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WO2011112065A1 - Turbine éolienne comportant un rotor cylindrique - Google Patents

Turbine éolienne comportant un rotor cylindrique Download PDF

Info

Publication number
WO2011112065A1
WO2011112065A1 PCT/LT2010/000003 LT2010000003W WO2011112065A1 WO 2011112065 A1 WO2011112065 A1 WO 2011112065A1 LT 2010000003 W LT2010000003 W LT 2010000003W WO 2011112065 A1 WO2011112065 A1 WO 2011112065A1
Authority
WO
WIPO (PCT)
Prior art keywords
wind
rotor
vane
width
receiver
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/LT2010/000003
Other languages
English (en)
Inventor
Sergej Gurtovoj
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of WO2011112065A1 publication Critical patent/WO2011112065A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/04Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F03D3/0436Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels for shielding one side of the rotor
    • F03D3/0472Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels for shielding one side of the rotor the shield orientation being adaptable to the wind motor
    • F03D3/049Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels for shielding one side of the rotor the shield orientation being adaptable to the wind motor with converging inlets, i.e. the shield intercepting an area greater than the effective rotor area
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/10Stators
    • F05B2240/13Stators to collect or cause flow towards or away from turbines
    • 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

Definitions

  • This invention is related to the field of wind power, specifically belonging to wind turbines with a cylinder rotor.
  • the wind generator is placed directly on the surface of the earth
  • This turbine has the following shortcomings:
  • the back rotor nacelle creates a large resistance to the airflow.
  • the rotor and nacelle become windproof almost like a flat hard obstacle with a small opening at the bottom. According to Figures 1 and 2 the width of this opening is equal to a maximum 1.5 times the width of the rotor blade; therefore, this structure has a low efficiency.
  • the rotor works at 1.5 times the load of the blade.
  • the remaining airflow bypasses the structure of the wind generator;
  • the wind generator is placed on the surface of the earth, which reduces its effectiveness, because of the numerous obstacles (buildings, forest) the velocity of the wind there is lower than that above.
  • a pole would be required, the manufacturing of which would require a large amount of materials;
  • the structure of the wind baffle, wind receiver and vane compared to the functions they perform is not rational and consumes a large amount of materials.
  • the wind generator is placed directly on the surface of the earth
  • This turbine is characterised not only by the same shortcomings as the one described above, but also by several additional ones:
  • the wind generator is often oriented downwind in an unstable manner, as it will swing at an amplitude of approximately 50°;
  • the vane is also placed on the ground, which prevents the placement of the wind generator above the ground.
  • this structure will be unable to operate.
  • the passage for the direct airflow is closed and it cannot return against itself.
  • the wind will have to flow through the structure of the wind generator as through a continuous obstacle similar to that of a wall (See Fig. 1A).
  • This structure has the following shortcomings:
  • the wind baffle battles with the vane creating the axel weight and poorly performs its second designated purpose - the release of the airflow onto the rotor blade.
  • Blades complicate the rotor structure, as well as its price; they also do not increase the rotation moment in comparison to the probable distribution of the rotor blades.
  • the ratio of the blade width in respect to the rotor diameter is 1/3; in addition, their number and form are optimal.
  • the wind vane is placed in the wind shadow of the rotor and moved to the opposite side of the wind baffle.
  • This structure has the following shortcomings:
  • the purpose of the invention is to create a highly efficient wind generator characterised by reliable construction and operating in a wide range of wind velocities.
  • the wind turbine with a cylinder rotor and wind deflecting device which includes the wind receiver, wind baffle and vane mantled on a rotating axle, is characterised by the fact that the rotor can have from 2 to 10 blades given the following ratio of the sizes of the elements:
  • the ratio of the width of the blade to its length is: 1:4 - 1 :8;
  • angles yand ⁇ correspondingly comprise 0° - 28° and 20° - 45°;
  • the wind turbine is also characterised by the fact that the sizes and positions of the wind receiver, wind baffle and wind vane are interrelated and their calculation is subject to the size of the rotor and the established average annual wind velocity in a particular region.
  • the curve of a cross-section of the blade must correspond to the minimum air resistance at the moment of motion with its arched section forward.
  • the wind turbine has top and bottom wings Ri and R 2 with the following measurements:
  • the width of the wing is equal to 0.4 - 0.8 of the width of the rotor blade, the length of the wing is equal to 1 ⁇ 2 times the width of the rotor blade.
  • the wings are placed on the active back part of the rotor and can be asymmetrical in relation to the vane axle.
  • the wind turbine is additionally characterised by having the vane constructed in a way that enables it to rotate in the planar and perpendicular motion in relation to the rotation axis and in the position parallel to the rotation axis.
  • Fig. 1 - depicts the schemes of the wind generator with a cylinder rotor of an existing technical level.
  • Fig. 2 - depicts the wind generator with a cylinder rotor indicating the scheme of the wind flow.
  • Fig. 3 - depicts the wind generator with a cylinder rotor including the scheme of the established measurements of the lines.
  • Fig. 4 - depicts the wind generator with a cylinder rotor including the scheme of the established measurements of the lines.
  • Fig. 5 - depicts the scheme of the wind generator with a cylinder rotor in the position when the wind vane is assembled.
  • Fig. 6 - depicts a general image of the wind generator with a cylinder rotor.
  • Fig. 7 - depicts possible forms of the blades.
  • the construction presented depends on the wind generator with a cylinder rotor.
  • the rotor is constructed from arched blades (marked with a letter B in Fig. 2-4), which are attached to the rotary axle (marked with a letter A in Fig. 2-4).
  • a solid construction is placed on this axle A, which consists of: - the wind baffle (marked with a letter C in Fig. 2-4) with an arch (marked with a letter R in Fig. 2-4);
  • This structure and rotor are able to rotate on the axle with respect to each other.
  • the electricity generator (marked with a letter G in Fig. 2-4) is placed on the bottom of the rotor - the pillar is reinforced with the help of strainers (marked with a letter E in Fig. 2-4), which are placed at an angle of 120° with respect to each other.
  • the ratio of the width of the blade (marked with a letter B in Fig. 2-4) to its length is approximately equal to 1/4.
  • the ratio of the width of blade B to the rotor diameter is approximately equal to 1/3.
  • the angle of the wind attack on the plane of the wind baffle C and wind receiver D (marked with a letter a in Fig. 1 a) is 30° - 45°.
  • the product of the width of the wind receiver (marked as Ld in Fig. 3) from the arm (marked as Pd in Fig. 3) side of the designed downwind forces (marked as Fd in Fig. 3) is equal to the product of the width of the wind baffle (marked as Lc in Fig. 3) from the arm (marked as Pc in Fig. 3) side of the designed downwind forces (marked as Fc in Fig. 2):
  • the ratio of the wind force created with the help of the vane width (marked as Sh in Fig. 4) and the arm (marked as Ph in Fig. 4) product to the wind force created with the hel of the product of the section of the wind baffle width (marked as Sc in figure 4) and the arm (marked as Pc in Fig. 4) should be larger than 1.5.
  • the wind baffle C ends with an arch along its entire width (marked with a letter R in Fig. 2), the size of which, when projected downwind, is equal to (0.2 ⁇ 0.5) Lc.
  • the top and bottom wings (Ri and R 2 in Fig. 2; 4) have the following measurements:
  • the width of the wing is equal to 0.4 - 0.8 of the width of the rotor blade
  • the wing length is equal to 1 ⁇ 2 times the width of the rotor blade.
  • the wind baffle C (Fig. 2) protects the arched sides of the rotor blades from the airflow and directs it towards the dented sides of the rotor blades.
  • Wind receiver D (Fig. 2) catches the airflow and also directs it towards the dented sides of the rotor blades.
  • Wind pressure on the wind baffle and wind receiver creates forces Fc and Fd (Fig. 2).
  • the positioning and proportions of the wind baffle and wind receiver allow maintenance of the balance of the structure (wind baffle, wind receiver and wind vane) when affected by the wind.
  • the wind vane H (Fig. 2) orients the structure against the wind flow. As depicted in Fig.
  • Wind baffle C ends in an arch R (Fig. 2), which creates a discharge in the passive zone of the rotor blade area.
  • Wings Ri and R 2 also create discharge in the passive zone of the rotor area in order to increase the wind flow in the active area of the rotor.
  • the wind vane H (Fig. 2, 3) can be lowered parallel to the rotor axle A rotating around the hinge Z (Fig. 2, 3), or to turn along the lower line at 90°, in order to reduce resistance to the airflow.
  • the vane In the condition of a storm- force wind, the vane is lowered and turned, while the wind generator construction is placed in the position with the lowest resistance to the airflow, and the rotor is able to continue operating at a light duty (Fig. 5).
  • the presented wind generator with a cylinder rotor has significant differences when compared to the existing ones and is characterised by the following features:
  • the form, number and measurements of the blades are - The form, number and measurements of the blades.
  • the optimal ratio of the width of the blade to the rotor diameter is 1/3, while the ratio of the width of the blade to its length is 1/4.

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 porte sur le domaine de l'énergie éolienne, plus précisément sur les turbines éoliennes comportant un rotor cylindrique, un récepteur de vent et un déflecteur de vent. Nous avons présenté la structure et le rapport des mesures des plans principaux de la génératrice éolienne. La construction proposée est efficace et fiable en présence de différentes vitesses de vent.
PCT/LT2010/000003 2010-03-08 2010-12-22 Turbine éolienne comportant un rotor cylindrique Ceased WO2011112065A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
LTLT2010020 2010-03-08
LT2010020A LT5702B (lt) 2010-03-08 2010-03-08 Vėjo jėgainė su cilindriniu rotoriumi

Publications (1)

Publication Number Publication Date
WO2011112065A1 true WO2011112065A1 (fr) 2011-09-15

Family

ID=42984340

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/LT2010/000003 Ceased WO2011112065A1 (fr) 2010-03-08 2010-12-22 Turbine éolienne comportant un rotor cylindrique

Country Status (2)

Country Link
LT (1) LT5702B (fr)
WO (1) WO2011112065A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017077648A (ja) * 2015-10-19 2017-04-27 横浜ゴム株式会社 タイヤ用ビードフィラの癖付け方法および装置並びにビード部材の製造方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1467248A1 (ru) * 1987-07-08 1989-03-23 Л.А.Шадурко Роторный ветродвигатель
RU2006665C1 (ru) * 1991-02-01 1994-01-30 Адхам Закирович Султанов Карусельный ветродвигатель
US5380149A (en) * 1990-05-31 1995-01-10 Valsamidis; Michael Wind turbine cross wind machine
JPH09296774A (ja) * 1996-05-02 1997-11-18 Makoto Suda 導風型風車装置
RU2168059C2 (ru) * 1999-07-27 2001-05-27 Баранов Александр Николаевич Ветродвигатель
RU81774U1 (ru) * 2008-10-30 2009-03-27 Владимир Ефимович Швалев Ветродвигатель

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US500956A (en) 1893-07-04 Meat-rack
US10199A (en) 1853-11-01 William t
US4017204A (en) 1974-06-28 1977-04-12 Sellman Donald L Wind motors
US4198280A (en) 1978-12-19 1980-04-15 American Hospital Supply Corporation Membrane support structure for electrochemical sensing probe
US4260325A (en) 1979-11-07 1981-04-07 Cymara Hermann K Panemone wind turbine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1467248A1 (ru) * 1987-07-08 1989-03-23 Л.А.Шадурко Роторный ветродвигатель
US5380149A (en) * 1990-05-31 1995-01-10 Valsamidis; Michael Wind turbine cross wind machine
RU2006665C1 (ru) * 1991-02-01 1994-01-30 Адхам Закирович Султанов Карусельный ветродвигатель
JPH09296774A (ja) * 1996-05-02 1997-11-18 Makoto Suda 導風型風車装置
RU2168059C2 (ru) * 1999-07-27 2001-05-27 Баранов Александр Николаевич Ветродвигатель
RU81774U1 (ru) * 2008-10-30 2009-03-27 Владимир Ефимович Швалев Ветродвигатель

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017077648A (ja) * 2015-10-19 2017-04-27 横浜ゴム株式会社 タイヤ用ビードフィラの癖付け方法および装置並びにビード部材の製造方法

Also Published As

Publication number Publication date
LT2010020A (en) 2010-10-25
LT5702B (lt) 2010-12-27

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