IP Library Granted Patent US 6,971,860
Granted Patent B2
US 6,971,860 · App. 10/428,524 · Granted Dec 6, 2005

Compressor unit housing

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Quick Facts
Patent No.
US 6,971,860
App. No.
10/428,524
Granted
Dec 6, 2005
Kind
B2
Abstract

A hermetic compressor unit housing comprised of a shell having a top section and a bottom section which receives the top section, the shell being formed of sheet metal and having generally cylindrical sidewalls wherein the sidewall taken in a generally axial direction is substantially straight, each shell section having an opening, a substantially cylindrical portion, and a closed end portion, the opening having a substantially circular horizontal cross-sectional geometry defined by a major axis and a minor axis, the horizontal cross-sectional geometry including substantially liner opposing sidewall portions preferably disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis, and methods of aligning the shell sections for installation of fixtures and mating of the shell sections.

Claims (13)

1. A compressor housing having a substantially cylindrical shape with substantially straight sidewalls, the compressor housing comprising an upper section and a lower section, each section comprising an opening, a sidewall, and a closed end portion, the opening of each section having a substantially circular horizontal cross-sectional geometry defined by a major axis and a minor axis, the horizontal cross-sectional geometry having a pair of substantially linear opposing portions, the pair being disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis, the pair of substantially linear opposing sections being disposed substantially perpendicular to the minor axis, the pair of substantially linear opposing sections extending from the opening through the sidewall and into at least part of the closed end portion of each housing section.

2. The compressor housing of claim 1 wherein the substantially circular horizontal cross-section geometry further includes substantially linear opposing sidewall portions disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis.

3. The compressor housing of claim 1 , wherein the cross-sectional length of each substantially linear opposing sidewall portion is from about 0.250 inches to about 3.0 inches.

4. The compressor housing of claim 1 wherein the length ratio of the major axis to the minor axis is from greater than 1.0 to about 1.6.

5. The compressor housing of claim 1 wherein the shell sections are comprised of low carbon steel, with sidewall thickness ranging from about 0.090 to about 0.160 inches.

6. The compressor housing of claim 1 wherein the upper shell section is generally cylindrical and is outwardly curved.

7. The compressor housing of claim 1 wherein the lower shell section is generally cylindrical and is outwardly curved.

8. A shell section for a compressor the shell section comprising an opening, a sidewall, and a closed end portion, the opening of each section having a substantially circular horizontal cross-section geometry defined by a major axis and a minor axis, the horizontal cross-section geometry having a pair of substantially linear opposing portions, the pair being disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis, the pair of substantially linear opposing sections being disposed substantially perpendicular to the minor axis, the pair of substantially linear opposing sections extending from the opening through the sidewall and into at least part of the closed end portion.

9. The shell section of claim 8 , wherein the cross-sectional length of each substantially linear opposing sidewall portion is from about 0.250 inches to about 3.0 inches.

10. The shell section of claim 8 , wherein the length ratio of the major axis to the minor axis is from greater than 1.0 to about 1.6.

11. The shell section of claim 8 , wherein the shell sections is comprised of low carbon steel, with sidewall thickness ranging from about 0.090 to about 0.160 inches.

12. The shell section of claim 8 , wherein the shell section is an upper shell section which is generally cylindrical and is outwardly curved.

13. The shell section of claim 8 , wherein the shell section is a lower shell section which is generally cylindrical and is outwardly curved.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 18, 2018
From: BRISTOL COMPRESSORS INTERNATIONAL, LLC
To: KULTHORN KIRBY PUBLIC COMPANY LIMITED
Reel/Frame 047951/0281 →
CHANGE OF NAME Recorded Mar 29, 2016
From: BRISTOL COMPRESSORS INTERNATIONAL, INC.
To: BRISTOL COMPRESSORS INTERNATIONAL, LLC
Reel/Frame 038278/0232 →