接合部53の長手方向の中央部の内面と、連結部51の前傾斜部51Bの第1辺部52Aの端面及び第2辺部52Bの端面とを当接させた状態で溶接し、一体化されている。また、後接合部55と連結部51とは、後接合部55の長手方向の中央部の内面と、連結部51の後傾斜部51Cの第1辺部52Aの端面及び第2辺部52Bの端面とを当接させた状態で溶接し、一体化されている。前接合部53及び後接合部55は直交する2面の夫々に6個ずつの貫通孔53X、55Xが設けられている。前接合部53及び後接合部55において、直交する各2面に設けられた貫通孔53X、55Xは、前接合部53及び後接合部55に溶接された連結部51を境にして上下両側に3個ずつ等間隔に配置されている。これら貫通孔53X、55Xは、後述するように、接合部材であるリベット90の軸部が挿通して連結部材50と翼部材70とを接合するために利用される。   The front joint portion 53 and the rear joint portion 55 are made of an aluminum alloy and are formed of an L-shaped angle material. The front joint part 53 and the connection part 51 are the inner surface of the center part of the longitudinal direction of the front joint part 53, the end surface of the 1st side part 52A of the front inclination part 51B of the connection part 51, and the end surface of the 2nd side part 52B. Are welded and integrated with each other. Further, the rear joint portion 55 and the connecting portion 51 are formed by the inner surface of the central portion in the longitudinal direction of the rear joint portion 55, the end surface of the first side portion 52A of the rear inclined portion 51C of the connecting portion 51, and the second side portion 52B. It is welded and integrated with the end face in contact. The front joint portion 53 and the rear joint portion 55 are each provided with six through holes 53X and 55X on two orthogonal surfaces. In the front joint portion 53 and the rear joint portion 55, the through holes 53 </ b> X and 55 </ b> X provided on the two orthogonal surfaces are on both the upper and lower sides with the connecting portion 51 welded to the front joint portion 53 and the rear joint portion 55 as a boundary. Three of them are arranged at equal intervals. These through holes 53X and 55X are used for joining the connecting member 50 and the blade member 70 through the shaft portion of the rivet 90 as a joining member, as will be described later.

前接合部53及び後接合部55は直交する2面を形成する一方の平板部が回転軸の放射方向に直交する方向に拡がる本体部53A,55Aに相当する。つまり、この連結部材50の本体部53A,55Aは、前後2つに分かれており、プレート状である。また、前接合部53は直交する2面を形成する他方の平板部が本体部53Aから回転軸側へ屈曲したリブ部53Bに相当する。また、後接合部55は直交する2面を形成する他方の平板部が本体部55Aから回転軸側へ屈曲したリブ部55Bに相当する。つまり、この連結部材50のリブ部53B,55Bは2つに分かれた本体部53A,55Aの前端縁及び後端縁から回転軸側へ屈曲している。   The front joint portion 53 and the rear joint portion 55 correspond to main body portions 53A and 55A in which one flat plate portion forming two orthogonal surfaces extends in a direction perpendicular to the radial direction of the rotation axis. That is, the main body portions 53A and 55A of the connecting member 50 are divided into two parts, front and rear, and have a plate shape. Further, the front joint portion 53 corresponds to a rib portion 53B in which the other flat plate portion forming two orthogonal surfaces is bent from the main body portion 53A to the rotating shaft side. Further, the rear joint portion 55 corresponds to a rib portion 55B in which the other flat plate portion forming two orthogonal surfaces is bent from the main body portion 55A to the rotating shaft side. That is, the rib portions 53B and 55B of the connecting member 50 are bent from the front end edge and the rear end edge of the two main body portions 53A and 55A toward the rotation axis.

この連結部材50は、中央部51A、前傾斜部51B、及び後傾斜部51Cを有する連結部51と、間に空間を有する前傾斜部51Bと後傾斜部51Cとによって形成されている。また、この連結部材50は、連結部51の前傾斜部51B、後傾斜部51Cの夫々にL型アングル材で形成された前接合部53、後接合部55を連結し、本体部53A,55Aとリブ部53B,55Bとを形成している。このような構成にすることによって、この連結部材50は強度を確保しつつ軽量化を図ることができる。   The connecting member 50 is formed by a connecting portion 51 having a central portion 51A, a front inclined portion 51B, and a rear inclined portion 51C, and a front inclined portion 51B and a rear inclined portion 51C having a space therebetween. In addition, the connecting member 50 connects the front joint portion 53 and the rear joint portion 55 formed of L-shaped angle material to the front inclined portion 51B and the rear inclined portion 51C of the connecting portion 51, and the main body portions 53A and 55A. And rib portions 53B and 55B are formed. By adopting such a configuration, the connecting member 50 can be reduced in weight while ensuring strength.

翼部材70は、図3〜図5に示すように、流線型の翼形である。翼部材70は、回転軸に平行に伸びており、4個のアーム30の先端部に設けられた連結部材50に連結されている。翼部材70は、前側翼部材71、中間翼部材73、後側翼部材75、カバー77、及び蓋部材79を有している。前側翼部材71、中間翼部材73、後側翼部材75、及びカバー77は、アルミ合金を押出成形したものである。   As shown in FIGS. 3 to 5, the wing member 70 is a streamlined wing shape. The wing member 70 extends parallel to the rotation axis, and is connected to a connecting member 50 provided at the tip of the four arms 30. The wing member 70 includes a front wing member 71, an intermediate wing member 73, a rear wing member 75, a cover 77, and a lid member 79. The front wing member 71, the intermediate wing member 73, the rear wing member 75, and the cover 77 are formed by extrusion molding of an aluminum alloy.

前側翼部材71は、図5に示すように、前側翼部71A、及び前側閉鎖壁部71Bを有している。前側翼部71Aは、湾曲しており、翼部材70の前縁から伸びる内側面部(回転軸側の側面部)の前端部、及び翼部材70の前縁から伸びる外側面部(回転軸と反対側の側面部)の前端部を構成している。前側翼部71Aは、翼部材70の外側面部を構成する部分の後部において、後述する中間翼部材73の中間外側面部73Aの前端部が重なる位置を凹ませており、段差が設けられている。前側閉鎖壁部71Bは、途中に段差が設けられた略平板状であり、前側翼部71Aの両端を連結している。このように、前側翼部材71は、翼幅方向に貫通した内部空間を有し、翼幅方向に直交する断面形状が略半楕円形である。   As shown in FIG. 5, the front wing member 71 has a front wing portion 71A and a front closing wall portion 71B. The front wing portion 71A is curved and has a front end portion of an inner side surface portion (side surface portion on the rotating shaft side) extending from the front edge of the wing member 70 and an outer side surface portion (side opposite to the rotating shaft) extending from the front edge of the wing member 70. The front end portion of the side surface portion) is configured. The front wing portion 71A is recessed at the rear portion of the portion constituting the outer surface portion of the wing member 70 at a position where the front end portion of the intermediate outer surface portion 73A of the intermediate wing member 73 described later overlaps. The front closing wall portion 71B has a substantially flat plate shape with a step provided in the middle, and connects both ends of the front wing portion 71A. Thus, the front wing member 71 has an internal space penetrating in the wing width direction, and the cross-sectional shape orthogonal to the wing width direction is substantially semi-elliptical.

中間翼部材73は、中間外側面部73A、前壁部73B、後壁部73C、連結壁部73D、及び2枚の隔壁部73Eを有している。中間外側面部73Aは、翼弦方向で外方向にわずかに膨らんでおり、翼部材70の外側面部の中間部を構成している。前壁部73Bは、略平板状であり、中間外側面部73Aの前端近傍の内面から中間外側面部73Aに略直交する方向に伸びている。後壁部73Cは、略平板状であり、中間外側面部73Aの後端近傍の内面から前壁部73Bと同じ方向であり、前壁部73Bに平行に伸びている。連結壁部73Dは、平板状であり、前壁部73Bの中間部と後壁部73Cの中間部とを連結している。各隔壁部73Eは、平板状であり、中間外側面部73Aと連結壁部73Dとの間に連結されており、中間外側面部73A、前壁部73B、後壁部73C、及び連結壁部73Dで形成された翼幅方向に貫通した内部空間を3個の空間に分割している。前壁部73B、2枚の隔壁部73E、及び後壁部73Cは略等間隔に平行に配置されている。前壁部73Bと後壁部73Cに挟まれ、連結壁部73Dよりも回転軸側の空間が凹部70Aを形成している。この凹部70Aは、連結部材50の連結部51の先端部(前傾斜部51Bの先端部及び後傾斜部51Cの先端部)、前接合部53、及び後接合部55を収納することができる。   The intermediate wing member 73 has an intermediate outer surface portion 73A, a front wall portion 73B, a rear wall portion 73C, a connecting wall portion 73D, and two partition walls 73E. The intermediate outer surface portion 73 </ b> A slightly bulges outward in the chord direction and constitutes an intermediate portion of the outer surface portion of the wing member 70. The front wall portion 73B has a substantially flat plate shape, and extends in a direction substantially orthogonal to the intermediate outer surface portion 73A from the inner surface in the vicinity of the front end of the intermediate outer surface portion 73A. The rear wall 73C has a substantially flat plate shape, extends in the same direction as the front wall 73B from the inner surface near the rear end of the intermediate outer surface 73A, and extends in parallel to the front wall 73B. The connecting wall portion 73D has a flat plate shape and connects the intermediate portion of the front wall portion 73B and the intermediate portion of the rear wall portion 73C. Each partition wall 73E has a flat plate shape and is connected between the intermediate outer surface 73A and the connecting wall 73D. The intermediate outer surface 73A, the front wall 73B, the rear wall 73C, and the connecting wall 73D. The formed internal space penetrating in the blade width direction is divided into three spaces. The front wall 73B, the two partition walls 73E, and the rear wall 73C are arranged in parallel at substantially equal intervals. A space between the front wall portion 73B and the rear wall portion 73C and closer to the rotating shaft than the connecting wall portion 73D forms a recess 70A. 70 A of this recessed part can accommodate the front-end | tip part (The front-end | tip part of 51 C of front inclination parts, and the front-end | tip part of 51 C of back inclination parts) of the connection member 50, the front junction part 53, and the rear junction part 55.

前接合部53及び後接合部55が凹部70Aに収納された際、前接合部53の本体部53Aの外側面が連結壁部73Dの前端部に当接し、後接合部55の本体部55Aの外側面が連結壁部73Dの後端部に当接する。つまり、中間翼部材73の連結壁部73Dの前端部及び後端部が翼部材70の第1取付部70Bに相当する。連結壁部73Dは、第1取付部70Bに相当する前端部及び後端部に複数の貫通孔70Xが設けられている。これら貫通孔70Xは、前接合部53の本体部53A及び後接合部55の本体部55Aに設けられた貫通孔53X、55Xに対応する位置に設けられている。   When the front joint portion 53 and the rear joint portion 55 are stored in the recess 70A, the outer surface of the main body portion 53A of the front joint portion 53 abuts on the front end portion of the connecting wall portion 73D, and the main body portion 55A of the rear joint portion 55 The outer side surface comes into contact with the rear end portion of the connecting wall portion 73D. That is, the front end portion and the rear end portion of the connecting wall portion 73 </ b> D of the intermediate blade member 73 correspond to the first attachment portion 70 </ b> B of the blade member 70. The connecting wall portion 73D is provided with a plurality of through holes 70X at a front end portion and a rear end portion corresponding to the first mounting portion 70B. The through holes 70X are provided at positions corresponding to the through holes 53X and 55X provided in the main body portion 53A of the front joint portion 53 and the main body portion 55A of the rear joint portion 55.

また、前接合部53及び後接合部55が凹部70Aに収納された際、前接合部53のリブ部53Bの外側面が中間翼部材73の前壁部73Bに当接し、後接合部55のリブ部55Bの外側面が中間翼部材73の後壁部73Cに当接する。つまり、中間翼部材73の連結壁部73Dよりも回転軸側の前壁部73Bと後壁部73Cが翼部材70の第2取付部70Cに相当する。前壁部73B及び後壁部73Cは、第2取付部70Cに相当する連結壁部73Dよりも回転軸側に複数の貫通孔70Yが設けられている。これら貫通孔70Yは、前接合部53のリブ部53B及び後接合部55のリブ部55Bに設けられた貫通孔53X,55Xに対応する位置に設けられている。このように、凹部70Aが非連結部を形成している。   Further, when the front joint portion 53 and the rear joint portion 55 are housed in the recess 70 </ b> A, the outer surface of the rib portion 53 </ b> B of the front joint portion 53 comes into contact with the front wall portion 73 </ b> B of the intermediate wing member 73. The outer surface of the rib portion 55B contacts the rear wall portion 73C of the intermediate blade member 73. That is, the front wall portion 73 </ b> B and the rear wall portion 73 </ b> C closer to the rotation shaft than the connecting wall portion 73 </ b> D of the intermediate blade member 73 correspond to the second attachment portion 70 </ b> C of the blade member 70. The front wall portion 73B and the rear wall portion 73C are provided with a plurality of through-holes 70Y closer to the rotating shaft than the connecting wall portion 73D corresponding to the second mounting portion 70C. These through holes 70Y are provided at positions corresponding to the through holes 53X and 55X provided in the rib part 53B of the front joint part 53 and the rib part 55B of the rear joint part 55. In this way, the recess 70A forms a non-connecting portion.

後側翼部材75は、後外側面部75A、後内側面部75B、及び後側閉鎖壁部75Cを有している。後外側面部75Aは、略平板状であり、翼部材70の外側面の後部を構成している。後外側面部75Aは、前部において、中間翼部材73の中間外側面部73Aの後端部が重なる位置を凹ませており、段差が設けられている。後外側面部75Aの後端が翼部材70の後縁である。後内側面部75Bは、略平板状であり、翼部材70の内側面の後部を構成している。後内側面部75Bは後端部が後外側面部75Aの後端より僅か前側に連結している。後側閉鎖壁部75Cは、途中に段差が設けられた平板状であり、後外側面部75Aの前端部と後内側面部75Bの前端部とを連結している。後側翼部材75は翼幅方向に貫通した内部空間を有している。   The rear wing member 75 has a rear outer surface 75A, a rear inner surface 75B, and a rear closing wall 75C. The rear outer surface portion 75 </ b> A has a substantially flat plate shape and constitutes the rear portion of the outer surface of the wing member 70. The rear outer surface portion 75A is recessed at the front portion at a position where the rear end portion of the intermediate outer surface portion 73A of the intermediate wing member 73 overlaps, and a step is provided. The rear end of the rear outer surface portion 75 </ b> A is the rear edge of the wing member 70. The rear inner side surface portion 75 </ b> B has a substantially flat plate shape and constitutes a rear portion of the inner side surface of the wing member 70. The rear inner side surface portion 75B has a rear end portion connected to the front side slightly from the rear end of the rear outer side surface portion 75A. The rear closing wall portion 75C has a flat plate shape with a step in the middle, and connects the front end portion of the rear outer side surface portion 75A and the front end portion of the rear inner side surface portion 75B. The rear wing member 75 has an internal space penetrating in the wing width direction.

カバー77は、図1に示すように、翼部材70の内側面に開口する凹部70Aの開口部を塞ぐように翼部材70に取り付けられている。カバー77は一つの翼部材70に対して5個に分割されている。カバー77は、図3及び図5に示すように、中間内側面部77A、前挿入片部77B、及び後挿入片部77Cを有している。中間内側面部77Aは、翼弦方向でわずかに外側に膨らんでおり、翼部材70の内側面の中間部を構成している。翼部材70の中間翼部材73に連結された4個の連結部材50の間に取り付けられるカバー77は、上下寸法(回転軸に平行な方向の寸法)が各連結部材50の連結部51の間隔と同じである。翼部材70の上下両端と、翼部材70の上下両端から最も近い位置に連結された連結部材50との間に取り付けられるカバー77は、上下寸法(回転軸に平行な方向の寸法)が翼部材70の上下両端から各連結部材50の連結部51までの間隔と同じである。前挿入片部77Bは、平板状であり、中間内側面部77Aの前端より僅かに後側から中間内側面部77Aに略直交する方向に伸びている。後挿入片部77Cは、平板状であり、中間内側面部77Aの後端よりも僅かに前側から前挿入片部77Bと同じ方向であり、前挿入片部77Bと平行に伸びている。カバー77は、翼部材70の中間翼部材73に形成された凹部70Aに前挿入片部77B、及び後挿入片部77Cを挿入して翼部材70に取り付けられて固定される。カバー77は、凹部70Aの開口部を塞ぐように取り付けられ、凹部70Aの周囲の翼部材70の内側面と段差なく連続する。   As shown in FIG. 1, the cover 77 is attached to the wing member 70 so as to close the opening of the recess 70 </ b> A that opens to the inner surface of the wing member 70. The cover 77 is divided into five parts for one wing member 70. As shown in FIGS. 3 and 5, the cover 77 has an intermediate inner side surface portion 77 </ b> A, a front insertion piece portion 77 </ b> B, and a rear insertion piece portion 77 </ b> C. The intermediate inner side surface portion 77A swells slightly outward in the chord direction, and constitutes an intermediate portion of the inner side surface of the wing member 70. The cover 77 attached between the four connecting members 50 connected to the intermediate blade member 73 of the wing member 70 has a vertical dimension (a dimension in a direction parallel to the rotation axis) between the connecting portions 51 of each connecting member 50. Is the same. The cover 77 attached between the upper and lower ends of the wing member 70 and the connecting member 50 connected to the position closest to the upper and lower ends of the wing member 70 has a vertical dimension (a dimension in a direction parallel to the rotation axis). The distance from the upper and lower ends of 70 to the connecting portion 51 of each connecting member 50 is the same. The front insertion piece 77B has a flat plate shape and extends slightly from the front end of the intermediate inner surface 77A in the direction substantially orthogonal to the intermediate inner surface 77A. The rear insertion piece 77C has a flat plate shape, slightly in front of the rear end of the intermediate inner side surface 77A, in the same direction as the front insertion piece 77B, and extends in parallel with the front insertion piece 77B. The cover 77 is attached and fixed to the wing member 70 by inserting the front insertion piece 77B and the rear insertion piece 77C into the recess 70A formed in the intermediate wing member 73 of the wing member 70. The cover 77 is attached so as to close the opening of the recess 70A, and is continuous with the inner surface of the wing member 70 around the recess 70A without a step.

蓋部材79は、図1に示すように、翼部材70の翼弦方向の断面と同じ形状の外形を有している。蓋部材79は、翼部材70の上下端部を封鎖するように、翼部材70の上下端面に取り付けられて固定される。   As shown in FIG. 1, the lid member 79 has an outer shape having the same shape as the cross section in the chord direction of the wing member 70. The lid member 79 is attached and fixed to the upper and lower end surfaces of the wing member 70 so as to seal the upper and lower ends of the wing member 70.

翼部材70の前側翼部材71、中間翼部材73、及び後側翼部材75は、次に説明するように、中間翼部材73に連結部材50を連結しつつ組み立てられる。
まず、図4及び図5に示すように、中間翼部材73に形成された凹部70Aに連結部材50の連結部51の先端部、前接合部53、及び後接合部55を挿入する。この際、前接合部53の本体部53Aの外側面を第1取付部70Bである連結壁部73Dの前端部に当接させ、後接合部55の本体部55Aの外側面を第1取付部70Bである連結壁部73Dの後端部に当接させる。また、この際、前接合部53のリブ部53Bの外側面が第2取付部70Cである中間翼部材73の前壁部73Bに当接し、後接合部55のリブ部55Bの外側面が第2取付部70Cである中間翼部材73の後壁部73Cに当接する。
The front wing member 71, the intermediate wing member 73, and the rear wing member 75 of the wing member 70 are assembled while the connecting member 50 is connected to the intermediate wing member 73 as described below.
First, as shown in FIGS. 4 and 5, the front end portion of the connecting portion 51 of the connecting member 50, the front joint portion 53, and the rear joint portion 55 are inserted into the recess 70 </ b> A formed in the intermediate blade member 73. At this time, the outer surface of the main body portion 53A of the front joint portion 53 is brought into contact with the front end portion of the connecting wall portion 73D as the first attachment portion 70B, and the outer surface of the main body portion 55A of the rear joint portion 55 is made to be the first attachment portion. It is made to contact | abut to the rear-end part of connection wall part 73D which is 70B. At this time, the outer surface of the rib portion 53B of the front joint portion 53 abuts on the front wall portion 73B of the intermediate blade member 73 as the second attachment portion 70C, and the outer surface of the rib portion 55B of the rear joint portion 55 is the first. 2 abuts against the rear wall portion 73C of the intermediate blade member 73 which is the attachment portion 70C.

前接合部53の本体部53Aと第1取付部70Bである連結壁部73Dの前端部とは、前接合部53の本体部53Aに設けられた貫通孔53Xに内側から接合部材であるリベット90の軸部を挿入し、リベット90の挿入端部をかしめて接合される。また、後接合部55の本体部55Aと第1取付部70Bである連結壁部73Dの後端部とは、後接合部55の本体部55Aに設けられた貫通孔55Xに内側から接合部材であるリベット90を挿入し、リベット90の挿入端部をかしめて接合される。また、前接合部53のリブ部53Bと第2取付部70Cである中間翼部材73の前壁部73Bとは、第2取付部70Cに設けられた貫通孔70Yに前側から接合部材であるリベット90を挿入し、リベット90の挿入端部をかしめて接合される。また後接合部55のリブ部55Bと第2取付部70Cである中間翼部材73の後ろ壁部とは、第2取付部70Cに設けられた貫通孔70Yに後側から接合部材であるリベット90を挿入し、リベット90の挿入端部をかしめて接合される。   The main body portion 53A of the front joint portion 53 and the front end portion of the connection wall portion 73D, which is the first attachment portion 70B, are connected to the through-hole 53X provided in the main body portion 53A of the front joint portion 53 from the inside with a rivet 90 that is a joining member. The shaft portion is inserted, and the insertion end portion of the rivet 90 is caulked and joined. Further, the main body portion 55A of the rear joint portion 55 and the rear end portion of the connecting wall portion 73D as the first attachment portion 70B are joined to the through hole 55X provided in the main body portion 55A of the rear joint portion 55 from the inside by a joining member. A rivet 90 is inserted, and the insertion end of the rivet 90 is caulked and joined. Further, the rib portion 53B of the front joint portion 53 and the front wall portion 73B of the intermediate blade member 73 which is the second attachment portion 70C are rivets that are joining members from the front side to the through holes 70Y provided in the second attachment portion 70C. 90 is inserted, and the insertion end of the rivet 90 is caulked and joined. In addition, the rib portion 55B of the rear joint portion 55 and the rear wall portion of the intermediate blade member 73 that is the second attachment portion 70C are connected to the through hole 70Y provided in the second attachment portion 70C from the rear side by a rivet 90 that is a joint member. Is inserted, and the insertion end of the rivet 90 is caulked and joined.

次に、連結部材50を連結した中間翼部材73に対して、前側翼部材71及び後側翼部材75をはめ合わせてリベット90によって接合する。なお、中間翼部材73に対して、前側翼部材71及び後側翼部材75のどちらを先に接合してもよい。このようにして組み立てられた翼部材70は、中間翼部材73の凹部70Aが回転軸側の側面を凹ませて被連結部を形成していることになる。   Next, the front wing member 71 and the rear wing member 75 are fitted and joined to the intermediate wing member 73 to which the connecting member 50 is connected by the rivet 90. Note that either the front wing member 71 or the rear wing member 75 may be joined to the intermediate wing member 73 first. In the wing member 70 assembled in this manner, the concave portion 70A of the intermediate wing member 73 has a side surface on the rotating shaft side recessed to form a coupled portion.

このような構成を有する垂直軸型風車は、連結部材50の前接合部53及び後接合部55が回転軸の放射方向に直交する方向に拡がるプレート状の本体部53A,55Aの前端縁及び後端縁から回転軸側へ屈曲したリブ部53B,55Bを形成し、リブ部53B,55Bの外側面が翼部材70の第2取付部70Cである中間翼部材73の前壁部73B及び後壁部73Cに接合されている。このため、この垂直軸型風車は、連結部材50のリブ部53B,55Bが強度部材として働き、回転した際に翼部材70及び連結部材50に対して生じる曲げ応力を分散させることができる。よって、この垂直軸型風車は、回転数が高くなっても翼部材70と連結部材50との連結を良好に維持することができる。   In the vertical axis type wind turbine having such a configuration, the front end edge and the rear end of the plate-like main body portions 53A and 55A in which the front joint portion 53 and the rear joint portion 55 of the connecting member 50 extend in a direction orthogonal to the radial direction of the rotation shaft. Rib portions 53B and 55B that are bent from the end edge toward the rotating shaft side are formed, and the outer surface of the rib portions 53B and 55B is the second mounting portion 70C of the wing member 70. It is joined to the portion 73C. For this reason, in this vertical axis type windmill, the rib portions 53B and 55B of the connecting member 50 function as strength members, and the bending stress generated on the blade member 70 and the connecting member 50 when rotating can be dispersed. Therefore, this vertical axis type windmill can maintain the connection between the blade member 70 and the connecting member 50 well even when the rotational speed increases.

したがって、実施例1の垂直軸型風車は良好に回転することができる。   Therefore, the vertical axis type windmill of Example 1 can rotate satisfactorily.

また、この垂直軸型風車において、連結部材50のリブ部53B,55B及び翼部材70の第2取付部70Cは、リブ部53B,55B及び第2取付部70Cを貫通するリベット90によって接合されている。このリベット90は垂直回転軸風車が回転した際に翼部材70に生じる遠心力に略直交する方向に伸びている。このため、この垂直軸型風車は、リブ部53B,55Bと第2取付部70Cの接合面に沿ってリブ部53B,55Bと第2取付部70Cとがずれ難く、接合強度を高めることができる。   Further, in this vertical axis type windmill, the rib portions 53B and 55B of the connecting member 50 and the second mounting portion 70C of the wing member 70 are joined by a rivet 90 that penetrates the rib portions 53B and 55B and the second mounting portion 70C. Yes. The rivet 90 extends in a direction substantially perpendicular to the centrifugal force generated in the blade member 70 when the vertical rotating shaft wind turbine rotates. For this reason, in this vertical axis type windmill, the rib portions 53B, 55B and the second mounting portion 70C are not easily displaced along the bonding surfaces of the rib portions 53B, 55B and the second mounting portion 70C, and the bonding strength can be increased. .

また、この垂直軸型風車の翼部材70は回転軸側の側面を凹ませた凹部70Aが被連結部を形成している。この翼部材70は内側面より外側に露出しないように連結部材50と翼部材70とを連結することができる。このため、この垂直軸型風車は、翼部材70の周りを流れる空気の流れが乱れにくく揚力の減少を抑えることができるため、良好に回転することができる。   Further, in the blade member 70 of this vertical axis type wind turbine, a recessed portion 70A having a recessed side surface on the rotating shaft side forms a connected portion. The connecting member 50 and the wing member 70 can be connected so that the wing member 70 is not exposed to the outside from the inner side surface. For this reason, this vertical axis type windmill can rotate satisfactorily because the flow of air flowing around the wing member 70 is less likely to be disturbed and the reduction in lift can be suppressed.

また、この垂直軸型風車の翼部材70は、被連結部を形成している凹部70Aの開口部を塞ぎ、被連結部の周囲の翼部材70の内側面と段差なく連続するカバー77を有している。このため、この垂直軸型風車は、カバー77によって、翼部材70の周りを流れる空気の流れがスムーズになり揚力を良好に発揮することができるため、良好に回転することができる。   Further, the blade member 70 of this vertical axis type wind turbine has a cover 77 that closes the opening of the concave portion 70A forming the connected portion and is continuous with the inner side surface of the blade member 70 around the connected portion without any step. doing. For this reason, this vertical axis type windmill can rotate satisfactorily because the flow of the air flowing around the wing member 70 is smoothed by the cover 77 and the lift force can be exhibited well.

また、この垂直軸型風車の翼部材70は、被連結部を有する中間翼部材73と、この中間翼部材73の前端部に連結される前側翼部材71と、中間翼部材73の後端部に連結される後側翼部材75とを有している。このため、この垂直軸型風車は、中間翼部材73、前側翼部材71、及び後側翼部材75を組み付ける前に連結部材50と中間翼部材73とを連結することができる。このため、この垂直軸型風車は容易に組み立てることができる。   Further, the blade member 70 of the vertical axis type wind turbine includes an intermediate blade member 73 having a connected portion, a front blade member 71 connected to the front end portion of the intermediate blade member 73, and a rear end portion of the intermediate blade member 73. The rear wing member 75 is connected to the rear wing member 75. For this reason, this vertical axis type windmill can connect the connecting member 50 and the intermediate blade member 73 before assembling the intermediate blade member 73, the front blade member 71, and the rear blade member 75. For this reason, this vertical axis type windmill can be easily assembled.

本発明は上記記述及び図面によって説明した実施例1に限定されるものではなく、例えば次のような実施例も本発明の技術的範囲に含まれる。
(1)実施例1では、連結部材の連結部が、前傾斜部と後傾斜部とを有し、その間に空間を形成していたが、図7に示すように、空間有さない台形状の平板材によって連結部材150の連結部151を形成してもよい。
(2)実施例1では、前接合部と後接合部に分けて連結部材の連結部の本体部とリブ部とを形成していたが、図7に示すように、連結部材150の前後方向の全体に広がる平板材で接合部の本体部153を形成し、その両端を折り曲げてリブ部155を形成してもよい。
(3)実施例1では、リベットで連結部材と翼部材と接合していたが、他の手段で連結部材と翼部材とを接合してもよい。
(4)実施例1では、翼部材の回転軸側の側面を凹ませて被連結部を形成したが、翼部材の回転軸側の側面を凹ませずに被連結部を形成してもよい。
(5)実施例1では、凹部を覆うカバーを有していたが、カバーを有さなくてもよい。
(6)実施例1では、翼部材を前側翼部材、中間翼部材、及び後側翼部材から形成したが、翼全体を一体に形成してもよい。また、翼部材を2部材、又は4部材以上から形成してもよい。
(7)実施例1では、連結部材及び翼部材をアルミ合金で形成したが、他の素材で形成してもよい。
(8)実施例1では、回転軸部材が円筒状であり、発電機の回転軸部とともに回転自在であったが、回転軸部材を円柱状又は円筒状の軸部と、軸部の周りを回転自在に設けられた円筒部とによって形成してもよい。軸部を円筒状にすると、軸部内にケーブル等を通すことができる。
(9)実施例1では、蓋部材が翼部材の翼弦方向の断面と同じ形状であったが、翼部材の翼弦方向の断面よりも大きい形状で翼部材の内外側面からはみ出してもよい。また、蓋部材は翼弦方向の断面形状と相違する形状であってもよい。
The present invention is not limited to the first embodiment described with reference to the above description and drawings. For example, the following embodiments are also included in the technical scope of the present invention.
(1) In Example 1, the connecting portion of the connecting member has a front inclined portion and a rear inclined portion, and a space is formed between them, as shown in FIG. The connecting portion 151 of the connecting member 150 may be formed of a flat plate material.
(2) In Example 1, the main body part and the rib part of the connecting part of the connecting member were formed separately in the front joint part and the rear joint part, but as shown in FIG. The main body portion 153 of the joint portion may be formed of a flat plate material that spreads over the whole, and the rib portions 155 may be formed by bending both ends thereof.
(3) In the first embodiment, the connecting member and the wing member are joined by the rivet, but the connecting member and the wing member may be joined by other means.
(4) In Example 1, although the to-be-connected part was formed by denting the side surface on the rotating shaft side of the wing member, the to-be-connected part may be formed without denting the side surface on the rotating shaft side of the wing member. .
(5) In Example 1, the cover for covering the concave portion is provided, but the cover may not be provided.
(6) Although the wing member is formed of the front wing member, the intermediate wing member, and the rear wing member in the first embodiment, the entire wing member may be integrally formed. Further, the wing member may be formed of two members, or four or more members.
(7) In Example 1, the connecting member and the wing member are formed of an aluminum alloy, but may be formed of other materials.
(8) In the first embodiment, the rotating shaft member is cylindrical and can be rotated together with the rotating shaft portion of the generator. However, the rotating shaft member is arranged around a columnar or cylindrical shaft portion and the shaft portion. You may form with the cylindrical part provided rotatably. If the shaft portion is cylindrical, a cable or the like can be passed through the shaft portion.
(9) In Example 1, the lid member has the same shape as the cross section in the chord direction of the wing member. However, the lid member may protrude from the inner and outer surfaces of the wing member in a shape larger than the cross section in the chord direction of the wing member. . The lid member may have a shape different from the cross-sectional shape in the chord direction.

10…回転軸部材
30…アーム
50…連結部材
53A,55A…本体部
53B,55B…リブ部
70…翼部材
70A…凹部(被連結部)
70B…第1取付部
70C…第2取付部
71…前側翼部材
73…中間翼部材
75…後側翼部材
77…カバー
90…リベット(接合部材)
DESCRIPTION OF SYMBOLS 10 ... Rotary shaft member 30 ... Arm 50 ... Connecting member 53A, 55A ... Main-body part 53B, 55B ... Rib part 70 ... Wing member 70A ... Recessed part (to-be-connected part)
70B ... 1st attaching part 70C ... 2nd attaching part 71 ... Front side wing member 73 ... Intermediate wing member 75 ... Rear side wing member 77 ... Cover 90 ... Rivet (joining member)

Claims (5)

発電機に連結され、回転軸が垂直方向に伸びた状態に回転自在に立てられる回転軸部材と、
この回転軸部材から前記回転軸の放射方向に伸びるアームと、
このアームの先端部に設けられた連結部材と、
この連結部材に連結された翼部材と、
を備えた垂直軸型風車であって、
前記連結部材は、前記回転軸の放射方向に直交する方向に拡がるプレート状の本体部と、この本体部の前端縁及び後端縁から前記回転軸側へ屈曲したリブ部とを有しており、
前記翼部材は、前記連結部材の本体部の外側面に接合する第1取付部、及びリブ部の外側面に接合する第2取付部を具備した被連結部を有していることを特徴とする垂直軸型風車。
A rotating shaft member connected to the generator and rotatably standing in a state where the rotating shaft extends in the vertical direction;
An arm extending in a radial direction of the rotary shaft from the rotary shaft member;
A connecting member provided at the tip of the arm;
A wing member connected to the connecting member;
A vertical axis wind turbine with
The connecting member has a plate-like main body that extends in a direction perpendicular to the radial direction of the rotary shaft, and a rib that is bent toward the rotary shaft from the front and rear edges of the main body. ,
The wing member has a connected portion including a first attachment portion that is joined to the outer surface of the main body portion of the connection member and a second attachment portion that is joined to the outer surface of the rib portion. A vertical axis windmill.
前記連結部材のリブ部及び前記翼部材の第2取付部は、前記リブ部及び前記第2取付部を貫通する接合部材によって接合されていることを特徴とする請求項1記載の垂直軸型風車。   The vertical axis wind turbine according to claim 1, wherein the rib portion of the connecting member and the second attachment portion of the wing member are joined by a joining member that penetrates the rib portion and the second attachment portion. . 前記翼部材は回転軸側の側面を凹ませた凹部が前記被連結部を形成していることを特徴とする請求項1または2記載の垂直軸型風車。   The vertical axis type wind turbine according to claim 1 or 2, wherein the wing member has a recessed portion in which a side surface on a rotating shaft side is recessed to form the connected portion. 前記翼部材は、前記被連結部を形成する前記凹部の開口部を塞ぎ、前記被連結部の周囲の回転軸側の側面に段差無く連続するカバーを有していることを特徴とする請求項3記載の垂直軸型風車。   The wing member has a cover that closes an opening of the concave portion that forms the connected portion, and that is continuous without a step on a side surface on the rotating shaft side around the connected portion. 3. A vertical axis wind turbine according to 3. 前記翼部材は、前記被連結部を有する中間翼部材と、この中間翼部材の前端部に連結される前側翼部材と、前記中間翼部材の後端部に連結される後側翼部材とを有していることを特徴とする請求項1乃至4のいずれか1項記載の垂直軸型風車。   The blade member includes an intermediate blade member having the connected portion, a front blade member connected to a front end portion of the intermediate blade member, and a rear blade member connected to a rear end portion of the intermediate blade member. The vertical axis type windmill according to any one of claims 1 to 4, wherein the windmill is a vertical axis type windmill.
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WO2022202488A1 (en) * 2021-03-22 2022-09-29 Ntn株式会社 Wind turbine and wind power generation apparatus
JP7433134B2 (en) 2020-05-22 2024-02-19 三菱重工業株式会社 Wind turbine blade, wind turbine, and method for manufacturing a wind turbine blade

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JP2005042570A (en) * 2003-07-24 2005-02-17 Fjc:Kk Blade of wind turbine
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WO2018168705A1 (en) * 2017-03-13 2018-09-20 Ntn株式会社 Vertical shaft wind turbine and wind turbine generator
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