Inlet connecting piece for an axial-flow compressor
View Patent ↗An inlet connection piece for an axial compressor, particularly for a turbocompressor, includes an inlet housing ( 1 ) in which is arranged a bearing housing ( 2 ) with a bearing ( 3 ), particularly a radial and/or axial bearing, for a rotor. The bearing housing ( 2 ) is connected to the inlet housing ( 1 ) by an inlet strut ( 4 ) which is connected to the inlet housing in a front cross section. The center of the bearing ( 3 ) is arranged axially in the flow direction of a fluid to be compressed behind the area center of the front cross section by at least 0.1-times, particularly at least 0.15-times, particularly at least 0.2-times, particularly at least 0.25-times, the chord length of the front cross section. In addition or alternatively, a fluid passage ( 5, 6 ) is formed in the inlet strut ( 4 ), and at least portions of this fluid passage ( 5, 6 ) form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.
1. An inlet connection piece for an axial compressor comprising:
an inlet housing ( 1 );
a bearing housing ( 2 ) disposed in said inlet housing ( 1 ), both said bearing housing and said inlet housing defining a main fluid passage for a main fluid flow to be compressed in a fluid flow direction;
an axial hydrodynamic bearing ( 3 ) for a rotor of the axial compressor, said bearing disposed in said bearing housing in a flow direction of the fluid to be compressed, said bearing having a center ( 3 a ) and being the first bearing in said fluid flow direction;
at least one inlet strut ( 4 ) formed as a single body, non-rotatably connected to said inlet housing ( 1 ) in a front cross-section having a center and a chord length; said inlet strut directly connecting said bearing housing ( 2 ) to said inlet housing ( 1 ) in the main fluid passage; and wherein
(a) said center ( 3 a ) of said bearing ( 3 ) in the flow direction is arranged axially within said cord length of said inlet strut and behind said center of said front cross-section by one of at least 0.1-times, at least 0.15-times, at least 0.2-times or at least 0.25-times said chord length of said front section of said inlet strut; and
(b) said at least one inlet strut ( 4 ) comprising at least one fluid passage ( 5 , 6 ) defined in and extending through said single body inlet strut, at least a portion of said fluid passage forming an acute angle with a normal plane relative to a longitudinal axis of said inlet connection piece.
2. The inlet connection piece according to claim 1 , wherein said bearing housing ( 2 ) is connected to said inlet housing ( 1 ) by a plurality of inlet struts ( 4 ).
3. The inlet connection piece according to claim 1 , wherein said bearing housing ( 2 ) is connected to said inlet housing ( 1 ) by three or more evenly or unevenly distributed inlet struts.
4. The inlet connection piece according to claim 1 , comprising a plurality of fluid passages ( 5 . 1 , 5 . 2 , 5 . 3 ; 6 . 1 , 6 . 2 ) in said at least one inlet strut ( 4 ).
5. The inlet connection piece according to claim 2 , wherein a plurality of fluid passages ( 6 . 1 , 6 . 2 ) is formed in a first inlet strut ( 4 ) and a different quantity of fluid passages ( 5 . 1 , 5 . 2 , 5 . 3 ) is formed in a second inlet strut ( 4 ).
6. The inlet connection piece according to claim 1 , wherein said at least one fluid passage ( 5 ) extends substantially in a straight line so that said fluid passage forms the same acute angle with a normal plane relative to a longitudinal axis of the inlet connection piece.
7. The inlet connection piece according to claim 6 , wherein the angle formed by said fluid passage ( 5 ) extending substantially in a straight line with a normal plane relative to the longitudinal axis of the inlet connection piece is in the range of 10° to 40°.
8. The inlet connection piece according to claim 1 , wherein said at least one fluid passage ( 6 ) has a bent shape so that at least a portion ( 8 ) of said fluid passage forms an acute angle with a normal plane relative to the longitudinal axis of said inlet connection piece.
9. The inlet connection piece according to claim 8 , wherein said angle formed by said portion ( 8 ) of said fluid passage ( 6 ) with a bent shape with a normal plane relative to the longitudinal axis of the inlet connection piece is in the range of 60° to 80°.
10. The inlet connection piece according to claim 1 , additionally comprising a common portion ( 8 ) communicating with the interior of the bearing housing ( 2 ), and wherein at least two fluid passages ( 6 . 1 , 6 . 2 ) open into said common portion ( 8 ).
11. The inlet connection piece according to claim 1 , additionally comprising a fluid passage formed for one of supplying and removing lubricant to or from said bearing ( 3 ).
12. The inlet connection piece according to claim 1 , wherein said fluid passage ( 5 , 6 ) opens into said bearing housing ( 2 ) in said bearing ( 3 ).
13. The inlet connection piece according to claim 1 , wherein said at least one inlet strut has an area center and a radial axis and wherein at least portions of said radial axis through said area centers of said at least one inlet strut form an acute angle with a normal plane relative to the longitudinal axis of the inlet connection piece.
14. The inlet connection piece according to claim 6 , wherein said angle formed by said fluid passage ( 5 ) extending substantially in a straight line with a normal plane relative to the longitudinal axis of the inlet connection piece is in the range of 20° to 30°.
15. The inlet connection piece according to claim 8 , wherein said angle formed by said portion ( 8 ) of said fluid passage ( 6 ) with a bent shape with a normal plane relative to the longitudinal axis of the inlet connection piece is in the range of 65° to 75°.
16. The inlet connection piece according to claim 1 , wherein said fluid passage ( 5 , 6 ) opens into said bearing housing ( 2 ) in the vicinity of said bearing ( 3 ).
17. An axial compressor comprising an inlet connection piece comprising:
an inlet housing ( 1 );
a bearing housing ( 2 ) disposed in said inlet housing ( 1 ), both said bearing housing and said inlet housing defining a main fluid passage for a main fluid flow to be compressed in a fluid flow direction;
an axial bearing ( 3 ) for a rotor of the axial compressor, said bearing disposed in said bearing housing in a flow direction of the fluid to be compressed, said bearing having a center ( 3 a ) and being the first bearing in said fluid flow direction;
at least one inlet strut ( 4 ) formed as a single body, non-rotatably connected to said inlet housing ( 1 ) in a front cross-section having a center and a chord length; said inlet strut directly connecting said bearing housing ( 2 ) to said inlet housing ( 1 ) in the main fluid passage; and wherein
(a) said center ( 3 a ) of said bearing ( 3 ) in the flow direction is arranged axially within said cord length of said inlet strut and behind said center of said front cross-section by one of at least 0.1-times, at least 0.15-times, at least 0.2-times and at least 0.25-times said chord length of said front section of said inlet strut; and
(b) said at least one inlet strut ( 4 ) comprising within said at least one fluid passage ( 5 , 6 ) defined in and extending through said single body inlet strut, at least a portion of said fluid passage forming an acute angle with a normal plane relative to a longitudinal axis of the inlet connection piece.