(1) Field of the Invention
The invention relates to a sealing arrangement particularly applied to the scroll type compressor to adjustably avoid leakage in operation.
(2) Description of the Prior Art
In the art, while in cranking up a compressor, a rapid pressure boost is required to prevent the working fluid from possible stroking back. Also, the pressure shall be controlled in a reign so that the accumulated pressure won't be too high to damage the scrolls or the compression elements of the compressor, especially to those with a high compression ratio.
In U.S. Pat. No. 6,059,549, an improved high-low pressure chamber sealing arrangement for a volute compressor is disclosed, in which a single air chamber is formed by coupling a gliding block and scrolls. As the compressor is actuated, the gliding block can be pushed upwardly by the pressure variation in the air chamber and the spring force to support the partition block, such that the fluid in the high-pressure chamber can be inhibited to leak to the low-pressure chamber so as to quickly build up the pressure. However, a clear drawback of such an arrangement is that the force to lift the gliding block is close to zero at time of cranking up the compressor or at times when the compression ratio is too low. Under such situations, the gliding block is quite possible unable to overcome the friction and the weight itself to motion upwardly, and thus leakage or failure of building up the pressure may be expected. To resolve the foregoing problem, additional spring force is required to push the gliding block. On the other hand, when the compression ratio is too high, the resultant force from the gliding block and the spring element may make the gliding block unable to motion downwardly so as to relieve part of the load, and thus the reliability of the compressor is definitely degraded.
In US Pat. Pub. No. 2004/0126246, the difficulty in assembling the combination of the gliding block and the O ring into the receiving chamber makes impossible the mass production of the compressor. Also, in assembling the combination, the O ring is vulnerable to be cut by the chamber and thus may be damaged to induce further leakage which will definitely affect the service life and the reliability of the compressor.
Accordingly, it is an object of the present invention to provide a scroll type compressor with an enhanced sealing arrangement which can avoid leakage, make easy the assembly process in production, and merchandise the compressor.
In the present invention, the scroll type compressor with an enhanced sealing arrangement comprises a housing, a bracket body, a partition block, a pair of scrolls, a gliding block, two sealing rings and a plurality of air chambers. The housing for forming an internal accommodation space to accommodate the bracket body further has an inlet and an outlet. The partition block located above the bracket body in the housing separates the accommodation space into a high-pressure chamber and a low-pressure chamber. The scroll pair located between the partition block and the bracket body includes a fixed scroll and a rotary scroll to mesh the fixed scroll. A circular receiving chamber located on top of the fixed scroll further including a first chamber and a second chamber, where the first chamber located above the second chamber is larger than the second chamber in diameter. The gliding block located at a center portion on top of the fixed scroll further includes a first part and a neighboring second part. The first part also located above the second part is larger than the second part in diameter. Upon such an arrangement, the first part of the gliding block can locate above the first chamber, while the second part locates above the second chamber. By matching the gliding block and the scroll pair, a plurality of air chambers can be formed between the fixed scroll and the rotary scroll. Also, by providing pressure variations in these air chamber, the gliding block can be forced to glide.
The aforesaid sealing rings having U-shape cross sections are installed respectively to peripheral walls of the first part and the second part and located respectively to the first chamber and the second chamber of the receiving chamber. The sealing rings also satisfy the following limitations:
h<H/2, and
θ1,θ2<20°
in which h is the depth of the U-shape cross section, H is the height of the U-shape cross section, and θ1, θ2 are the sidewall inclination angles of the U-shape cross section.
By providing the foregoing design criteria to the sealing rings, the load-regulating apparatus (i.e. the scroll type compressor) can be protected from the leakage.
All these objects are achieved by the scroll type compressor with an enhanced sealing arrangement described below.
The present invention will now be specified with reference to its preferred embodiment illustrated in the drawings, in which:
The invention disclosed herein is directed to a scroll type compressor with an enhanced sealing arrangement. In the following description, numerous details are set forth in order to provide a thorough understanding of the present invention. It will be appreciated by one skilled in the art that variations of these specific details are possible while still achieving the results of the present invention. In other instance, well-known components are not described in detail in order not to unnecessarily obscure the present invention.
Referring now to
A circular receiving chamber 55 located on top of the fixed scroll 51 is included to mount the cylindrical gliding block 40. The receiving chamber 55 further includes a first chamber 56 and a second chamber 57, where the first chamber 56 located above the second chamber 57 is larger than the second chamber 57 in diameter. At the bottom portion of the gliding block 40, a first part 41 and a second part 42 are included, in which the first part 41 located above the second part 42 is larger than the second part 42 in diameter. In the state that the gliding block 40 is installed into the receiving chamber 55, the first part 41 of the gliding block 40 can locate above the first chamber 56, and the second part 42 can locate above the second chamber 57. Upon such an arrangement, a first air chamber 61 is formed between the first part 41 of the gliding block 40 and the first chamber 56, and a second air chamber 62 is formed between the second part 42 of the gliding block 40 and the second chamber 57. Also, it is noted that the first chamber 56 and the second chamber 57 of the receiving chamber 55 are firmed in a unique piece, and the first part 41 and the second part 42 of the gliding block 40 are formed in a single piece.
As shown, peripheral sidewalls of the first part 41 and the second part 42 of the gliding block 40 includes respective grooves 43 for mounting the sealing rings 71 and 72, respectively. Referring also to
h<H/2, and
θ1,θ2<20°
in which h is the depth of the U-shape cross section, H is the height of the U-shape cross section, and θ1, θ2 are the sidewall inclination angles of the U-shape cross section.
By providing the foregoing design criteria to the sealing rings 71 and 72, the air leakage between the gliding block and the receiving chamber 55 can be substantially avoided. Also, air holes 44 at the center of the gliding block 40 can be included to communicate in space with the letting-out hole 53 of the fixed scroll 51.
Referring now to
In the case that the compressor is cranked to a state as shown in
Referring to
Referring to
While the present invention has been particularly shown and described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be without departing from the spirit and scope of the present invention.
Number | Date | Country | Kind |
---|---|---|---|
94143489 A | Dec 2005 | TW | national |
95124426 A | Jul 2006 | TW | national |
Number | Name | Date | Kind |
---|---|---|---|
5540572 | Park et al. | Jul 1996 | A |
6059549 | Tarng et al. | May 2000 | A |
6267565 | Seibel et al. | Jul 2001 | B1 |
6913448 | Liang et al. | Jul 2005 | B2 |
7207787 | Liang et al. | Apr 2007 | B2 |
20040126246 | Liang et al. | Jul 2004 | A1 |
Number | Date | Country |
---|---|---|
04121473 | Apr 1992 | JP |
05141201 | Jun 1993 | JP |
Number | Date | Country | |
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20070134117 A1 | Jun 2007 | US |