Airflow power installations
10018181 ยท 2018-07-10
Inventors
Cpc classification
Y02T10/90
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
F05B2240/941
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/17
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/728
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
Y02B10/30
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
Y02E10/72
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
F03D15/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/16
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
Y02E70/30
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
F03D13/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D3/0463
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A stationary power installation for conversion of wind airflow energy is proposed, including a cylindrical body having a top rim radially protruded from the body's walls. The rim includes a groove on its upper surface, guide rollers, support rollers peripherally mounted on the groove's bottom. The installation includes an upper level mounted above the body, having columns supporting a roof, a net screen peripherally surrounding the upper level's inner space, support members supporting an air compressor associated with a compressed air storage, a compressor gear conveying rotation to the compressor, a top shaft, a shutter including a lateral arc member having a bottom edge mounted in the groove and movable between the guide and support rollers, a nave situated above the roof, top bridge rods fixed to the top of arc member, a counter-load mounted diameteraly opposite to the arc member, a flat wind vane, and a brake mechanism.
Claims
1. A stationary power installation for conversion of wind airflow energy comprising: a lower level in the form of cylindrical body (35) having walls (33) and a top rim radially protruded from the walls, said rim including: a groove arranged on an upper surface of said rim, said groove includes vertical inner sides and a bottom, a number of guide rollers (46) peripherally mounted on the vertical inner sides of said groove, and a number of support rollers (47) peripherally mounted on the bottom of said groove; an upper level mounted above said lower level, said upper level including: an inner space and a floor, a number of columns (67) supporting a roof (68), a net screen (69) surrounding the inner space of said upper level, an upper X-shaped support member (34) horizontally disposed and located under the roof (68) and a lower X-shaped support member (43) horizontally disposed and located at the floor of said upper level; a turbine (38) fixed on a turbine shaft (42) rotatably supported substantially by said upper X-shaped support member (34) and said lower X-shaped support member (43), said turbine (38) having a plurality of blades (12) of a predetermined shape; an air compressor (40) mounted on said lower level; a compressed air tank (20) pneumatically associated with said air compressor (40); a belt gear (11-14) controllably conveying rotation of said turbine (38) to said air compressor (40); a top shaft (49) rotatably mounted on said upper X-shaped support member (34) and said lower X-shaped support member (43) above said upper level; a shutter (32) including: a lateral arc member shaped as a cylindrical arc segment, the bottom edge of said arc member is mounted in said groove and movable between said guide rollers (46) and said support rollers (47), a nave (48) fixedly mounted on said top shaft (49) and situated above said roof (68), top bridge rods coupled with said nave (48) and fixed to the top of said arc member, said top bridge rods supporting said arc member, and a counter-load (37) mounted on said nave (48) situated diameteraly opposite to said arc member; a flat wind vane (36) vertically fixed in to said nave (48), wherein the plane of said flat wind vane (36) is situated at a predetermined angle to a corresponding arc radius ending at the center of said arc member; and a brake mechanism essentially mounted to said lower level, said brake mechanism including: a disc (50) fixed on said turbine shaft (42), a pneumo-cylinder (70) communicated with said compressed air tank (20), a piston (70P) slidely mounted within said pneumo-cylinder (70), coupled to a rod and capable of vertical displacement upward and downward depending on the air pressure in said compressed air tank (20), and a lever (44-45) pivotally mounted substantially to said lower level, a first end of said lever (44-45) is attached to the upper end of the rod, and a second end of the lever (44-45) is furnished with a braking plate (51), said lever (44-45) is capable of conveying a braking force to said disc (50) through said plate (51) at a predetermined threshold pressure in said compressed air tank (20).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
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DETAIL DESCRIPTION OF PREFERRED EMBODIMENTS OF THE INVENTION
(5) While the invention may be susceptible to embodiment in different forms, there are shown in the drawings, and will be described in detail herein, specific embodiments of the present invention, with the understanding that the present disclosure is to be considered an exemplification of the principles of the invention, and is not intended to limit the invention to that as illustrated and described herein.
(6) Stationary Wind Airflow Power Installation
(7) The present invention may be embodied as a stationary wind airflow power installation (or SWAPI) illustrated on
(8) The upper level includes a number of columns or polls 67 (
(9) The SWAPI comprises support bearings (not shown) disposed in the centers of the members 34 and 43; a horizontal turbine 38 (
(10) As shown on
(11) The SWAPI comprises a shutter 32 (
(12) The SWAPI comprises a flat wind vane 36 (
(13) The SWAPI comprises a tank 20 (
(14) The SWAPI comprises a brake mechanism preferably attached to the ceiling of the lower level. The brake mechanism includes a disc 50 fixed on the turbine shaft 42 above the driving pulley 11 (as shown on
(15) The brake mechanism includes a substantially horizontal lever 44-45 (shown on
(16) The SWAPI operates as follows: the wind airflow encounters the vane 36 with the arc member of shutter 32 and turns them at a certain angle depending on its direction and intensity. It creates an asymmetrical configuration causing an uneven distribution of the airflow among the blades 12 of the turbine 38 that starts rotating. The rotation is conveyed from the turbine shaft 42, the gear pulleys 11 and 14 to the pump 40. When the air pressure in the tank 20 is lower than a predetermined lowest threshold, the control system opens the valves for inlet of compressed air from the pump 40 into the tank 20, until the pressure reaches a predetermined uppermost threshold, whereat the piston 70P rises such that acting upon the lever 44-45.
(17) The pressurized air can be utilized for various purposes: e.g., for rotation of a pneumo-motor (not shown on