Compressor inlet adjustment mechanism

Patent metadata

Field	Value
Publication number	US-11525451-B2
Application number	US-201916967484-A
Country	US
Kind code	B2
Filing date	Feb 22, 2019
Priority date	Feb 27, 2018
Publication date	Dec 13, 2022
Grant date	Dec 13, 2022

Abstract

The present invention relates to an adjustment mechanism (100) for variably adjusting the cross-section of a compressor inlet (22) and further relates to a corresponding compressor (20) including such an adjustment mechanism (100). The adjustment mechanism (100) comprises a plurality of rotatable orifice elements (110) and an actuation ring (120). The actuation ring (120) is mechanically coupled to the plurality of orifice elements 110 such that rotation of the actuation ring 120 causes movement of the orifice elements 110. The movement of the orifice elements (110) thereby adjusts the cross-section of a compressor inlet (22). The adjustment mechanism (100) further comprises a plurality of support members (140) which are arranged axially between the plurality of orifice elements (110) and the actuation ring (120). Additionally, the adjustment mechanism (100) comprises a spring (130), more specific a ring-shaped wave spring. The spring (130) is adapted to axially preload the plurality of orifice elements (110) and the actuation ring (120) when being in a mounted state.

First claim

The invention claimed is:

1. An adjustment mechanism ( 100 ) comprising:
a plurality of orifice elements ( 110 ), wherein each of the plurality of orifice element ( 110 ) comprises a plate-shaped body and
a rotatable actuation ring ( 120 ) mechanically coupled to the plurality of orifice elements ( 110 );
characterized by
a plurality of support members ( 140 ), each having a protrusion ( 144 ), a point-like or oval-like contact surface ( 142 ), and a recess ( 146 ), arranged axially between the plurality of orifice elements ( 110 ) and the actuation ring ( 120 ), wherein each of the plurality of support members ( 140 ) is in the shape of a cone, or bump and wherein the plurality of support members ( 140 ) are integrally formed with the actuation ring ( 120 ) and wherein each of the orifice elements ( 110 ) comprises a shaft ( 116 ) adapted to be supported in a compressor housing ( 20 ) and wherein each of the plurality of support members ( 140 ) are designed as protrusions ( 144 ) which extend from the actuation ring ( 120 ) in an axial direction towards the plurality of orifice elements ( 110 ).

2. The adjustment mechanism ( 100 ) of claim 1 , wherein the support members ( 140 ) are configured to axially support the actuation ring ( 120 ) against the plurality of orifice elements ( 110 ).

3. The adjustment mechanism ( 100 ) of claim 1 , wherein the support members ( 140 ) are adapted in size, local arrangement and/or material to minimize friction between the support members ( 140 ) and the plurality of orifice elements ( 110 ).

4. The adjustment mechanism ( 100 ) of claim 1 , wherein the plurality of support members ( 140 ) comprises at least 3 support members ( 140 ).

5. The adjustment mechanism ( 100 ) of claim 4 , wherein the number of support members ( 140 ) equals the number of orifice elements ( 110 ).

6. The adjustment mechanism ( 100 ) of claim 1 , wherein the support members ( 140 ) are distributed equally spaced in a circumferential direction ( 54 ) of the actuation ring ( 120 ).

7. The adjustment mechanism ( 100 ) of claim 1 , wherein the support members ( 140 ) are located close to a radial inner circumference ( 124 ) of the actuation ring ( 120 ).

8. The adjustment mechanism ( 100 ) of claim 1 , wherein the support members ( 140 ) are located close to respective pivot axes ( 114 ) of the orifice elements ( 110 ).

9. A compressor ( 10 ) for a charging device, comprising:
a compressor housing ( 20 ) defining a compressor inlet ( 22 ), and
a compressor wheel ( 30 ) arranged in the compressor housing ( 20 );
characterized by
an adjustment mechanism ( 100 ) according to claim 1 , wherein the adjustment mechanism ( 100 ) is arranged in the compressor inlet ( 22 ).

10. The compressor ( 10 ) of claim 9 , wherein the adjustment mechanism ( 100 ) is axially mounted between the compressor housing ( 20 ) and an inlet cover ( 24 ) of the compressor housing ( 20 ), the inlet cover ( 24 ) being arranged axially opposite of the orifice elements ( 110 ) relative to the actuation ring ( 120 ).

11. An adjustment mechanism ( 100 ) comprising:
a plurality of orifice elements ( 110 ), wherein each of the plurality of orifice element ( 110 ) comprises a plate-shaped body and
a rotatable actuation ring ( 120 ) mechanically coupled to the plurality of orifice elements ( 110 );
characterized by
one or more springs ( 130 ) adapted to axially preload the plurality of orifice elements ( 110 ) and/or the actuation ring ( 120 ) in a mounted state in a compressor housing ( 20 ) and a plurality of support members ( 140 ), each having a protrusion ( 144 ), a point-like or oval-like contact surface ( 142 ), and a recess ( 146 ), arranged axially between the plurality of orifice elements ( 110 ) and the actuation ring ( 120 ), wherein each of the plurality of support members ( 140 ) is in the shape of a cone, or bump and wherein the plurality of support members ( 140 ) are integrally formed with the actuation ring ( 120 ) and wherein each of the orifice elements ( 110 ) comprises a shaft ( 116 ) adapted to be supported in a compressor housing ( 20 ) and wherein each of the plurality of support members ( 140 ) are designed as protrusions ( 144 ) which extend from the actuation ring ( 120 ) in an axial direction towards the plurality of orifice elements ( 110 ).

12. The adjustment mechanism ( 100 ) of claim 11 wherein the plurality of support members ( 140 ) are arranged axially between the plurality of orifice elements ( 110 ) and the actuation ring ( 120 ).

13. The adjustment mechanism ( 100 ) of claim 12 , wherein the support members ( 140 ) are configured to axially support the actuation ring ( 120 ) against the plurality of orifice elements ( 110 ).

14. The adjustment mechanism ( 100 ) of claim 11 , wherein the one or more springs ( 130 ) are arranged axially between the actuation ring ( 120 ) and a surface of a compressor housing ( 20 ) to apply an axial force via the actuation ring ( 120 ) on the plurality of orifice elements ( 110 ).

15. The adjustment mechanism ( 100 ) of claim 11 , wherein said one or more springs ( 130 ) is a ring-shaped wave spring.

16. The adjustment mechanism ( 100 ) of claim 11 wherein the plurality of support members ( 140 ) are arranged axially between the plurality of orifice elements ( 110 ) and the actuation ring ( 120 ) and wherein the one or more springs ( 130 ) are arranged axially between the actuation ring ( 120 ) and a surface of a compressor housing ( 20 ) to apply an axial force via the actuation ring ( 120 ) on the plurality of orifice elements ( 110 ).

Assignees

• Borgwarner Inc

Inventors

• Karstadt Sascha

Classifications

• F04D27/0253 Primary

  by throttling (F04D27/0246 takes precedence) · CPC title

• F02B33/34

  with rotary pumps (with cell-type pressure exchangers or the like F02B33/42) · CPC title

• F04D29/4213

  suction ports · CPC title

• F05D2270/101

  Compressor surge or stall · CPC title

• F04D29/464 Primary

  adjusting flow cross-section, otherwise than by using adjustable stator blades · CPC title