Fuel cell system and aircraft having an inerting system
US-2024379984-A1 · Nov 14, 2024 · US
US10069154B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10069154-B2 |
| Application number | US-201214237375-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2012 |
| Priority date | Aug 24, 2011 |
| Publication date | Sep 4, 2018 |
| Grant date | Sep 4, 2018 |
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An air feed device (1) for a fuel cell, having a shaft (2); a compressor wheel (4) fastened to one of the ends (5, 20) of the shaft (2), a bearing arrangement (6, 7, 8) arranged in a bearing housing (9) for mounting the shaft (2), and an electric motor (10) for driving the shaft (2), which electric motor is arranged in the bearing housing (9). The shaft (2) has two shaft bearing portions (11, 12) and a magnet portion (13) arranged between the shaft bearing portions (11, 12), forming the rotor of the electric motor (10). The shaft bearing portions (11, 12) and the magnet portion (13) are centered relative to one another by means of a centering arrangement (12A, 13F) which engages on an outer edge (A), the shaft bearing portions (11, 12) and the magnet portion (13) bearing in each case axially against one another.
Opening claim text (preview).
The invention claimed is: 1. An air feed device ( 1 ) for a fuel cell, having a shaft ( 2 ) having first and second ends ( 5 , 20 ); a compressor wheel ( 4 ) arranged in a compressor housing ( 3 ) and fastened to the first end ( 5 ) of the shaft ( 2 ), a bearing arrangement ( 6 , 7 , 8 ) arranged in a bearing housing ( 9 ) for mounting the shaft ( 2 ), and an electric motor ( 10 ) for driving the shaft ( 2 ), said electric motor arranged in the bearing housing ( 9 ), wherein the shaft ( 2 ) is comprised of at at least a first shaft bearing part ( 11 ), a second shaft bearing part ( 12 ), and a shaft magnet part ( 13 ) arranged between the first and second shaft bearing parts ( 11 , 12 ), and forming a rotor of the electric motor ( 10 ), the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) being braced against one another, wherein the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) are centered co-axially relative to one another by way of a circumferential centering arrangement ( 12 A, 13 F), each of the shaft bearing parts ( 11 , 12 ) bearing axially against the shaft magnet part ( 13 ), wherein the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) are braced against one another by way of a tie rod ( 19 ), and wherein the compressor wheel ( 4 ) is connected to the shaft ( 2 ) by a screw connection ( 23 ) that is separate from the tie rod ( 19 ), said screw connection ( 23 ) comprising a threaded pin ( 23 A) having an inner end and an outer end, said threaded pin ( 23 A) extending through the compressor wheel ( 4 ), said inner end screwed into an internal thread of the shaft bearing portion ( 12 ) of the shaft ( 2 ), and a nut ( 23 B), said nut ( 23 B) screwed onto said outer end, said nut ( 23 B) fastening the compressor wheel ( 4 ) to the shaft ( 2 ). 2. The air feed device as claimed in claim 1 , wherein a coil ( 14 ) is provided which forms a stator of the electric motor ( 10 ) and which is arranged around the shaft magnet part ( 13 ) in the bearing housing ( 9 ). 3. The air feed device as claimed in claim 2 , wherein the coil ( 14 ) has first and second axial ends ( 15 , 16 ) and is guided by way of two axial guide elements ( 17 , 18 ), which bear against the first and second axial ends ( 15 , 16 ) of said coil, in the bearing housing ( 9 ). 4. The air feed device as claimed in claim 1 , wherein the bearing arrangement is an air bearing arrangement with a radial air bearing ( 6 , 7 ) arranged on each side of the electric motor ( 10 ) on the shaft bearing part ( 11 , 12 ), and an axial air bearing ( 8 ). 5. The air feed device as claimed in claim 4 , wherein the axial air bearing ( 8 ) is arranged adjacent to the compressor wheel ( 4 ) in the bearing housing ( 9 ). 6. The air feed device as claimed in claim 5 , wherein the axial air bearing ( 8 ) has two axial bearing halves ( 33 , 34 ) which are arranged one on either side of a shaft collar ( 31 ) and which are preloaded by way of a spring pack arrangement ( 35 ) arranged in the bearing housing ( 9 ). 7. The air feed device as claimed in claim 1 , wherein a cooling device ( 24 ) is provided between the bearing housing ( 9 ) and an outer casing ( 25 ) which surrounds said bearing housing. 8. The air feed device as claimed in claim 7 , wherein the cooling device ( 24 ) has flow-guiding elements ( 26 ). 9. The air feed device as claimed in claim 8 , wherein the flow-guiding elements ( 26 ) are in the form of an arrangement of spiral ducts. 10. The air feed device as claimed in claim 8 , wherein the bearing arrangement includes an axial bearing, and wherein the cooling device ( 24 ) has an axial bearing cooling portion ( 27 ) arranged in the bearing housing ( 9 ). 11. The air feed device as claimed in claim 8 , wherein the outer casing ( 25 ) is supported on the bearing housing ( 9 ) via O-rings ( 28 , 29 ). 12. The air feed device as claimed in claim 1 , wherein the compressor housing ( 3 ) has a bladed diffuser ( 30 ). 13. The air feed device as claimed in claim 12 , wherein the diffuser ( 30 ) is provided with a double blading ( 32 ). 14. An air feed device ( 1 ) for a fuel cell, having a shaft ( 2 ) having first and second ends ( 5 , 20 ); a compressor wheel ( 4 ) arranged in a compressor housing ( 3 ) and fastened to the first end ( 5 ) of the shaft ( 2 ), a bearing arrangement ( 6 , 7 , 8 ) arranged in a bearing housing ( 9 ) for mounting the shaft ( 2 ), and an electric motor ( 10 ) for driving the shaft ( 2 ), said electric motor arranged in the bearing housing ( 9 ), wherein the shaft ( 2 ) is comprised of at at least a first shaft bearing part ( 11 ), a second shaft bearing part ( 12 ), and a shaft magnet part ( 13 ), arranged between the first and second shaft bearing parts ( 11 , 12 ), and forms a rotor of the electric motor ( 10 ), the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) being braced against one another, wherein the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) are centered co-axially relative to one another by way of a circumferential centering arrangement ( 12 A, 13 F), each of the shaft bearing parts ( 11 , 12 ) bearing axially against the shaft magnet part ( 13 ), wherein a turbine wheel ( 21 ) having a bore is arranged on the second end ( 20 ) of the shaft ( 2 ), wherein the turbine wheel ( 21 ), the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) are braced against one another by way of a tie rod ( 19 ), wherein a first nut ( 19 C) is provided for the securing the turbine wheel ( 21 ) on the second end ( 20 ) of the shaft ( 2 ) as well as bracing of the shaft bearing parts ( 11 , 12 ) and the shaft magnet part ( 13 ) against one another, and wherein the compressor wheel ( 4 ) is connected to the shaft ( 2 ) by a screw connection ( 23 ) that is separate from the tie rod ( 19 ), said screw connection ( 23 ) comprising a threaded pin ( 23 A) having an inner end and an outer end, said threaded pin ( 23 A) extending through the compressor wheel ( 4 ), said inner end screwed into an internal thread of the shaft bearing portion ( 12 ) of the shaft ( 2 ), and a second nut ( 23 B), said second nut ( 23 B) screwed onto said outer end, said second nut ( 23 B) fastening the compressor wheel ( 4 ) to the shaft ( 2 ). 15. The air feed device as claimed in claim 14 , wherein one of the compressor wheel ( 4 ) and the turbine wheel ( 21 ) is connected to the shaft ( 2 ) by way of a screw connection ( 23 ), and the other of the compressor wheel ( 4 ) and the turbine wheel ( 21 ) is connected to the shaft ( 2 ) via a tie rod ( 19 ) separate from the screw connection ( 23 ). 16. The air feed device as claimed in claim 14 , wherein the turbine wheel ( 21 ) is arranged in a turbine housing which is provided with a variable turbine geometry ( 22 ).
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