Condensation type kinetic energy and power conversion device and heat power system thereof
A power conversion and condensing technology, which is applied to non-variable engines, engine components, machines/engines, etc., can solve the problems of large size, heavy weight, and high cost
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0113] like figure 1 The shown condensing kinetic energy power conversion device includes a rotating shaft 1, a turbine blade 2, a nozzle 3 and a casing 4, the rotating shaft 1 is arranged in the casing 4, and the turbine blade 2 is arranged in the casing 4. On the rotating shaft 1, a condensation cooling zone is set in the turbine blade 2, a liquid outlet 5 is set on the casing 4 and on the rotating shaft 1, The condensable gas working medium inlet 6, the working medium outlet of the nozzle 3 is communicated with the condensable gas working medium inlet 6.
[0114] In order to eliminate the loss of residual velocity to the greatest extent, in this embodiment and all the following embodiments including the turbine blade 2, the condensable gas working medium introduced through the nozzle 3 can be placed in the turbine blade. 2 and leaves the turbine blades 2 in liquid form into the liquid outlet 5 .
Embodiment 2
[0116] like figure 2 In the shown condensing type kinetic energy power conversion device, on the basis of Embodiment 1, the turbine blade 2 is further set as an axial flow blade 22 , and a liquid outlet 5 is added on the turbine blade 2 .
Embodiment 3
[0118] like image 3 The shown condensing type kinetic energy power conversion device, on the basis of Example 2, further adds a condensable gas working medium inlet 6 on the rotating shaft 1, and makes the working medium outlet of the nozzle 3 and the added station. The condensable gas working medium inlet 6 communicates with each other, and at the same time, the liquid outlet 5 provided on the turbine blade 2 and the rotating shaft 1 is eliminated.
[0119] In this embodiment, the nozzle 3 communicating with the condensable gas working medium inlet 6 provided on the rotating shaft 1 is set as a Laval nozzle 31 .
[0120] As an alternative embodiment, the condensable gas working medium inlet 6 can also be set on the turbine blade 2 and communicated with the nozzle 3. The specific setting method can be rotated with reference to this embodiment. The communication mode between the condensable gas working medium inlet 6 on the shaft and the nozzle 3 .
[0121] As an alternative...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


