FIELD: heating.
SUBSTANCE: method of heat exchanger heating by gas-dynamic flow is characterized in that, the gas-dynamic flow is accelerated in the nozzle and due to the ejection it vacuumizes the cavity, the depression waves of which increase the pressure drop in the nozzle, which leads to the additional acceleration of the gas-dynamic flow, which is decelerated, and by the temperature got at gas-dynamic flow deceleration the heat exchanger is heated. The device for implementing the method of the heat exchanger heating, consisting a checker, including the nozzle, tightly connected between each other, forming between them the ejector evacuated cavity, and the heat exchanger, wherein not less than once or the tapering part of the nozzle is equipped with the heat exchanger, or not less than after one nozzle the heat exchanger is mounted, or available both simultaneously.
EFFECT: extension of gas acceleration method using and the device for its implementation.
2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
NOZZLE HEAD | 2011 |
|
RU2551289C2 |
SHESTERENKO'S SUPERNOZZLE (VERSIONS) | 2005 |
|
RU2361680C2 |
NOZZLE DEVICE | 2004 |
|
RU2303491C2 |
NOZZLE ASSEMBLY | 2003 |
|
RU2267360C2 |
SHESTERENKO(S SUPERSONIC NOZZLE | 2011 |
|
RU2574788C2 |
SHESTERENKO SUPERNOZZLE (VERSIONS) | 2004 |
|
RU2361679C2 |
SHESTERENKO'S HEAD PIECE (VERSIONS) | 2006 |
|
RU2356637C2 |
PROBE | 2001 |
|
RU2206410C2 |
SHESTERENKO'S ADAPTER NOZZLE | 2004 |
|
RU2346753C2 |
SHESTERENKO MOUTHPIECE | 2005 |
|
RU2354459C2 |
Authors
Dates
2017-05-02—Published
2012-01-23—Filed