Patent US5297928A successfully refreshed from Google Patents.
US5297928A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Centrifugal compressor
Assignee: Mitsubishi Heavy Industries Ltd
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Filing: 1992-06-15
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Granted: 1994-03-29
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Expires: 2012-06-15
Abstract
Abstract A centrifugal compressor has a plurality of seals arranged at the back of an impeller for sealing the impeller outlet and form an annular space defined at the back of the impeller. The annular space is fed with a cold gas under a higher pressure than that of the air discharged at the impeller outlet. Thus, the back of the impeller is cooled down.
Inventors
- 👤 Koichiro Imakiire
- 👤 Keiichi Shiraishi
- 👤 Masanori Kimura
- 👤 Masayoshi Tagawa
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 10:40
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/58; F04D29/582; F04D29/5846; F04D29/08; F04D29/16; F04D29/161; F04D29/162
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
133 words
A centrifugal compressor comprising: an impeller having an outlet through which gas is discharged; a fixed structure disposed to the back of said impeller in the compressor, the back of said impeller and said fixed structure defining a space therebetween; a labyrinth seal including fins forming a labyrinth of the seal, said seal defining an annular space between respective groups of said fins, and said seal being interposed between the outlet of said impeller and said space; and said fixed structure having a passage extending therethrough and open to the labyrinth of said seal via said annular space defined between respective groups of the fins of said seal, whereby cold gas under a higher pressure than that at the outlet of the impeller can be fed into the annular space through the passage.
Claim 2
Dependent Claim
133 words
A centrifugal compressor comprising: an impeller having an outlet through which gas is discharged; a fixed structure disposed to the back of said impeller in the compressor, the back of said impeller and said fixed structure defining a space therebetween; a labyrinth seal including fins forming a labyrinth of the seal, said seal defining an annular space between respective groups of said fins, and said seal being interposed between the outlet of said impeller and said space; and said fixed structure having a passage extending therethrough and open to the labyrinth of said seal via said annular space defined between respective groups of the fins of said seal, whereby cold gas under a higher pressure than that at the outlet of the impeller can be fed into the annular space through the passage.
Claim 3
Dependent Claim
31 words
A centrifugal compressor as claimed in claim 1, wherein said labyrinth seal is a one-piece member having portions disposed at radially innermost and radially outermost portions of said annular space, respectively.
Claim 4
Independent Claim
70 words
A method of cooling a centrifugal compressor, said method comprising the steps of: sealing the outlet of an impeller of the compressor from a space defined at and delimited by the back of the impeller; and cooling the back of the impeller by feeding cold gas under a pressure higher than that of gas at the outlet of the compressor into the space defined at the back of the impeller.
Claim 5
Independent Claim
70 words
A method of cooling a centrifugal compressor, said method comprising the steps of: sealing the outlet of an impeller of the compressor from a space defined at and delimited by the back of the impeller; and cooling the back of the impeller by feeding cold gas under a pressure higher than that of gas at the outlet of the compressor into the space defined at the back of the impeller.
Claim 6
Dependent Claim
29 words
A method of cooling a centrifugal compressor as claimed in claim 3, wherein the step of cooling comprises feeding cold gas from an engine air cooler into the space.
Claim 7
Dependent Claim
64 words
A method of cooling a centrifugal compressor as claimed in claim 3, wherein the step of sealing comprises interposing a labyrinth seal having a plurality of fins between the outlet of the impeller and the space at the back of the impeller, and the step of cooling comprises feeding cold gas to a location between respective groups of the fins of the labyrinth seal.
Claim 8
Dependent Claim
64 words
A method of cooling a centrifugal compressor as claimed in claim 4, wherein the step of sealing comprises interposing a labyrinth seal having a plurality of fins between the outlet of the impeller and the space at the back of the impeller, and the step of cooling comprises feeding cold gas to a location between respective groups of the fins of the labyrinth seal.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-03-28 | 1997-09-27 | 1998-03-29 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-03-28 | 2001-09-27 | 2002-03-29 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-03-28 | 2005-09-27 | 2006-03-29 | $7700.00 | Window Closed / Lapsed |