Elliptical shaped hermetic compressor shell with offset electrical connector

Abstract

A sealed compressor housing includes a tubular top cover and a tubular lower housing each with an elliptical horizontal cross section that can be snap-fitted together. Major and minor axial centerlines of the top cover and the lower housing respectively coincide with each other. A terminal pin is provided on the lower housing and is disposed axially symmetrical about a centerline of the terminal pin. A portion of the top face on the side of the terminal pin and a front side of the top face are higher than a rear side thereof. A bottom outer surface of the lower housing has a smooth ellipsoid shape. An angle is formed between the centerline of the terminal pin and the major axial centerlines.

Claims

1. A compressor housing, comprising: an upper cover; a lower shell; the upper cover and the lower shell each having a cylindrical shape with an elliptical horizontal cross section, and being engageable with each other at the elliptical horizontal cross sections; the elliptical horizontal cross sections of the upper cover and the lower shell each having a major axial centerline and a minor axial centerline, and the respective major axial centerlines and the respective minor axial centerlines being aligned to coincide with each other when the upper cover and the lower shell are engaged; a cylinder block having a centerline being aligned to coincide with the major axial centerlines of the upper cover and the lower shell when viewed from above the upper cover; and a terminal pin located on the lower shell and symmetrically disposed with respect to a terminal pin bore centerline, first and second welding planes are positioned symmetrically relative to the major axial centerline, wherein a top surface of the upper cover is an asymmetric spherical contraction, a portion of the upper cover on a side of the terminal pin and a front side of the upper cover are higher than a rear side of the upper cover, wherein a bottom surface of the lower shell is a smooth ellipsoidal contraction, wherein the terminal pin bore centerline forms an angle with the major axial centerline, the angle is formed by a clockwise rotation of the terminal pin bore centerline from the elliptical major axial centerline forming an angle in a range of 10° to 45°, and wherein an internal side of a bottom portion of the lower shell is provided with four welding planes for internal support pins that support pump components inside the housing, wherein the first welding plane is among the four welding planes, the first and the second of the welding planes are symmetrically positioned on opposite sides of the elliptical major axial centerline, and the remaining two of the welding planes are spaced apart and positioned on the elliptical major axial centerline, and the four welding planes are positioned with an offset toward a rear portion of the compressor cylinder block.

2. The compressor housing according to claim 1, wherein: welding surfaces are formed on the bottom surface of the lower shell, respectively on a side of the terminal pin and on an opposite side of the terminal pin, configured to weld compressor feet onto the lower shell, the welding surfaces each are curved and have a curvature consistent with that of the lower shell, the welding surfaces are distributed on opposite sides of the terminal pin bore centerline, the welding surfaces are distributed along a periphery of the bottom surface of the lower shell, and are configured to weld a welding end of the respective compressor feet, welding ends of the compressor feet each include a curved welding with two forked interconnections, the curved welding surfaces each upwardly arch and have a curvature consistent with that of the respective welding surfaces of the lower shell, supporting planes are provided at respective ends of the compressor feet opposite to the welding ends, the supporting planes are 3 to 8 mm away from a lowest point on the bottom surface of the lower shell, and a centerline connecting the supporting planes of the compressor feet on opposite sides is aligned to coincide with the terminal pin bore centerline.

3. The compressor housing according to claim 1, wherein at a location above the terminal pin bore, the upper cover and the lower shell are each provided with a positioning plane with an equal width, and the positioning planes make a smooth transition into the compressor housing.

4. The compressor housing according to claim 3, wherein the upper cover is provided with an enhancing groove at a location above the positioning planes, the enhancing groove is sunk below the outer surface of the upper cover into the inside of the upper cover and forms a smooth projection on the interior wall of the upper cover, and the enhancing groove includes a vertically straight strip.

5. The compressor housing according to claim 1, wherein the compressor housing is configured to use in a sealed refrigeration compressor.

6. A compressor housing, comprising: an upper cover; a lower shell; the upper cover and the lower shell each having a cylindrical shape with an elliptical horizontal cross section, and being engageable with each other at the elliptical horizontal cross sections; the elliptical horizontal cross sections of the upper cover and the lower shell each having a major axial centerline and a minor axial centerline, and the respective major axial centerlines and the respective minor axial centerlines being aligned to coincide with each other when the upper cover and the lower shell are engaged; a cylinder block having a centerline being aligned to coincide with the major axial centerlines of the upper cover and the lower shell when viewed from above the upper cover; and a terminal pin located on the lower shell and symmetrically disposed with respect to a terminal pin bore centerline, first and second welding planes are positioned symmetrically relative to the major axial centerline, wherein a top surface of the upper cover is an asymmetric spherical contraction, a portion of the upper cover on a side of the terminal pin and a front side of the upper cover are higher than a rear side of the upper cover, wherein a bottom surface of the lower shell is a smooth ellipsoidal contraction, and wherein the terminal pin bore centerline forms an angle with the major axial centerline, the angle is formed by a clockwise rotation of the terminal pin bore centerline from the elliptical major axial centerline forming an angle in a range of 10° to 45°, and wherein: the lower shell sidewall is provided with first and second lower shell retaining grooves that are symmetrically positioned with respect to the major axial centerlines, the upper cover is provided with a plurality of retaining grooves, wherein a first and a second retaining grooves of the plurality of retaining grooves are symmetrically positioned on opposite sides of the major axial centerlines, a third retaining groove of the plurality of retaining grooves is positioned on the major axial centerline and at a location above a rear portion of the compressor cylinder block, and the plurality of retaining grooves of the upper cover are sunk below an outer surface of the upper cover into an inside of the upper cover and form projections on an interior wall of the upper cover or the lower shell, and the first and second lower shell retaining grooves of the lower shell are sunk into an inside of the lower shell and form projections on an interior wall of the lower shell.

7. The compressor housing according to claim 6, wherein the shape of the retaining grooves is one of circular, oval, and smooth polygonal.

Description

DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a front perspective view of a compressor housing, according to one embodiment.

(2) FIG. 2 is a top perspective view of the compressor housing of FIG. 1.

(3) FIG. 3 is a left side perspective view of the compressor housing of FIG. 1.

(4) FIG. 4 is a top view of a general assembly of the compressor housing of FIG. 1.

(5) FIG. 5 is a side view of FIG. 4 along an axis A.

(6) Features in the drawings include the following: 1—upper cover, 2—lower shell, 3—terminal pin, 4—internal support pin (4), 5—compressor foot (2), 6—compressor cylinder block, 7—compressor cylinder cover, 8—intake muffler chamber, 9—welding plane for internal support pin (4 locations), 10—curved compressor foot welding surface (4 locations), 11—first retaining groove on the lower shell, 12—second retaining groove on the lower shell, 13—first retaining groove on the upper cover, 14—second retaining groove on the upper cover, 15—third retaining groove on the upper cover, 16—lower shell positioning plane, 17—upper cover positioning plane, 18—upper cover groove, 19—rear portion of compressor cylinder block, 20—head portion of compressor cylinder block, 21—elliptical major axial centerline (compressor cylinder block cylinder bore centerline), 22—elliptical minor axial centerline, 23—terminal pin bore centerline.

DETAILED DESCRIPTION

(7) The following, in conjunction with the examples in FIGS. 1-5, provides a detailed description of the embodiments which are to be considered in all respects as illustrative and not limiting.

(8) In reference to FIGS. 1-5, a compressor housing suitable for a sealed refrigeration compressor, for example, a small-sized, sealed refrigeration compressor, is provided. The compressor housing includes an upper cover 1 and a lower shell 2. The upper cover 1 and the lower shell 2 each have a cylindrical shape and can be snap-fitted together. The upper cover 1 and the lower shell 2 each have an elliptical horizontal cross-section. An elliptical major axial centerline of the elliptical horizontal cross-section of the upper cover 1 and that of the lower shell are aligned with each other as a major axial centerline 21. Similarly, an elliptical minor axial centerline of the elliptical horizontal cross-section of the upper cover 1 and that of the lower shell are aligned with each other as a minor axial centerline 22.

(9) A terminal pin 3 is provided on the lower shell 2 and is symmetrically disposed with respect to a terminal pin bore centerline 23. The upper cover 1 has a top surface that is an asymmetric spherical contraction. A portion of the top surface on the side of the terminal pin 3 and a front side portion of the top surface are higher than a rear side portion of the top surface. The lower shell 2 has a bottom surface that is a smooth ellipsoidal contraction.

(10) A compressor cylinder block 6 is positioned along the major axial centerline 21 and attached to the compressor housing via respective cylinder bores at ends thereof. The cylinder bores are disposed around a cylinder bore centerline that is aligned to coincide with the major axial centerline 21. The compressor cylinder block 6 includes a larger end that is a head portion 20, and a smaller end that is a rear portion 19 of the compressor cylinder block 6. A compressor cylinder cover 7 and a muffler chamber 8 are located at the head portion 20 of the compressor cylinder block 6.

(11) The terminal pin bore centerline 23 forms an angle A (10° to 45°) with the major axial centerline 21. This can prevent collision between the compressor cylinder cover 7 and the terminal pins and between the muffler chamber 8 and the terminal pin 3. This structure can eliminate the need to extend the length of the elliptical major axial centerline of the lower shell, thereby reduce the amount of space and cost.

(12) Four welding planes 9 are provided at an internal side of a bottom portion of the lower shell 2. The welding planes 9 are configured to weld internal support pins 4 to the lower shell 2. Two of the welding planes 9 are symmetrically located on opposite sides of the major axial centerline 21. The other two of the welding planes 9 are spaced apart and located along the major axial centerline 21. The welding planes 9 as a whole are positioned with an offset toward the side of the rear portion 19 of the compressor cylinder block 6 to provide a compact configuration. The offset toward the side of the rear portion 19 can allocate a maximum space to accommodate components of the compressor such as, for example, the compressor cylinder cover 7, the muffler chamber 8, etc. The welding planes 9 can support, for example, pump components inside the compressor housing.

(13) Welding surfaces 10 are formed on a bottom portion of the lower shell 2 for welding respective compressor feet 5 to the lower shell 2. The welding surfaces 10 are respectively disposed on the side of the terminal pin 3 and the opposite side. The welding surfaces 10 are curved and have a curvature that is consistent with that of an outer surface of the bottom portion of the lower shell 2. The welding surfaces 10 are positioned on opposite sides of the terminal pin bore centerline 23, with two of the welding surfaces 10 positioned on one side and two of the welding surfaces 10 posited on the opposite side. The welding surfaces 10 are distributed along a periphery of the bottom portion of the lower shell 2 that has a smooth ellipsoidal shape. The welding surfaces 10 can correspondingly weld welding ends of the compressor feet 5 thereon.

(14) The welding ends of the compressor feet 5 each include a curved welding surface with two forked interconnections. The curved welding surfaces each upwardly arch and have a curvature consistent with that of the respective welding surfaces 10 of the lower shell 2. A supporting plane is provided at the opposite end of the respective compressor feet 5, which is about 3 to 8 mm (preferably 5 mm) away from the lowest point on the bottom portion of the lower shell 2. A centerline connecting the supporting planes of the compressor feet 5 on opposite sides of the bottom shell 2 is aligned to coincide with the terminal pin bore centerline 23. In this embodiment, the compressor feet 5 are directly welded onto the welding surfaces 10 that have a curvature consistent with that of the lower shell 2, instead of welding a compressor foot onto an entirely flat surface on the lowest part of a lower shell. This allows the outer surface of the bottom portion of the lower shell 2 to have a smooth ellipsoidal shape instead of a cylindrical shape. Thus the amount of oil injected into the compressor housing can be minimized and the overall height of the compressor can be reduced.

(15) A first retaining groove 11 and a second retaining groove 12 are provided on a side wall of the lower shell 2. The first and second retaining grooves 11 and 12 of the lower shell 2 are symmetrically positioned with respect to the major axial centerline 21, and are configured to prevent excessive left and right movements of a lower portion of a pump.

(16) Three retaining grooves are provided on the upper cover 1, including first, second and third retaining grooves 13, 14 and 15. The second retaining groove 14 and the third retaining groove 15 of the upper cover 1 are symmetrically positioned on opposite sides of the major axial centerline 21 and are positioned above the head portion 20 of the compressor cylinder block 6, so as to limit the left and right movements of the compressor cylinder cover 7. The first retaining groove 13 of the upper cover 1 is positioned on the major axial centerline 21 and at a location above the rear portion 19 of the compressor cylinder block 6, so as to limit the range of front and back movement of the rear portion 19 of the compressor cylinder block 6.

(17) The grooves 11-15 are sunk below the outer surface of the compressor housing into an inside of the housing and form smooth projections on an interior wall of the housing. The grooves 11-15 may be circular, oval, or smooth polygonal.

(18) The housing is used as a sealed housing for a compressor. The major and minor elliptical axial centerlines of the upper cover 1 are respectively aligned to coincide with the respective major and minor elliptical axial centerlines of the lower shell 2. To prevent the upper cover 1 and the lower shell 2 from misplacement when rotated with respect to each other during assembly, positioning planes 16 and 17 are provided as mating surfaces configured to engage the upper cover 1 and the lower shell 2 and to facilitate the mating and positioning of the upper cover 1 and the lower shell 2. The positioning plane 17 with a particular width is provided above a terminal pin bore on the upper cover 1. The positioning plane 16 is provided on the lower shell 2 and has a width matching the width of the positioning plane 17. The positioning planes 16 and 17 each have a smooth transition into their respective cover/shell.

(19) An enhancing groove 18 is provided above the positioning plane 17 of the upper cover 1 to improve the strength of the upper cover 1. The enhancing groove 18 is sunk below the outer surface of the upper cover 1 into the inside of the upper cover 1, and forms a smooth projection on the interior wall of the upper cover 1. The enhancing groove 18 includes a vertically straight strip.

(20) The above disclosure is only intended to illustrate the preferred embodiments of the present invention and is not intended to limit the scope of the present invention. Therefore any equivalent changes made based on the disclosure of the present invention, such as improvements on the process parameters or the apparatus, are still within the protective scope of the present invention.