Compression device for rotating blade type compressor
A compression device and a technology of rotating blades, applied in the field of compressors, can solve the problems of gaseous refrigerant suction loss, lower compression efficiency and compressor reliability, and difficulty in sucking gaseous refrigerant, so as to prevent friction loss and improve compression efficiency and reliability Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0045] Fig. 4 is a transverse sectional view of Embodiment 1 of the compression device of the rotary vane compressor of the present invention.
[0046] Usually, the annular vane on the rotary vane of the rotary vane compressor rotates inside the cylinder under the drive of the crankshaft, and forms inner and outer compression chambers inside the cylinder.
[0047] As shown in Figure 4, the cylinder 4 of the compression device of the rotary vane compressor of the present invention is formed with an operating space 110 of annular blades 140, and a sealing member 110a is used to form a closed circular structure on one side of the operating space 110; The one side end and the other side end of the operating space 110 are respectively formed with a side air inlet 43 and inner and outer air outlets 44, 44a.
[0048] There is a gap between the end of the annular blade 140 on the suction port 43 side and the end of the running space 110, so that a suction passage is formed between the...
Embodiment 2
[0053] Fig. 5 is a transverse sectional view of Embodiment 2 of the compression device of the rotary vane compressor of the present invention;
[0054] As shown in Figure 5, same as Embodiment 1, the compression device of the rotary vane compressor of the present invention forms an operating space 110 closed on one side through a sealing member 110a, and at one end of the operating space 110 and The other end is respectively provided with a side suction 43 and inner and outer exhaust ports 44, 44a.
[0055] There is a gap between the end of the annular blade 140 on the suction port 43 side and the end of the running space 110, so that a suction passage is formed between the end of the annular blade 140 and the end of the running space 110 120 ; the end of the annular vane 140 on the side of the exhaust port forms a seal between the inner and outer compression chambers A2 and B2 under the action of the airtight mechanism 130 .
[0056] One side of the arc-shaped slider 132 of ...
Embodiment 3
[0058] Fig. 6 is a transverse sectional view of Embodiment 3 of the compression device of the rotary vane compressor of the present invention.
[0059] As shown in Figure 6, same as Embodiment 1, the compression device of the rotary vane compressor of the present invention forms an operating space 110 closed on one side through a sealing member 110a, and at one end of the operating space 110 and The other end is respectively provided with a side suction port 43 and inner and outer exhaust ports 44, 44a.
[0060] There is a gap between the end of the annular blade 140 on the suction port 43 side and the end of the running space 110, so that a suction passage is formed between the end of the annular blade 140 and the end of the running space 110 120 ; the end of the annular vane 140 on the side of the exhaust port forms a seal between the inner and outer compression chambers A2 and B2 under the action of the airtight mechanism 130 .
[0061] One side of the arc-shaped slider 13...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 