Impeller and rotary machine provided with same

Patent metadata

Field	Value
Publication number	US-2016195094-A1
Application number	US-201414912416-A
Country	US
Kind code	A1
Filing date	Sep 16, 2014
Priority date	Oct 9, 2013
Publication date	Jul 7, 2016
Grant date	—

Abstract

The impeller is provided with a disk that rotates about an axis line, and a plurality of blades provided at intervals around the circumference of the disk. Defining the blade angle of the tip of each blade as a first blade angle, the tip has a constant-tip-angle area in which the first blade angle is constant from an inlet where fluid flows in toward an outlet side, and an increasing-tip-angle area that is continuous with the outlet side of the constant-tip-angle area and that has a gradually increasing first blade angle towards the outlet.

First claim

1 .- 10 . (canceled)

11 . An impeller comprising:
a disk which rotates about an axis line; and a plurality of blades which are provided at intervals in a circumferential direction at the disk and rotate integrally with the disk, thereby guiding a fluid which flows inward from an axis line direction in which the axis line extends, toward the outside in a radial direction with respect to the axis line, wherein among angles that a tangential line in a projection curve obtained by projecting a center curve of a thickness of the blade from the axis line direction to the disk makes with an imaginary straight line orthogonal to a straight line which connects a tangential point between the projection curve and the tangential line and the axis line, an angle which is formed on a rear side in a rotation direction of the disk and an outer periphery side of the disk is defined as a blade angle, and in a case where the blade angle of a tip of the blade is defined as a first blade angle, the tip has a constant-tip-angle area in which the first blade angle is constant from an inlet where the fluid flows in, toward an outlet side where the fluid flows out, and an increasing-tip-angle area which is continuous with the outlet side of the constant-tip-angle area and in which the first blade angle gradually increases towards the outlet, and the first blade angle is the largest at the outlet.

12 . The impeller according to claim 11 , wherein in the increasing-tip-angle area,
a first angle area which is continuous with the outlet side of the constant-tip-angle area, and a second angle area which is continuous with the outlet side of the first angle area through an inflection point and in which a mean gradient that is a rate of change of the blade angle is smaller than that in the first angle area, are formed.

13 . The impeller according to claim 12 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the hub has an increasing-hub-angle area in which the second blade angle gradually increases toward the outlet side from the inlet, and a decreasing-hub-angle area which is continuous with the outlet side of the increasing-hub-angle area through a local maximum point at which the second blade angle becomes the maximum, and in which the second blade angle gradually decreases towards the outlet.

14 . The impeller according to claim 13 , wherein the increasing-hub-angle area is formed such that a mean gradient, which is a rate of change of the blade angle, is larger than that in the increasing-tip-angle area.

15 . The impeller according to claim 14 , wherein the local maximum point is formed further toward the inlet side than the inflection point.

16 . The impeller according to claim 11 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the hub has an increasing-hub-angle area in which the second blade angle gradually increases toward the outlet side from the inlet, and a decreasing-hub-angle area which is continuous with the outlet side of the increasing-hub-angle area through a local maximum point at which the second blade angle becomes the maximum, and in which the second blade angle gradually decreases towards the outlet.

17 . The impeller according to claim 11 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

18 . The impeller according to claim 11 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

19 . The impeller according to claim 11 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the first blade angle is formed to be less than or equal to the second blade angle over an area from the inlet to the outlet.

20 . A rotary machine comprising: the impeller according to claim 11 .

21 . The impeller according to claim 12 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

22 . The impeller according to claim 13 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

23 . The impeller according to claim 14 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

24 . The impeller according to claim 15 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

25 . The impeller according to claim 16 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the inlet of the blade is formed to be larger than the first blade angle in the inlet of the blade.

26 . The impeller according to claim 12 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

27 . The impeller according to claim 13 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

28 . The impeller according to claim 14 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

29 . The impeller according to claim 15 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

30 . The impeller according to claim 16 , wherein in a case where the blade angle of a hub of the blade is defined as a second blade angle,
the second blade angle in the outlet of the blade and the first blade angle in the outlet of the blade are formed to be the same.

Assignees

• Mitsubishi Heavy Ind Ltd
• Mitsubishi Heavy Ind Compressor Corp

Inventors

• Yamashita Shuichi

Classifications

• F04D29/284

  for compressors · CPC title

• F05D2240/301

  Cross-sectional characteristics · CPC title

• F04D17/10 Primary

  for compressing or evacuating · CPC title

• F04D17/122

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

• F04D29/30 Primary

  Vanes · CPC title