METHOD OF AND DEVICE FOR CONVERTING ENERGY OF WIND Russian patent published in 2005 - IPC

Abstract RU 2249723 C2

FIELD: wind power engineering.

SUBSTANCE: invention can be used for converting energy of air flows into electric energy. Proposed method includes passing of first on-coming air flow between two conversing and diverging aerodynamic surfaces in direction of flow to form zone of reduced pressure and transmitting of second air flow along pipeline from surrounding space into zone of reduced pressure. Converter is installed on way of second air flow. Space is made in zone of reduced pressure in, at least, one of aerodynamic surfaces to provide swirling of second air flow by wall of said space. Swirling of second air flow is formed tangentially in direction of passing of first on-coming air flow. Device contains two plates. Pipeline is designed to transmit second air flow. One end of pipeline is made open and it is connected with surrounding space, and other end is connected to outer surface of one of plates. Converter is installed in pipeline. AT least one of plates is provided with space to swirl second air flow. Space communicates with pipeline. Space is made orthogonally relative to direction of first on-coming air flow tangentially in direction of first on-coming air flow.

EFFECT: improved efficiency of energy conversion.

23 cl, 14 dwg

Similar patents RU2249723C2

Title Year Author Number
ROAD VEHICLE BODY (VERSIONS) 2003
  • Nefedov Sergej Ivanovich
RU2270125C2
METHOD OF REDUCING DRAG OF MOVING OBJECT AND DEVICE FOR ITS EMBODIMENT 2000
  • Nemykin A.S.
  • Nefedov S.I.
RU2173658C1
METHOD OF SUPPLY OF POWER TO AEROSTAT 1995
  • Pikul' Vadim Nikolaevich
RU2093414C1
VORTEX EJECTOR 2019
  • Serebryakov Rudolf Anatolevich
  • Dorzhiev Sergej Sodnomovich
RU2703119C1
AEROSPACE AIRCRAFT (VERSIONS) 2008
  • Beljaev Vjacheslav Ivanovich
RU2397924C2
FLYING VEHICLE, BOUNDARY LAYER SUCTION CONTROL SYSTEM, CONTROL SYSTEM OF INJECTION TO BOUNDARY LAYER, DEVICE FOR FIXING POSITION OF SHEDDING OF FLOW FROM TRAILING EDGE OF FUSELAGE AND ITS AIR CUSHION ALIGHTING GEAR 1992
  • Shchukin L.N.
  • Savitskij A.I.
  • Shchukin I.L.
  • Mass A.M.
  • Karelin V.G.
  • Shibanov A.P.
  • Sobko A.P.
  • Ermishin A.V.
  • Khutsishvili V.G.
  • Pushkin R.M.
  • Fishchenko S.V.
RU2033945C1
HOLLOW SOFT WING WITH AIR INTAKE AT TIP AND SHAPED SLOT ON UPPER SURFACE 2008
  • Shved Jurij Vital'Evich
RU2389644C2
METHOD OF SUPPLY OF POWER TO AEROSTAT 2001
  • Pikul' V.N.
RU2196072C2
AIRCRAFT RAMJET ENGINE 2004
  • Prudnikov Aleksandr Grigor'Evich
  • Sokolovskij Gennadij Aleksandrovich
  • Janovskij Jurij Grigor'Evich
RU2269022C2
SELF-ADJUSTABLE AIR INTAKE 1997
  • Medvedev V.T.
RU2171211C2

RU 2 249 723 C2

Authors

Nefedov S.I.

Dates

2005-04-10Published

2003-03-31Filed