Co-rotating compressor with multiple compression mechanisms

Patent metadata

Field	Value
Publication number	US-10215174-B2
Application number	US-201715425374-A
Country	US
Kind code	B2
Filing date	Feb 6, 2017
Priority date	Feb 6, 2017
Publication date	Feb 26, 2019
Grant date	Feb 26, 2019

Abstract

A compressor may include a shell, first and second compression mechanisms, and first and second motor assemblies. The first compression mechanism may include first and second compression members that are rotatable relative to the shell about first and second rotational axes, respectively. The first motor assembly may be disposed within the shell and may include a first rotor attached to the first compression member and surrounding the first and second compression members. The second compression mechanism may include third and fourth compression members that are rotatable relative to the shell about third and fourth rotational axes, respectively. The second motor assembly may be disposed within the shell and may include a second rotor attached to the third compression member and surrounding the third and fourth compression members.

First claim

What is claimed is:

1. A compressor comprising:
a shell;
a first compression mechanism disposed within the shell and including a first compression member that is rotatable relative to the shell about a first rotational axis and a second compression member that is rotatable relative to the shell about a second rotational axis that is parallel to and offset from the first rotational axis;
a first motor assembly disposed within the shell and including a first rotor attached to the first compression member and surrounding the first and second compression members;
a second compression mechanism disposed within the shell and including a third compression member that is rotatable relative to the shell about a third rotational axis and a fourth compression member that is rotatable relative to the shell about a fourth rotational axis that is parallel to and offset from the third rotational axis;
a second motor assembly disposed within the shell and including a second rotor attached to the third compression member and surrounding the third and fourth compression members, wherein the first and second rotors each include a radially extending portion that extends radially outward relative to the first rotational axis and an axially extending portion that extends parallel to the first rotational axis, wherein the axially extending portion of the first rotor engages the first compression member and surrounds the second compression member, and wherein the axially extending portion of the second rotor engages the third compression member and surrounds the fourth compression member;
a first seal engaging the second compression member and the radially extending portion of the first rotor; and
a second seal engaging the fourth compression member and the radially extending portion of the second rotor,
wherein the radially extending portions of the first and second rotors are disposed axially between end plates of the second and fourth compression members.

2. The compressor of claim 1 , wherein the first, second, third and fourth compression members are scroll members each having an end plate and a spiral wrap extending from the end plate.

3. The compressor of claim 1 , wherein the first and third rotational axes are collinear, and wherein the second and fourth rotational axes are collinear.

4. The compressor of claim 1 , wherein the first and second motor assemblies are operable independently of each other, and wherein the first and second rotors are rotatable independently of each other.

5. The compressor of claim 1 , wherein the first compression mechanism receives and further compresses fluid discharged from the second compression mechanism.

6. The compressor of claim 5 , further comprising:
a first bearing housing disposed within the shell and rotatably supporting a first hub of the first compression member;
a second bearing housing disposed within the shell and rotatably supporting a second hub of the second compression member and a fourth hub of the fourth compression member; and
a third bearing housing disposed within the shell and rotatably supporting a third hub of the third compression member.

7. The compressor of claim 6 , wherein the fourth hub of the fourth compression member includes a discharge passage through which fluid compressed by the second compression mechanism flows, wherein the second hub of the second compression member includes an inlet passage that receives fluid from the discharge passage, and wherein the second bearing housing includes an aperture that provides fluid communication between the discharge passage and the inlet passage.

8. The compressor of claim 7 , wherein an end plate of the second compression member includes a radially extending passage in fluid communication with the inlet passage and a pocket defined by spiral wraps of the first and second compression members.

9. The compressor of claim 1 , further comprising:
a first bearing housing disposed within the shell and rotatably supporting a first hub of the first compression member;
a second bearing housing disposed within the shell and rotatably supporting a second hub of the second compression member and a fourth hub of the fourth compression member; and
a third bearing housing disposed within the shell and rotatably supporting a third hub of the third compression member,
wherein the first bearing housing cooperates with the shell to define a first discharge chamber receiving fluid discharged by the first compression mechanism, and wherein the third bearing housing cooperates with the shell to define a second discharge chamber receiving fluid discharged by the second compression mechanism.

10. The compressor of claim 9 , wherein the first and third bearing housings cooperate to define a suction chamber therebetween, and wherein the first and second compression mechanisms receive fluid from the suction chamber at a pressure that is lower than a pressure of the fluid in at least one of the first and second discharge chambers.

11. The compressor of claim 10 , further comprising a discharge conduit extending through the suction chamber and providing fluid communication between the first and second discharge chambers.

12. The compressor of claim 10 , wherein the shell defines a lubricant sump disposed in the second discharge chamber, and wherein the first, second and third bearing housings include lubricant passages in fluid communication with the lubricant sump and providing lubricant to the first, second, third and fourth compression members.

13. A compressor comprising:
a shell;
a first compression mechanism disposed within the shell and including a first compression member that is rotatable relative to the shell about a first rotational axis and a second compression member that is rotatable relative to the shell about a second rotational axis that is parallel to and offset from the first rotational axis;
a first bearing housing fixed relative to the shell and rotatably supporting a first hub of the first compression member;
a second bearing housing fixed relative to the shell and rotatably supporting a second hub of the second compression member;
a first motor assembly disposed between the first and second bearing housings and including a first rotor attached to the first compression member;
a second compression mechanism disposed within the shell and including a third compression member that is rotatable relative to the shell about a third rotational axis and a fourth compression member that is rotatable relative to the shell about a fourth rotational axis that is parallel to and offset from the third rotational axis, the fourth compression member including a fourth hub that is rotatably supported by the second bearing housing;
a third bearing housing fixed relative to the shell and rotatably supporting a third hub of the third compression member; and
a second motor assembly disposed between the second and third bearing housings and including a second rotor attached to the third compression member.

14. The compressor of claim 13 , wherein the first and third rotational axes are collinear, and wherein the second and fourth rotational axes are collinear.

15. The compressor of claim 13 , wherein the first and second motor assemblies are operable independently of each other, and wherein the first and second rotors are rotatable independently of each other.

16. The compressor of claim 13 , wherein the first, second, third and fourth compression members are scroll members each having an end plate and a spiral wrap extending from the end plate.

17. The compressor of claim 13 , wherein the f

Assignees

• Emerson Climate Technologies

Inventors

• Stover Robert C
• Doepker Roy J

Classifications

• F04C29/02

  Lubrication (of machines or engines in general F01M); Lubricant separation (separation in general B01D) · CPC title

• F04C18/02

  of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents · CPC title

• F04C2240/30

  Casings or housings · CPC title

• F04C29/12

  Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet · CPC title

• F04C29/0085

  Prime movers · CPC title