Centrifugal compressor with extended operating range
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F25B-049/02
F04D-027/00
F04D-029/44
F04D-027/02
F25B-001/053
F25B-001/10
출원번호
US-0096395
(2013-12-04)
등록번호
US-9157446
(2015-10-13)
발명자
/ 주소
Brasz, Joost
Rasmussen, Mogens
출원인 / 주소
DANFOSS A/S
대리인 / 주소
Carlson, Gaskey & Olds, P.C.
인용정보
피인용 횟수 :
1인용 특허 :
24
초록▼
This disclosure relates to a centrifugal compressor. In a first example, the compressor includes a first impeller provided in a main refrigerant flow path, a second impeller provided in the main refrigerant flow path downstream of the first impeller, and a recirculation flow path. In the first examp
This disclosure relates to a centrifugal compressor. In a first example, the compressor includes a first impeller provided in a main refrigerant flow path, a second impeller provided in the main refrigerant flow path downstream of the first impeller, and a recirculation flow path. In the first example, the recirculation flow path is provided between a first location and a second location along the main refrigerant flow path. The first location is downstream of the second location, and the second location is downstream of the first impeller. In a second example, the compressor includes an impeller provided in a main refrigerant flow path, and a recirculation flow path provided between a first location and a second location along the main refrigerant flow path. In the second example, the recirculation flow path includes a recirculation volute. Further disclosed is a method for operating a centrifugal compressor.
대표청구항▼
1. A centrifugal compressor, comprising: a first impeller provided in a main refrigerant flow path;a second impeller provided in the main refrigerant flow path downstream of the first impeller;a recirculation flow path provided between a first location and a second location along the main refrigeran
1. A centrifugal compressor, comprising: a first impeller provided in a main refrigerant flow path;a second impeller provided in the main refrigerant flow path downstream of the first impeller;a recirculation flow path provided between a first location and a second location along the main refrigerant flow path, the first location being downstream of the second impeller, the second location being downstream of the first impeller;a first vaned diffuser downstream of the first impeller, the second location adjacent the first vaned diffuser, the first vaned diffuser including a plurality of vanes having leading edges;a plurality of recirculation nozzles provided in the recirculation flow path, each of the recirculation nozzles having an outlet arranged adjacent the first vaned diffuser and downstream of the first impeller, wherein the outlets of the recirculation nozzles are arranged at least partially radially outward of the leading edges of the vanes of the first vaned diffuser with respect to a radial distance measured in a radial direction which is perpendicular to a central axis of said impeller; andwherein the recirculation flow path includes a recirculation volute adjacent inlets of the recirculation nozzles, the recirculation volute being upstream, relative to the recirculation flow path, of the recirculation nozzles. 2. The compressor as recited in claim 1, wherein the compressor includes an outlet volute downstream of the second impeller, the first location adjacent the outlet volute. 3. The compressor as recited in claim 1, including an injection plate, the recirculation nozzles formed in the injection plate. 4. The compressor as recited in claim 1, further including: a controller; anda flow regulator provided in the recirculation flow path, the flow regulator selectively regulating a flow of refrigerant within the recirculation flow path in response to instructions from the controller. 5. The compressor as recited in claim 4, wherein the controller provides instructions to the flow regulator in response to a compressor operating capacity. 6. The compressor as recited in claim 1, wherein second location is upstream of the second impeller. 7. The compressor as recited in claim 1, wherein at least a portion of the recirculation flow path is external to a compressor housing. 8. The compressor as recited in claim 7, wherein the recirculation flow path has no deswirl vanes. 9. The compressor as recited in claim 1, wherein the flow regulator includes an actuator and a mechanical valve. 10. The compressor as recited in claim 1, wherein the recirculation volute spirals around an axis of rotation of the first impeller. 11. The compressor as recited in claim 1, wherein a semi-vaneless space is provided between adjacent vanes of the first vaned diffuser, and wherein the outlets of the recirculation nozzles including a semi-vaneless portion radially aligned with the semi-vaneless space and a vaneless portion radially aligned with a space upstream of the semi-vaneless space. 12. The compressor as recited in claim 11, wherein the semi-vaneless space is bounded by (1) an arc about an axis of rotation of the first and second impellers, the arc having a radius equivalent to a radial distance between the axis of rotation and the leading edges of the vanes of the first vaned diffuser, (2) a throat between the adjacent vanes, and (3) a radially inner surface of one of the adjacent vanes. 13. The compressor as recited in claim 1, wherein the outlets of the recirculation nozzles are arranged partially radially outward of the leading edges of the vanes of the first vaned diffuser and partially radially inward of the leading edges of the vanes of the first vaned diffuser. 14. A centrifugal compressor, comprising: an impeller provided in a main refrigerant flow path;an outlet volute downstream of the impeller;a recirculation flow path provided between a first location and a second location along the main refrigerant flow path, the recirculation flow path including a recirculation volute, the recirculation volute being upstream relative to the recirculation flow path, of the second location;a vaned diffuser downstream of the impeller, the second location adjacent the vaned diffuser and downstream of the impeller, the vaned diffuser including a plurality of vanes having leading edges; anda plurality of recirculation nozzles provided in the recirculation flow path, wherein each of the recirculation nozzles has an outlet arranged at least partially radially outward of the leading edges of the vanes of the vaned diffuser with respect to a radial distance measured in a radial direction which is perpendicular to a rotation axis of said impeller. 15. The compressor as recited in claim 14, wherein the second location is upstream, relative to the main refrigerant flow path, of the first location. 16. The compressor as recited in claim 14, wherein the outlets of the recirculation nozzles are arranged partially radially outward of the leading edges of the vanes of the vaned diffuser and partially radially inward of the leading edges of the vanes of the vaned diffuser. 17. A method of operating a centrifugal compressor, comprising: establishing a first flow of refrigerant along a main refrigerant flow path; pressurizing the first flow of refrigerant with a first impeller;selectively introducing a second flow of refrigerant into the main refrigerant flow path at a location downstream of the first impeller, the second flow of refrigerant sourced from the main refrigerant flow path, the second flow of refrigerant flowing through a recirculation volute before being introduced into the main refrigerant flow path;pressurizing the combined first and second flows of refrigerant with a second impeller; andwherein the second flow of refrigerant is sourced from the main refrigerant flow path at a location downstream of the second impeller, and is introduced into the main refrigerant flow path via a plurality of recirculation nozzles, the recirculation nozzles arranged such that at least a portion of an outlet of each recirculation nozzle is radially outward of a leading edge of a vane of a vaned diffuser with respect to a radial distance measured in a radial direction which is perpendicular to a rotation axis of said impeller.
Sommer, Steven Trent; Trevino, Jr., John; Iancu, Florin; Chervil, Rudy; Smyder, Eric John, Compressor control system using a variable geometry diffuser.
Slovisky, John A.; Barton, Michael T.; Gunaraj, John A.; Mansour, Mahmoud L.; Palmer, Donald L.; Paine, Charles J.; Perrone, George L.; Nolcheff, Nick A., Compressor including an aerodynamically variable diffuser.
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