FIELD: engines and pumps.
SUBSTANCE: rotary wind drive includes vertical mast with horizontal traverses, on which slot-type wings of non-closed profile are fixed by means of rubber-metal hinges and formed in nose part of U-shaped fairings, reinforced on external part of arc-shaped frames. In rear part, the wing skin is reinforced on rear inner side of frames so that a vertical through longitudinal slot is formed and edges of fairing and rear skin of wing are covered. Tie rods connect either adjacent, or in-pair located opposite wings of rotor to each other; mast of rotor is connected by means of gimbal joint to upper semi-axis of self-locking differential. Its lower semi-axis is connected through free-wheel clutch to fixed brake, and carrier is connected to conical main gear, the side gear of which is kinematically connected to low-speed compressor connected in parallel with own compressor of heat pump, conditioner, chiller or any other machine being useful mechanical load of wind drive.
EFFECT: easier control of wind drive and its coordination with load at improvement of manufacturability of the design and specific power.
8 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| THERMOBALANCED DIRIGIBLE | 2010 |
|
RU2457149C2 |
| SELF-LOCKING DIFFERENTIAL | 2011 |
|
RU2463501C1 |
| ROTOR WINDMILL | 2002 |
|
RU2269028C2 |
| AERODYNAMIC SCALE | 2012 |
|
RU2517778C2 |
| PROTECTIVE WET SUIT | 2010 |
|
RU2422323C1 |
| VANE BLADE | 2012 |
|
RU2499155C2 |
| SELF-SUSTAINED POWER AND HEAT SUPPLY SYSTEM FOR BUILDING | 2014 |
|
RU2569403C1 |
| ANGULAR DRIVE (VERSIONS) | 2009 |
|
RU2424446C2 |
| COMBINED HELICOPTER (VERSIONS) | 2009 |
|
RU2397919C1 |
| PROPULSION SYSTEM OF HIGH-SPEED ROTARY-WINGED AIRCRAFT (VERSIONS) | 2015 |
|
RU2629635C2 |
