KR20120004006A - Variable system of wind power turbine - Google Patents

Variable system of wind power turbine Download PDF

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Publication number
KR20120004006A
KR20120004006A KR1020100064619A KR20100064619A KR20120004006A KR 20120004006 A KR20120004006 A KR 20120004006A KR 1020100064619 A KR1020100064619 A KR 1020100064619A KR 20100064619 A KR20100064619 A KR 20100064619A KR 20120004006 A KR20120004006 A KR 20120004006A
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South Korea
Prior art keywords
tail wing
rotor
wind
wind turbine
tail
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KR1020100064619A
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Korean (ko)
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KR101151335B1 (en
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설창우
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(주)설텍
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    • 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
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06—Rotors
    • F03D1/065—Rotors characterised by their construction elements
    • F03D1/0675—Rotors characterised by their construction elements of the blades
    • 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 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022—Adjusting aerodynamic properties of the blades
    • F03D7/0232—Adjusting aerodynamic properties of the blades with flaps or slats
    • 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 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/0264—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for stopping; controlling in emergency situations
    • F03D7/0268—Parking or storm protection
    • 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
    • F05B2240/00—Components
    • F05B2240/20—Rotors
    • F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
    • 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
    • F05B2270/00—Control
    • F05B2270/30—Control parameters, e.g. input parameters
    • F05B2270/32—Wind speeds
    • 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
    • Y02E10/72—Wind turbines with rotation axis in wind direction

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  • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Wind Motors (AREA)

Abstract

PURPOSE: A variable device of a wind turbine is provided to naturally and automatically control retraction and return of a rotor and a tail vane by eccentricity, elevation-type folding unit, and gravity of the tail vane. CONSTITUTION: A variable device of a wind turbine comprises a body(1), a rotor(2), and a tail vane(3). The body is idled above a post(A). The rotor is installed in the front of the body and rotated by wind power. The tail vane is installed in a wind direction and let the rotor turn to be faced in the wind direction. The center of the vertical body is separated to one side from the major axis and installed eccentrically. The tail vane is inclined in an upward direction at the opposite side of a vertical eccentric part and folded.

Description

풍력 터빈의 가변장치{Variable system of wind power turbine}Variable system of wind power turbine

본 발명은 풍력 터빈에 관한 것으로, 더 상세하게는 태풍과 같이 풍속이 터빈의 발전시스템에 손상이 우려될 만한 세기로 발생되면 회전자 및 꼬리날개가 회피동작을 취함으로써 터빈 및 발전시스템을 풍속으로부터 보호되게 한 것이다.
The present invention relates to a wind turbine, and more particularly, when the wind speed is generated at such an intensity that the turbine's power generation system may be damaged, such as a typhoon, the rotor and the tail blades may avoid the wind turbine and power generation system from the wind speed. It is to be protected.

일반적으로 발전에 필요한 속도 이상의 풍속이 발생되면 과부하로 인해 발전시스템 및 터빈이 손상되는 것을 보호하기 위해 다양한 방법이 제안되고 있지만, 풍속변화에 따라 회전자와 꼬리날개를 각각 풍향에 대해 접혀지는 방식이 제안된 바 있었다.In general, various methods have been proposed to protect the power generation system and turbine from damage due to overload when wind speeds exceed the speed required for power generation.However, the rotor and tail wings are folded in the wind direction according to the wind speed change. It was proposed.

접힘에 의해 회피동작을 취하는 방식의 일 예로는 발명 제0594757호의 "풍력발전시스템에 있어서 풍속변화에 따른 꼬리날개 위치 가변장치"와 같이, 회전자가 장치된 몸체 후미에 꼬리날개를 힌지결합하고, 상기 꼬리날개는 일측에 견인줄을 결속시켜 견인줄에 의해 몸체 일측방향으로 접힐 수 있도록 구성되어 있으며, 그 작동은 풍속의 변화에 따른 센서의 감지에 의해 상기 꼬리날개를 모터의 동력으로 견인줄을 당겨서 몸체 일측으로 접으면 꼬리날개가 풍향을 추종함에 따라 회전자를 풍향과 마주보는 상태에서 직교로 선회시켜 회피동작을 취하게 되고, 반대로 견인줄을 풀어주면 다시 복귀하도록 되어 있다.An example of a method of taking the avoiding action by folding is to hinge-couple the tail blades to the rear of the body equipped with the rotor, such as "the device for changing the position of the tail blades according to the change of the wind speed in the wind power generation system" of No. 0594757. The wing is configured to bind the tow line on one side so that it can be folded in one side of the body by the tow line, the operation of which is connected to one side of the body by pulling the tow line by the power of the motor by the detection of the sensor according to the change of wind speed. As the tail wing follows the wind direction, the rotor rotates orthogonally in the state facing the wind direction, and the avoidance action is performed.

그러나, 종래와 같은 방식은 상기 회전자와 꼬리날개의 회피 및 복귀가 모터와 같은 동력에 의존하여 구동되고 있으며, 상기 모터의 구동 역시 풍속에 따른 센서의 감지 여부에 의해 결정되고 있었다.
However, in the conventional method, the avoidance and return of the rotor and the tail blades are driven depending on the same power as the motor, and the driving of the motor is also determined by the detection of the sensor according to the wind speed.

KR 10-0594757 "풍력발전시스템에 있어서 풍속변화에 따른 꼬리날개위치 가변장치"KR 10-0594757 "Variable tail wing position by wind speed change in wind power generation system"

본 발명은 종래와 같이 풍속에 따라 가변되는 회전자와 꼬리날개의 회피 및 복귀 동작을 기계적 전기적 출력 없이 풍속의 세기에 영향을 받아 자연적으로 달성되도록 함에 그 목적이 있다.
The object of the present invention is to enable the avoidance and return of the rotor and tail blades, which are variable according to the wind speed, to be naturally achieved under the influence of the wind speed without mechanical or electrical output.

본 발명은 상기 목적을 달성하기 위하여, 지주 상단에서 공회전 되도록 설치되는 몸체와; 상기 몸체 선단에 장착되어 풍속에 의해 회전되는 회전자와; 상기 몸체와 회전자의 주축 사이에 설치되어 풍력에 의한 회전으로 발전되는 발전시스템이 구성된 것을 포함하며, 상기 몸체 후미에 장착되어 풍향에 일직선이 되면서 회전자를 풍향과 마주보도록 선회시키는 꼬리날개로 된 통상의 풍력터빈에 있어서, The present invention and the body is installed to be idle in the upper end of the support to achieve the above object; A rotor mounted to the front end of the body and rotated by wind speed; It is installed between the main shaft of the body and the rotor comprises a power generation system configured to be generated by the rotation by the wind, and is mounted on the rear of the body is a straight tail of the rotor to face the wind direction while being in line with the wind direction In wind turbine of

상기 몸체는 지주의 주축을 중심으로 수직상 몸체(1) 중심을 일측으로 이격시켜 편심지도록 설치하고, 상기 꼬리날개는 몸체를 중심으로 수직상 편심부 반대측의 상측방향으로 기울어진 채 절첩되도록 구성한 것을 특징으로 한다.
The body is installed so as to be eccentric to the center of the vertical body (1) centered around the main axis of the support, and the tail wing is configured to be folded while being inclined in the upper direction opposite the vertical eccentric portion around the body It features.

본 발명의 풍력 터빈은 회전자를 지지하는 몸체가 지주로부터 편심지게 설치되어 젖혀지게 되어 있고, 꼬리날개는 사선으로 승강하면서 몸체로부터 접혀지도록 되어 있다.In the wind turbine of the present invention, the body supporting the rotor is eccentrically installed and retracted from the support, and the tail wing is folded from the body while lifting up diagonally.

이는 터빈 및 발전시스템에 손상을 유발하는 세기의 풍속이 발생되면 회전자는 편심 반대측으로 받는 하중이 커짐에 따라 풍향에 맞서는 상태에서 직교방향으로 젖혀지게 되고, 이때 꼬리날개는 몸체로부터 사선으로 승강하면서 접혀지는 회피동작을 취하며, 다시 풍속이 약해지면 사선으로 승강한 꼬리날개가 무게에 의해 하강하려는 힘이 풍속보다 강해지면서 회전자를 풍향과 마주보도록 선회시켜 자연적으로 복귀토록 한 것이다.This causes the rotor to be flipped in an orthogonal direction in the face of the wind direction as the load received on the opposite side of the eccentric increases when the wind speed of the intensity causing damage to the turbine and the power generation system is generated. When the wind speed weakens, the tail wing, which is raised diagonally, turns to face the wind direction as the force to descend by the weight becomes stronger than the wind speed, and then returns to nature.

따라서, 본 발명은 회전자 및 꼬리날개의 회피 그리고 복귀가 편심과 승강식 절첩수단 및 꼬리날개의 중력에 의해 자동으로 이루어짐으로써 기계적 전기적 출력 없이 자연적으로 구현되는 이점이 있다.
Accordingly, the present invention has the advantage that the avoidance and return of the rotor and the tail blades are automatically achieved by the eccentricity, the lifting means and the gravity of the tail blades, thereby being naturally implemented without mechanical or electrical output.

도 1은 본 발명의 전체 예시도
도 2는 본 발명의 요부 사시도
도 3의 (가)(나)는 본 발명의 꼬리날개를 후방에서 본 작동 예시도
도 4의 (가)(나)(다)는 본 발명을 평면에서 본 작동 예시도 이다.1 is an overall illustration of the present invention
2 is a perspective view of main parts of the present invention;
Figure 3 (a) (b) is an illustration of the operation of the tail wing of the present invention seen from the rear
4 (a) (b) (c) is an exemplary view showing the present invention in plan view.

이하 본 발명의 바람직한 실시 예를 첨부된 도면을 참조하여 상세히 설명하면 다음과 같다. 단, 상세한 설명에 있어 본 발명의 요지를 흐릴 수 있는 일반적인 기술내용이나 공지된 사항은 생략 또는 간단한 명칭 등으로 대체한다.
Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. However, in the detailed description, general description or well-known matters that may obscure the gist of the present invention are omitted or replaced with simple names.

본 발명은 지주(A) 상단에서 공회전 되도록 설치되는 몸체(1)와; 상기 몸체(1) 선단에 장착되어 풍속에 의해 회전되는 회전자(2)와; 상기 몸체(1)와 회전자(2)의 주축 사이에 설치되어 풍력에 의한 회전으로 발전되는 발전시스템이 구성된 것을 포함하며, 상기 몸체(1) 후미에 장착되어 풍향에 일직선이 되면서 회전자(2)를 풍향과 마주보도록 선회시키는 꼬리날개(3)로 된 통상의 풍력발전시스템에 있어서, 상기 몸체(1)는 지주(A)의 주축을 중심으로 수직상 몸체(1) 중심을 일측으로 이격시켜 편심지도록 설치하고, 상기 꼬리날개(3)는 몸체(1)를 중심으로 수직상 편심부(10) 반대측의 상측방향으로 기울어진 채 절첩되도록 구성한 것이다.
The present invention and the body (1) is installed to be idle in the upper end of the support (A); A rotor (2) mounted at the tip of the body (1) and rotated by wind speed; It is installed between the main shaft of the body (1) and the rotor (2) comprises a power generation system configured to be generated by the rotation by the wind, the rotor (2) mounted on the rear end of the body (1) to be in a straight line in the wind direction In the conventional wind power generation system having a tail wing (3) for turning the wind to face the wind direction, the body (1) is eccentric by spaced apart from the center of the vertical body (1) to one side about the main axis of the support (A) It is installed so that the tail wing 3 is configured to be folded while being inclined in an upward direction on the opposite side of the vertical eccentric portion 10 about the body 1.

더 상세하게는, 지주(A) 상단에서 공회전되되, 지주의 주축에서 몸체(1)가 이격된 채 편심지게 설치되도록 편심축부(10)를 가진 몸체(1)를 구성하고, 상기 몸체(1)의 선단에 장착되어 풍속에 의해 회전되는 회전자(2)가 구비되며, 상기 몸체(1) 내에 설치되어 몸체(1)와 회전자(2)의 주축 사이에서 풍력을 이용한 회전에 의해 발전되는 발전시스템이 구축되고, 상기 몸체(1)의 후미에 설치되어 풍향을 추종하면서 회전자(2)를 선회시켜 풍향과 맞서도록 하되, 주축이 몸체(1) 중심에서 수직상 일측으로 기울어지고, 기울어진 면이 수평에서 편심축부(10) 반대측의 상측방향으로 승강하면서 절첩되도록 한 꼬리날개(3)로 이루어진다.
More specifically, it is to be idle in the upper end of the support (A), to configure the body (1) having an eccentric shaft portion 10 so that the body (1) is installed eccentrically spaced apart from the main shaft of the support, the body (1) It is provided with a rotor (2) mounted at the front end of the rotation by the wind speed, is installed in the body (1) is generated by the rotation using the wind power between the main shaft of the body (1) and the rotor (2) The system is constructed and installed at the rear of the body (1) to rotate the rotor (2) to follow the wind direction while following the wind direction, so that the main axis is inclined toward one side vertically from the center of the body (1), the inclined surface It consists of a tail blade 3 which is made to be folded while raising and lowering in the upper direction opposite to the eccentric shaft part 10 in this horizontal direction.

본 발명에서 몸체(1)와 꼬리날개(3)의 절첩구성은, 몸체(1)는 후미에 절첩공간(13)을 가진 장착홈(11)을 형성하고, 꼬리날개(3)는 몸체 장착홈(11)에 개재될 수 있는 축부(30)를 마련하여, 힌지결합 함으로써 가능하다.
In the present invention, the folding configuration of the body 1 and the tail wing 3, the body 1 forms a mounting groove 11 having a folding space 13 at the rear, the tail wing 3 is the body mounting groove ( 11) it is possible by providing a shaft portion 30 that can be interposed, hinged.

더 상세하게는 첨부도면 도1 내지 도2와 같이, 상기 몸체(1)의 후미는 꼬리날개(3)의 축부(30)를 장착할 수 있게 기울어진 채 장착홈(11)을 형성하고, 이 장착홈(1)에 관통되는 축공(12), 그리고 이 축공(12)으로 부터 꼬리날개(3)의 축부(30)를 체결하는 볼트(4) 및 너트(41)가 구비되며, 상기 장착홈(11)에는 꼬리날개(3)의 주축이 기울어진 면을 따라 절첩공간(13)을 형성하여서 된다.
More specifically, as shown in FIGS. 1 and 2, the rear end of the body 1 forms a mounting groove 11 while being inclined to mount the shaft portion 30 of the tail wing 3. A shaft hole 12 penetrating the mounting groove 1 and a bolt 4 and a nut 41 for fastening the shaft portion 30 of the tail wing 3 from the shaft hole 12 are provided. In (11), the folding space 13 may be formed along the inclined surface of the main axis of the tail wing 3.

상기에서 꼬리날개(3) 및 장착홈(11)이 기울어지는 각도는 몸체(1) 중심으로부터 수직상 5°~20°사이로 하는 것이 바람직하고, 축부(30)와 볼트(4) 간에 축간 결합시 공차를 헐겁게 하여 공회전 되도록 하되, 작동이 원활하게 축부(30)에 베어링을 구성하여도 무방하다.
The angle at which the tail wing 3 and the mounting groove 11 are inclined is preferably 5 ° to 20 ° vertically from the center of the body 1, and is interaxially coupled between the shaft portion 30 and the bolt 4. The tolerance is loosened so as to be idle, but the bearing may be configured on the shaft portion 30 smoothly in operation.

상기 장착홈(11)은 편심축부(10) 방향으로 꼬리날개(3)를 몸체(1)와 일직선이 되는 위치를 잡아주는 내측패킹(14)을 구성하고, 상기 장착홈(11)의 접힘공간(13)에는 접힘시 꼬리날개(3)가 몸체(1)와 직교되는 위치를 잡아주는 외측패킹(15)을 구성하되, 내측패킹(14) 및 외측패킹(15)은 접촉시 충격 등이 완화 되도록 고무 등과 같은 완충소재로 구성함이 바람직하다.
The mounting groove 11 constitutes an inner packing 14 for holding the tail wing 3 in a straight line with the body 1 in the direction of the eccentric shaft portion 10, and a folding space of the mounting groove 11. In the (13), when the folded wing 3 is configured to the outer packing 15 to hold the position orthogonal to the body 1, the inner packing 14 and the outer packing 15 to mitigate the impact, such as when contacted Preferably, it is preferably composed of a buffer material such as rubber.

그리고, 상기에서 외측패킹(15)은 꼬리날개(3)가 절첩시 평면상 몸체에서 70°이하의 각도 내에서 멈춰지도록 가변위치를 제한케 함으로써, 꼬리날개(3)의 복귀능력을 향상할 수 있다.
In the above, the outer packing 15 is to limit the variable position so that the tail wing (3) is stopped within an angle of 70 ° or less from the body on the plane when folded, thereby improving the return capability of the tail wing (3). have.

상기 꼬리날개(3)는 기본적으로 연결대(31) 선단에 축공(300)을 가진 축부(30)가 구비되고 후미에는 날개판(32)이 부착되어 지되, 몸체(1)와 결합될 수 있는 축부(30)만 구비한다면 구조나 형태는 다양하게 변경할 수 있을 것이다.
The tail wing 3 is basically provided with a shaft portion 30 having a shaft hole 300 at the front end of the connecting rod 31 and the wing plate 32 is attached to the rear end, the shaft portion can be coupled to the body (1) If only 30 is provided, the structure or form may be changed in various ways.

본 발명의 작용은 첨부도면 도3 내지 도4와 같이 단계적으로 설명하면 다음과 같다.
The operation of the present invention will be described step by step as shown in Figures 3 to 4 as follows.

먼저 첨부도면 도 3의 (가)(나)와 같이, 몸체(1)는 주축(A)으로부터 편심지게 설치되어 일측으로 젖혀질 수 있고, 꼬리날개(3)는 수직상 기울어진 채 수평상 편심 반대측 상측 방향의 기울어진 면을 따라 접혀지도록 작용한다.
First, as shown in (a) and (b) of FIG. 3, the body 1 may be eccentrically installed from the main shaft A and be flipped to one side, and the tail wing 3 is horizontally eccentric while inclined vertically. It acts to fold along the inclined plane of the opposite side upwards.

상기 작용을 전제로 첨부도면 도 4의 (가)에서 (나)와 같이, 발전에 필요한 적정 세기 이상의 풍속이 발생하면 회전자에서 받는 하중이 커짐에 따라 몸체 편심축부를 중심으로 편심 반대측으로 쏠림현상이 발생되어 회전자(2)가 바람방향과 일직선으로 젖혀지게 되며, 이때 꼬리날개(3)는 몸체(1)로부터 접혀져 풍향을 추종하게 됨에 따라 회전자(2)와 꼬리날개(3)가 평행한 상태에서 풍향과 일직선이 된다.As shown in (a) to (b) of FIG. 4, when the wind speed more than the proper intensity required for power generation is generated, the load from the rotor increases and the body is oriented toward the opposite side of the eccentric shaft from the eccentric shaft part. This causes the rotor 2 to be folded in a straight line with the wind direction. At this time, the tail blades 3 are folded from the body 1 to follow the direction of the wind, so that the rotor 2 and the tail blades 3 are parallel to each other. In a state it is in line with the wind direction.

그러므로, 회전자(1)는 회전력이 급감하게 되면서 과부하를 방지할 수 있으므로 발전시스템 및 터빈을 강한 풍속으로부터 보호할 수 있게 된다.
Therefore, the rotor 1 can prevent the overload while reducing the rotational force, thereby protecting the power generation system and the turbine from the strong wind speed.

이어서, 첨부도면 도 4의 (다)와 같이 풍속이 다시 약해지면 꼬리날개(3)의 무게가 풍력에 의해 기울어진 면으로 승강하려는 힘보다 중력에 의해 낙하하는 힘이 강하게 작용하여 기울어진 면을 따라 다시 원위치로 복귀하게 되고, 이때 꼬리날개(3)가 몸체(1)와 일직선으로 유지하려고 하는 하중(W)이 몸체 후미의 편심 반대측에 가해지면서(몸체와 일체로 되려는 고정력을 갖게 됨) 회전자(2)를 풍향과 마주보도록 선회시키게 된다.Subsequently, when the wind speed is weakened again as shown in FIG. 4 (c), the weight of the tail blades 3 is lowered by gravity than the force to lift and lift the tilted surface. Then, it returns to its original position, and the load (W) that the tail wing (3) tries to keep in line with the body (1) is applied to the eccentric opposite side of the body aft (with the fixing force to be integral with the body). The electrons 2 are turned to face the wind direction.

상기에서 풍속변화에 따라 회전자(2)가 젖혀지는 풍속의 세기에서는 꼬리날개(3)도 같이 접혀져야 하며, 반면 회전자(2)가 젖혀지지 않는 풍속 세기에서는 꼬리날개(3)도 같이 접혀지지 않아야 한다. In the above-described strength of the wind speed that the rotor (2) is flipped in accordance with the change in wind speed, the tail wing (3) should be folded together, while in the wind speed strength that the rotor (2) is not flipped, the tail wing (3) is also folded together. It must not be supported.

즉 풍속의 세기에 따라 회전자(2) 및 꼬리날개(3)가 풍속에 영향을 받지 않고 버틸 수 있는 범위를 설정하여 발전량 및 규모를 결정할 수 있을 것이다.That is, the amount and scale of power generation may be determined by setting a range in which the rotor 2 and the tail blades 3 can stand without being affected by the wind speed.

이때 회전자(2)가 풍속에 대한 회피 및 버틸 수 있는 범위는 몸체(1)의 중심으로부터 편심축부(10)의 이격거리로 설정이 가능하고, 꼬리날개(3)가 몸체로부터 접힘 및 버틸 수 있는 범위는 사선으로 승강하는 각도와 꼬리날개의 무게 및 면적 등으로 설정이 가능할 것이다.
At this time, the range that the rotor (2) can avoid and stand against the wind speed can be set to the distance of the eccentric shaft portion 10 from the center of the body (1), the tail wing (3) can be folded and held from the body The range can be set by the angle of elevating the oblique line, the weight and the area of the tail wing, and the like.

본 발명은 상기와 같이 실시 예를 설명하였지만 해당기술분야의 숙련된 당업자는 본 발명의 특허청구범위에 기재된 사상 및 영역으로부터 벗어나지 않는 범위 내에서 다양하게 수정 및 변경하여 사용할 수 있을 것이다.
Although the present invention has been described in the above embodiments, those skilled in the art will be able to use variously modified and changed within the scope without departing from the spirit and scope described in the claims of the present invention.

A: 지주 1: 몸체
10: 편심축부 11: 장착홈
12: 축공 13: 절첩공간
14: 내측패킹 15: 외측패킹
2: 회전자 3: 꼬리날개
30: 축부 300: 축공
31: 연결대 32: 날개판
4: 볼트 41: 너트A: Shore 1: Body
10: Eccentric Shaft 11: Mounting Groove
12: Axis 13: Folded space
14: inner packing 15: outer packing
2: rotor 3: tail wing
30: shaft 300: shaft work
31: connecting rod 32: wing plate
4: bolt 41: nut

Claims (6)

지주(A) 상단에서 공회전 되도록 설치되는 몸체(1)와; 상기 몸체(1) 선단에 장착되어 풍속에 의해 회전되는 회전자(2)와; 상기 몸체(1) 후미에 장착되어 풍향에 일직선이 되면서 회전자(2)를 풍향과 마주보도록 선회시키는 꼬리날개(3)로 된 통상의 풍력 터빈에 있어서,
상기 몸체(1)는 지주(A)의 주축을 중심으로 수직상 몸체(1) 중심을 일측으로 이격시켜 편심지도록 설치하고, 상기 꼬리날개(3)는 몸체(1)를 중심으로 수직상 편심부(10) 반대측의 상측방향으로 기울어진 채 절첩되도록 구성한 것을 특징으로 하는 풍력 터빈의 가변장치.
Body (1) is installed to be idle in the upper end of the support (A); A rotor (2) mounted at the tip of the body (1) and rotated by wind speed; In the conventional wind turbine, which is mounted to the rear of the body (1) and the tail wing (3) for turning the rotor (2) to face the wind direction while being in a straight line in the wind direction,
The body (1) is installed so as to be eccentrically spaced apart from the center of the vertical body (1) with respect to the main axis of the support (A) to one side, the tail wing (3) is a vertical eccentric around the body (1) (10) A wind turbine variable device, characterized in that configured to be folded while being inclined in an upward direction on the opposite side.
제 1항에 있어서,
상기 꼬리날개(3)가 기울어진 각도는 5°~20°사이로 한정한 것을 특징으로 하는 풍력 터빈의 가변장치.
The method of claim 1,
The tilt angle of the tail blades (3) is variable in the wind turbine, characterized in that limited to between 5 ° ~ 20 °.
제 1항에 있어서,
상기 몸체(1)와 꼬리날개(3)의 절첩구성은, 몸체(1)는 후미에 절첩공간(13)을 가진 장착홈(11)을 형성하고, 꼬리날개(3)는 몸체(1) 장착홈(11) 내에 개재될 수 있는 축부(30)를 마련하여 힌지결합한 것을 특징으로 하는 풍력 터빈의 가변장치.
The method of claim 1,
The folding configuration of the body (1) and the tail wing (3), the body (1) forms a mounting groove 11 having a folding space 13 in the rear, the tail wing (3) is the body (1) mounting groove (11) Variable unit of the wind turbine, characterized in that the hinge is provided by providing the shaft portion 30 which can be interposed.
제 3항에 있어서,
상기 장착홈(11)에는 꼬리날개(3)가 하강시 평면상 몸체(1)와 일직선이 되는 위치에서 고정되도록 하는 내측패킹(14)과, 꼬리날개(3)가 절첩시 평면상 몸체(1)와 직교되는 위치에서 고정되도록 하는 외측패킹(15)이 구성되고, 상기 내측패킹(14) 및 외측패킹(15)은 고무와 같이 충격을 흡수할 수 있는 완충소재로 된 것을 특징으로 하는 풍력 터빈의 가변장치.
The method of claim 3, wherein
The mounting groove 11 has an inner packing 14 so that the tail wing 3 is fixed at a position in line with the planar body 1 when the tail wing 3 descends, and the planar body 1 when the tail wing 3 is folded. The outer packing 15 is configured to be fixed in a position orthogonal to the), and the inner packing 14 and the outer packing 15 is a wind turbine, characterized in that the shock absorbing material, such as rubber Variable device.
제 4항에 있어서,
상기 외측패킹(15)은 꼬리날개(3)가 절첩시 평면상 몸체에서 70°이상의 각도를 넘지 못하게 가변위치를 제한케 한 것을 특징으로하는 풍력 터빈의 가변장치.
The method of claim 4, wherein
The outer packing (15) is a wind turbine variable device, characterized in that to limit the variable position so that the tail wing (3) does not exceed an angle of more than 70 ° from the planar body when folded.
제 1항에 있어서,
상기 꼬리날개(3)는 연결대(31) 선단에 축공(300)을 가진 축부(30)가 구비되고 후미에는 날개판(32)이 부착된 것을 특징으로 하는 풍력 터빈의 가변장치.The method of claim 1,
The tail wing (3) is a variable unit of the wind turbine, characterized in that the shaft portion having a shaft hole (300) is provided at the front end of the connecting table (31) and the wing plate (32) is attached to the rear.
KR1020100064619A 2010-07-06 2010-07-06 Variable system of wind power turbine KR101151335B1 (en)

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KR101331169B1 (en) * 2012-09-26 2013-11-19 한국에너지기술연구원 Variable horizontal wing for small size wind powered generator and power control method of the same
CN105822501A (en) * 2016-03-17 2016-08-03 乐清市昊众电力科技有限公司 Actively folding tail vane of wind driven generator and hydraulic control system thereof
CN110985283A (en) * 2019-12-30 2020-04-10 上海致远绿色能源股份有限公司 Lateral deviation locking structure and method of lateral deviation type wind driven generator
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KR101331169B1 (en) * 2012-09-26 2013-11-19 한국에너지기술연구원 Variable horizontal wing for small size wind powered generator and power control method of the same
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CN103047083A (en) * 2012-12-22 2013-04-17 广州红鹰能源科技有限公司 Side-deviating type wind power generator and operating method thereof
CN105822501A (en) * 2016-03-17 2016-08-03 乐清市昊众电力科技有限公司 Actively folding tail vane of wind driven generator and hydraulic control system thereof
CN110985283A (en) * 2019-12-30 2020-04-10 上海致远绿色能源股份有限公司 Lateral deviation locking structure and method of lateral deviation type wind driven generator
CN113137333A (en) * 2021-05-21 2021-07-20 广州赛特新能源科技发展有限公司 Corrosion-resistant tail vane and wind driven generator

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