SU150065A1 - Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6) - Google Patents

Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6)

Info

Publication number
SU150065A1
SU150065A1 SU725726A SU725726A SU150065A1 SU 150065 A1 SU150065 A1 SU 150065A1 SU 725726 A SU725726 A SU 725726A SU 725726 A SU725726 A SU 725726A SU 150065 A1 SU150065 A1 SU 150065A1
Authority
SU
USSR - Soviet Union
Prior art keywords
speed
wind
adjusting
small high
wheel
Prior art date
Application number
SU725726A
Other languages
Russian (ru)
Inventor
В.Н. Волостных
М.О. Франкфурт
Original Assignee
В.Н. Волостных
М.О. Франкфурт
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 В.Н. Волостных, М.О. Франкфурт filed Critical В.Н. Волостных
Priority to SU725726A priority Critical patent/SU150065A1/en
Application granted granted Critical
Publication of SU150065A1 publication Critical patent/SU150065A1/en

Links

Classifications

    • 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
    • Y02E10/72Wind turbines with rotation axis in wind direction

Landscapes

  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

В известных способах регулировани  оборотов небольших быстроходных ветровых колес (z 3-r6) нутем их вывода из-под ветра поворотом относительно вертикальной оси головки не обеспечнВаетс  достаточна  динамическа  устойчивость системы при соответствуюш,ей закономьрности изменени  поворотного момента ветрового колеса.In the known methods of controlling the revolutions of small high-speed wind wheels (z 3-r6), by removing them from the wind by rotating the head about the vertical axis of the head, the dynamic stability of the system is not sufficient, if the turning wheel of the wind wheel changes accordingly.

В предлагаемом способе этот недостаток устранен тем, что на лобовой стороне крыльев ветрового колеса помещают жесткие открылки, концентрично расположенные относительно оси вращени  колеса.In the proposed method, this disadvantage is eliminated by the fact that on the front side of the wings of the wind wheel, there are rigid wing panels concentrically located relative to the axis of rotation of the wheel.

На фиг. 1 схематически изображено осуществление способа; на фиг. 2 - графические характеристики коэффициентов касательных сил.FIG. 1 schematically shows the implementation of the method; in fig. 2 - graphic characteristics of the coefficients of tangential forces.

Предлагаемый способ изменени  формы характеристик поворотных моментов ветроколеса 1 предусматривает установку на его лопаст х 2 неподвижных односторонних открылков 3. При расположении открылков со стороны набегающего потока концентрично оси вращени  ветроколеса они практически не вли ют -на мощностные характеристики ветроколеса при его нормальном обтекании. В то же врем  при косой обдувке ветроколеса присутствие открылков существенно сказываетс  на моменте аэродинамических сил, поворачивающем ветроколесо около оси головки ветродвигател . Это подтверждаетс  фиг. 2, на которой даны характеристики коэффициентов касательных сил т / (г) и центра парусности Z f (z) быстроходного ветроколеса при различных углах его косой обдувки Yi, полученные при испытани х модели в аэродинамической трубе. Как видим, при наличии открылков не только увеличиваютс  касательные силы, но и наблюдаетс  смещение центра парусности к задней кромке ветроколеса, благодар  чему момент от сил лобово-го давлени  становитс  положительным при любых углах его косой обдувки.The proposed method of changing the shape of the characteristics of the turning points of the windwheel 1 provides for the installation on its blades x 2 fixed one-sided wings 3. With the location of the wings from the side of the incident flow concentric with the axis of rotation of the wind-wheel, they practically do not affect the power characteristics of the wind-wheel during its normal flow. At the same time, in the case of oblique blowing of the wind-wheel, the presence of the wings significantly affects the moment of aerodynamic forces turning the wind-wheel near the axis of the head of the wind turbine. This is confirmed by FIG. 2, which gives the characteristics of the coefficients of the tangential forces t / (g) and the center of sail Z f (z) of the high-speed propeller at different angles of its oblique blowing Yi, obtained from testing the model in a wind tunnel. As you can see, in the presence of an velcque, not only the tangential forces increase, but also the displacement of the center of the windage to the rear edge of the windwheel is observed, due to which the moment from the frontal pressure forces becomes positive at any angles of its oblique blowing.

№ 150065No. 150065

Предмет изобретени Subject invention

Способ регулировани  оборотов небольших быстроходных ветровых колес (z ) путем их: вывода из-под ветр-а поворотом относительно вертикальной оси головки, отличающийс  тем, что, с целью обеспечени  динамической устойчивости системы при соответствующей закономерности изменени  поворотного момента ветрового колеса, на лобовой стороне его крыльев помещают жесткие открылки, концентрично расположенные относнтелыно оси вращени  колеса.The method of controlling the revolutions of small high-speed wind wheels (z) by means of their: output from under the wind by turning about the vertical axis of the head, characterized in that, in order to ensure the dynamic stability of the system with a corresponding pattern of change of the turning point of the wind wheel, on its front side Wings placed rigid wing, concentrically located relative to the axis of rotation of the wheel.

2 2

Направление потомDirection later

Фи2.1Phi2.1

SU725726A 1961-04-10 1961-04-10 Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6) SU150065A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU725726A SU150065A1 (en) 1961-04-10 1961-04-10 Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU725726A SU150065A1 (en) 1961-04-10 1961-04-10 Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6)

Publications (1)

Publication Number Publication Date
SU150065A1 true SU150065A1 (en) 1961-11-30

Family

ID=48305078

Family Applications (1)

Application Number Title Priority Date Filing Date
SU725726A SU150065A1 (en) 1961-04-10 1961-04-10 Method of adjusting the speed of small high-speed wind wheels (z = 3 - 6)

Country Status (1)

Country Link
SU (1) SU150065A1 (en)

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