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US3861820A Expired / Lapsed US ⏱️ 0.0 years remaining

Centrifugal gas compressor unit

Assignee: Ingersoll Rand Co
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Filing: 1974-02-22
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Granted: 1975-01-21
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Expires: 1994-02-22
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Abstract

Abstract A multi-housing compressor having a plurality of gas compressing stages in each of parallel housings, the housings being integral with and extending perpendicularly from a gear housing. Rotor assemblies and associated diffusors are slidably replaceable from the respective housings, obviating any requirement to dismantle the gear housings. While the housings each receive gas, sequentially, for further compression, impellers and shafts in a plurality of the compressor housings are of identical weight, with the impellers thereof of identical axial length albeit of differing diameters.

Inventors

  • 👤 Hanns Hornschuch

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 14:49
CPC Classifications
F; F16; F16H; F16H57/00; F16H57/0018; F16H57/0025; F04; F04D; F04D25/00; F04D25/16; F04D25/163; F04D29/00; F04D29/26; F04D29/266; F04D29/28; F04D29/284; F04D29/286; F16D; F16D1/00; F16D1/06; F16D1/08; F16D1/0817; F16H37/00; F16H57/04; F16H2700/00; F16H2700/02; Y; Y10; Y10T; Y10T403/00; Y10T403/70; Y10T403/7098

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 303 words
A centrifugal gas compressor unit, comprising: a plurality of separate, gas compressor housings; a plurality of successive gas compressing stages within each of said housings; means for admitting gas to a first of said housings; means for discharging compressed gas from a last of said housings; means for communicating gas between each of said housings for successive gas compression; said stages each comprising a bladed gas compressor impeller and vaned diffusor; a shaft confined within each of said housings rotatably supporting said impellers; and bearing means interposed between each of said shafts and housings for supporting said shafts for rotation; wherein at least one of said impeller shafts is substantially circular in cross-section, having a central locus and at least one portion on The circumferential surface thereof which is eccentric, defining of said circumferential surface a first segment located a first radial distance from said locus, and a second segment located a second radial distance from said locus: at least one of said impellers of said one shaft has a substantially circular shaft mounting hole formed therein, said mounting hole having a radial center and at least one portion on the circumferential surface of said mounting hole which is eccentric, defining of said latter circumferential surface a first arcuate portion located a first radial distance from said center; and a second arcuate portion located a second radial distance from said center; and said shaft circumferential surface and said impeller mounting hole dimensionally define a mutual, slidable engagement and interface, upon one of said first and second segments being disposed in common, radial alignment and juxtaposition with one of said first and second arcuate portions, and define a torqued, interference fit, upon a portion of said second segment being disposed in common, radial alignment and juxtaposition with a portion of said first arcuate portion.
Claim 2
Dependent Claim 303 words
A centrifugal gas compressor unit, comprising: a plurality of separate, gas compressor housings; a plurality of successive gas compressing stages within each of said housings; means for admitting gas to a first of said housings; means for discharging compressed gas from a last of said housings; means for communicating gas between each of said housings for successive gas compression; said stages each comprising a bladed gas compressor impeller and vaned diffusor; a shaft confined within each of said housings rotatably supporting said impellers; and bearing means interposed between each of said shafts and housings for supporting said shafts for rotation; wherein at least one of said impeller shafts is substantially circular in cross-section, having a central locus and at least one portion on The circumferential surface thereof which is eccentric, defining of said circumferential surface a first segment located a first radial distance from said locus, and a second segment located a second radial distance from said locus: at least one of said impellers of said one shaft has a substantially circular shaft mounting hole formed therein, said mounting hole having a radial center and at least one portion on the circumferential surface of said mounting hole which is eccentric, defining of said latter circumferential surface a first arcuate portion located a first radial distance from said center; and a second arcuate portion located a second radial distance from said center; and said shaft circumferential surface and said impeller mounting hole dimensionally define a mutual, slidable engagement and interface, upon one of said first and second segments being disposed in common, radial alignment and juxtaposition with one of said first and second arcuate portions, and define a torqued, interference fit, upon a portion of said second segment being disposed in common, radial alignment and juxtaposition with a portion of said first arcuate portion.
Claim 3
Dependent Claim 78 words
A gas compressor unit, according to claim 1, wherein: said at least one impeller shaft, in cross-section, is of plural lobe shape defining a plurality of eccentric portions on the circumferential shaft surface; said shaft mounting hole of said one impeller is of plural lobe shape defining a plurality of eccentric portions on the circumferential hole surface; and said lobes lie intermediate said eccentric portions formed on each of said shaft and impeller mounting hole and circumferential surfaces.
Claim 4
Dependent Claim 32 words
A gas compressor unit, according to claim 2, wherein: said lobes of said shaft and impeller, respectively, are torqued into an interference fit with said eccentric portions of said impeller and shaft.

References Cited (Backward Citations)

US2854926A Cited
US2893769A Cited
US2969250A Cited
US3053118A Cited
US3355096A Cited
US3424372A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-01-20 1978-07-22 1979-01-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-01-20 1982-07-22 1983-01-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-01-20 1986-07-22 1987-01-21 $7700.00 Window Closed / Lapsed

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