A turbo machine according to the present disclosure includes a rotating shaft, an impeller, a first bearing, and a first supply passage. The rotating shaft includes a first taper portion and a first cylindrical portion. The first bearing includes a first taper support surface and a first cylindrical
A turbo machine according to the present disclosure includes a rotating shaft, an impeller, a first bearing, and a first supply passage. The rotating shaft includes a first taper portion and a first cylindrical portion. The first bearing includes a first taper support surface and a first cylindrical portion support surface, the first taper support surface including a first taper hole forming surface and rotatably supporting the first taper portion, the first cylindrical portion support surface rotatably supporting the first cylindrical portion. The first supply passage is open to a space formed between the first cylindrical portion and first cylindrical portion support surface. An inclination angle of the first taper hole forming surface with respect to the axial direction of the first bearing is greater than an inclination angle of an outer surface of the first taper portion with respect to the axial direction of the rotating shaft.
대표청구항▼
1. A turbo machine comprising: a rotating shaft;an impeller;a first bearing that supports the rotating shaft; anda first supply passage for supplying a lubricating liquid between the rotating shaft and the first bearing, whereinthe impeller is fixed to the rotating shaft, a working fluid intake side
1. A turbo machine comprising: a rotating shaft;an impeller;a first bearing that supports the rotating shaft; anda first supply passage for supplying a lubricating liquid between the rotating shaft and the first bearing, whereinthe impeller is fixed to the rotating shaft, a working fluid intake side of the impeller facing the first bearing,the rotating shaft includes a first taper portion and a first cylindrical portion, the first taper portion increasing in diameter toward the impeller in an axial direction of the rotating shaft, the first cylindrical portion being located adjacent to a large diameter end of the first taper portion,the first bearing includes a first taper support surface and a first cylindrical portion support surface, the first taper support surface including a first taper hole forming surface that forms a taper hole that extends toward a small diameter end of the first taper portion from a particular point on the first bearing in an axial direction of the first bearing, the first taper support surface rotatably supporting the first taper portion via the lubricating liquid, the first cylindrical portion support surface rotatably supporting the first cylindrical portion via the lubricating liquid,the first supply passage is open to a space formed between the first cylindrical portion and the first cylindrical portion support surface, andan inclination angle of the first taper hole forming surface with respect to the axial direction of the first bearing is greater than an inclination angle of an outer surface of the first taper portion with respect to the axial direction of the rotating shaft. 2. The turbo machine according to claim 1, wherein an outer surface of the rotating shaft and an inner surface of the first bearing form an extended space at a position adjacent to the large diameter end of the first taper portion, the extended space having a width in the radial direction of the first bearing, the width being greater than a width of a space between an outer surface of the first cylindrical portion and the first cylindrical portion support surface. 3. The turbo machine according to claim 2, wherein the extended space is formed by the inner surface of the first bearing and the outer surface of the first taper portion, the inner surface extending from the first taper hole forming surface outward in the radial direction of the first bearing between the first cylindrical portion support surface and the first taper hole forming surface in the axial direction of the rotating shaft. 4. The turbo machine according to claim 2, wherein the extended space is formed by the first taper hole forming surface and a part of the outer surface of the rotating shaft, the outer surface extending from the first cylindrical portion inward in the radial direction of the rotating shaft. 5. The turbo machine according to claim 1, further comprising: a second bearing that supports the rotating shaft; anda second supply passage for supplying a lubricating liquid between the rotating shaft and the second bearing, whereinthe rotating shaft further includes a second taper portion and a second cylindrical portion, the second taper portion increasing in diameter toward the impeller on a side of the impeller opposite from the first taper portion in the axial direction of the rotating shaft, the second cylindrical portion being located adjacent to a large diameter end of the second taper portion,the second bearing includes a second taper support surface and a second cylindrical portion support surface, the second taper support surface including a second taper hole forming surface that forms a taper hole that extends toward a small diameter end of the second taper portion from a particular point on the second bearing in an axial direction of the second bearing, the second taper support surface rotatably supporting the second taper portion via the lubricating liquid, the second cylindrical portion support surface rotatably supporting the second cylindrical portion via the lubricating liquid,the second supply passage is open to a space formed between the second cylindrical portion and the second cylindrical portion support surface, andan inclination angle of the second taper hole forming surface with respect to the axial direction of the second bearing is greater than an inclination angle of an outer surface of the second taper portion with respect to the axial direction of the rotating shaft.
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이 특허에 인용된 특허 (3)
Sullivan Robert F. (Indianapolis IN), Bleed valve control circuit.
Peter Fledersbacher DE; Gernot Hertweck DE; Siegfried Sumser DE; Juergen Willand DE; Friedrich Wirbeleit DE, Exhaust-gas turbocharger for an internal combustion engine.
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