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US4547131A Expired / Lapsed US ⏱️ 0.0 years remaining

Refrigeration compressor and method of assembling same

Assignee: Copeland Corp LLC
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Filing: 1983-07-25
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Granted: 1985-10-15
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Expires: 2003-07-25
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Abstract

Abstract A method of assembling a hermetic refrigeration motor compressor is disclosed wherein the motor stator is assembled in a first shell section, the compressor is assembled in another shell section and the two shell sections are aligned and secured together in such a manner as to insure a uniform air gap between the rotor and stator. The method employed enables the two shell sections to be initially locked in position before complete welding of the periphery so as to avoid potential heat distortion.

Inventors

  • 👤 Delmar R. Riffe
  • 👤 John P. Elson
  • 👤 Dilip S. Sathe
  • 👤 Walter T. Grassbaugh

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 04:37
CPC Classifications
F; F04; F04B; F04B39/00; F04B39/0027; F04B39/0055; F04B35/00; F04B35/04; F04B39/0072; F04B39/12; F04B39/127; Y; Y10; Y10S; Y10S417/00; Y10S417/902; Y10T; Y10T29/00; Y10T29/49; Y10T29/49229; Y10T29/49236; Y10T29/49826; Y10T29/49895

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 164 words
A hermetic refrigeration compressor comprising: a first shell section; a compressor assembly including a compressor housing fixedly supported within said first shell section, said compressor housing including a rotatable drive shaft extending outwardly from one end of said first shell section; and a second shell section; an electric driving motor assembly including a stator fixedly supported within said second shell section, said stator having a rotor receiving bore extending therethrough and a rotor supported on said drive shaft within said bore; said first and second shell sections being radially positioned with respect to each other whereby said rotor is coaxially positioned within said bore to thereby provide a uniform air gap between said rotor and said stator said sections being welded together in said position, said weld being the sole means for preventing relative radial movement between said compressor housing fixedly supported in said first shell section and said stator fixedly supported in said second shell section and hence maintaining said uniform air gap.
Claim 2
Dependent Claim 164 words
A hermetic refrigeration compressor comprising: a first shell section; a compressor assembly including a compressor housing fixedly supported within said first shell section, said compressor housing including a rotatable drive shaft extending outwardly from one end of said first shell section; and a second shell section; an electric driving motor assembly including a stator fixedly supported within said second shell section, said stator having a rotor receiving bore extending therethrough and a rotor supported on said drive shaft within said bore; said first and second shell sections being radially positioned with respect to each other whereby said rotor is coaxially positioned within said bore to thereby provide a uniform air gap between said rotor and said stator said sections being welded together in said position, said weld being the sole means for preventing relative radial movement between said compressor housing fixedly supported in said first shell section and said stator fixedly supported in said second shell section and hence maintaining said uniform air gap.
Claim 3
Dependent Claim 32 words
A hermetic refrigeration compressor as set forth in claim 1 wherein said first and second shells each include a generally radially outwardly extending annular flange portion, said flange portions being welded together.
Claim 4
Dependent Claim 38 words
A hermetic refrigeration compressor as set forth in claim 2 wherein said flange portions define a slight gap therebetween around a portion of the periphery, said welding filling said gap so as to sealingly secure said flanges together.
Claim 5
Independent Claim 99 words
A method of assembling a hermetic refrigeration compressor comprising: positioning a first shell section containing a compressor in aligned end to end relationship with a second shell section containing a stator; aligning radially said first shell section with respect to said second shell section whereby a rotor receiving crankshaft is positioned in coaxial relationship within a rotor receiving bore of said stator; and thereafter welding said ends of said first and second shell sections together to lock said crankshaft receiving rotor in said coaxial postion whereby a uniform air gap will be provided between the rotor and said stator.
Claim 6
Independent Claim 99 words
A method of assembling a hermetic refrigeration compressor comprising: positioning a first shell section containing a compressor in aligned end to end relationship with a second shell section containing a stator; aligning radially said first shell section with respect to said second shell section whereby a rotor receiving crankshaft is positioned in coaxial relationship within a rotor receiving bore of said stator; and thereafter welding said ends of said first and second shell sections together to lock said crankshaft receiving rotor in said coaxial postion whereby a uniform air gap will be provided between the rotor and said stator.
Claim 7
Dependent Claim 29 words
A method as set forth in claim 4 wherein said aligning may create slight gaps along peripheral portions of said ends, said welding being operative to fill said gaps.
Claim 8
Dependent Claim 47 words
A method as set forth in claim 4 further comprising forming radially outwardly extending flanges on said one ends of said first and second shell sections, said flanges being operative to inhibit distortion of said shell sections resulting from heating during welding of said shell sections together.
Claim 9
Independent Claim 192 words
A method of assembling a hermetic motor compressor wherein said motor compressor includes a compressor assembly fixedly secured within a first shell section and a stator fixedly secured within a second shell section, said method comprising: placing said second shell section on a mandrel having a portion extending into a rotor receiving bore in said stator; placing one end of said first shell section in axially aligned relationship with one end of said second shell section, said first shell section having a crankshaft extending outwardly from said one end and being received within a bore in said mandrel, said mandrel being operative to effect a radial shifting of said first shell section to precisely position said crankshaft in coaxial relationship with said stator bore, whereby upon assembly of a motor rotor a uniform air gap will be provided around the periphery thereof; and tack welding said ends of said first and second shell sections together at a plurality of locations to lock said shell sections together with said crankshaft in aligned coaxial relationship with respect to said bore; and thereafter welding the periphery of said shell to seal said one ends together.
Claim 10
Independent Claim 192 words
A method of assembling a hermetic motor compressor wherein said motor compressor includes a compressor assembly fixedly secured within a first shell section and a stator fixedly secured within a second shell section, said method comprising: placing said second shell section on a mandrel having a portion extending into a rotor receiving bore in said stator; placing one end of said first shell section in axially aligned relationship with one end of said second shell section, said first shell section having a crankshaft extending outwardly from said one end and being received within a bore in said mandrel, said mandrel being operative to effect a radial shifting of said first shell section to precisely position said crankshaft in coaxial relationship with said stator bore, whereby upon assembly of a motor rotor a uniform air gap will be provided around the periphery thereof; and tack welding said ends of said first and second shell sections together at a plurality of locations to lock said shell sections together with said crankshaft in aligned coaxial relationship with respect to said bore; and thereafter welding the periphery of said shell to seal said one ends together.
Claim 11
Dependent Claim 47 words
A method as set forth in claim 7 further comprising forming radially outwardly extending flanges on said one ends of said first and second shell sections, said flanges being operative to inhibit distortion of said shell sections resulting from heating during welding of said shell sections together.
Claim 12
Dependent Claim 34 words
A method as set forth in claim 8 wherein shell sections are positioned with said flanges abutting each other at at least one peripheral location when said crankshaft is axially aligned with said bore.
Claim 13
Dependent Claim 24 words
A method as set forth in claim 7 wherein said ends are tack welded at dimetrically opposite sides of said one ends substantially simultaneously.
Claim 14
Dependent Claim 35 words
A method as set forth in claim 10 wherein said first and second shell sections are further tack welded on diametrically opposite sides, said further tack welds being spaced approximately 90° from said tack welds.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-10-14 1989-04-15 1989-10-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-10-14 1993-04-15 1993-10-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-10-14 1997-04-15 1997-10-15 $7700.00 Window Closed / Lapsed

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