Atomizer, combustion device including atomizer, and gas turbine plant

Patent metadata

Field	Value
Publication number	US-9970356-B2
Application number	US-201514736785-A
Country	US
Kind code	B2
Filing date	Jun 11, 2015
Priority date	Jun 12, 2014
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

An atomizer of the invention includes a mixing chamber, spray fluid flow passages supplying a spray fluid to the mixing chamber, a spray medium flow passage supplying a spray medium to the mixing chamber, outlet holes spraying a fluid mixture of the spray fluid and the spray medium, and fluid mixture flow passages connecting the mixing chamber and the outlet holes to each other. The fluid mixture flowing through each of the fluid mixture flow passages joins with each other at a joining section and is sprayed from the outlet hole. The mixing chamber includes a middle ejection hole spraying the spray fluid to the mixing chamber. The middle ejection hole is arranged at a joining section of the spray fluid flow passages. The spray fluid flowing through the spray fluid flow passages joins with each other at the joining section and is sprayed from the middle ejection hole.

First claim

What is claimed is:

1. An atomizer, comprising:
a mixing chamber configured to form a fluid mixture that includes a spray fluid as fuel and a spray medium as gas, the gas being configured to atomize the spray fluid;
a pair of spray fluid flow passages configured to supply the spray fluid to the mixing chamber;
a spray medium flow passage configured to supply the spray medium to the mixing chamber; and
one or more outlet holes configured to spray the fluid mixture to the outside; wherein
the mixing chamber includes at least one middle ejection hole configured to spray the spray fluid to the mixing chamber,
the pair of spray fluid flow passages is connected to each other on a downstream side of a flow of the spray fluid,
the at least one middle ejection hole is arranged at a joining section where the pair of spray fluid flow passages is connected to each other,
the spray fluid configured to flow through the pair of spray fluid flow passages is configured to join with each other at the joining section of the pair of spray fluid flow passages, and is configured to be sprayed from the at least one middle ejection hole,
the spray medium is configured to flow along a side partition wall of the mixing chamber and along an axial direction of the atomizer,
the mixing chamber includes a groove that communicates with the at least one middle ejection hole, and
the groove is arranged to extend in a direction perpendicular to a direction along which the pair of spray fluid flow passages is connected to each other.

2. The atomizer according to claim 1 further comprising:
a plurality of the outlet holes.

3. The atomizer according to claim 1 , wherein
the mixing chamber includes one or more outlets of the spray medium flow passage,
the atomizer includes at least one of: i) the at least one middle ejection hole including a plurality of middle ejection holes, and ii) the one or more outlets including a plurality of outlets of the spray medium flow passage, and
when the atomizer includes a plurality of the middle ejection holes, the atomizer includes a plurality of the pair of spray fluid flow passages and each middle ejection hole of the plurality of middle ejection holes is arranged at each joining section where the pair of spray fluid flow passages is connected to each other.

4. The atomizer according to claim 1 , wherein
the mixing chamber includes two outlets of the spray medium flow passage, and
the two outlets of the spray medium flow passage are arranged on opposite sides of the groove in a direction perpendicular to an extending direction of the groove.

5. The atomizer according to claim 1 , wherein
the mixing chamber includes an outlet of the spray medium flow passage, and
the outlet of the spray medium flow passage is configured in an annular shape to surround the at least one middle ejection hole along a wall surface of the mixing chamber extending in an axial direction of the atomizer.

6. The atomizer according to claim 1 , wherein
a cross-section of the mixing chamber perpendicular to an axial direction of the atomizer is configured to decrease in a direction toward downstream of a flow of the fluid mixture.

7. A combustion device, comprising:
an atomizer according to claim 1 , wherein
the atomizer is configured to be supplied with a liquid fuel as the spray fluid and is configured to be supplied with air or steam as the spray medium, and
the atomizer is configured to spray the fluid mixture of the spray fluid and the spray medium.

8. A gas turbine plant, comprising:
a gas turbine combustor configured to combust a liquid fuel;
a fuel tank configured to store the liquid fuel;
a compressor configured to compress air to form combustion air and configured to supply the combustion air to the gas turbine combustor; and
a turbine configured to be driven by a combustion gas, the gas turbine combustor being configured to generate the combustion gas, wherein
the gas turbine combustor is a combustion device including the atomizer according to claim 7 , and
the atomizer is configured to be supplied with the liquid fuel stored in the fuel tank and the atomizer is configured to spray the liquid fuel to the gas turbine combustor.

9. A combustion device, comprising:
an atomizer according to claim 1 , wherein
a liquid fuel and combustion air are configured to be mixed and combusted with the liquid fuel being sprayed from the atomizer,
the atomizer is configured to be supplied with the liquid fuel as the spray fluid and is configured to be supplied with a part of the combustion air as the spray medium, and
the atomizer is configured to spray the fluid mixture of the spray fluid and the spray medium.

10. A gas turbine plant, comprising:
a gas turbine combustor configured to combust a liquid fuel;
a fuel tank configured to store the liquid fuel;
a compressor configured to compress air to form combustion air and configured to supply the combustion air to the gas turbine combustor; and
a turbine configured to be driven by a combustion gas, the gas turbine combustor being configured to generate the combustion gas, wherein
the gas turbine combustor is a combustion device including the atomizer according to claim 9 , and
the atomizer is configured to be supplied with the liquid fuel stored in the fuel tank and the atomizer is configured to spray the liquid fuel to the gas turbine combustor.

Assignees

• Mitsubishi Hitachi Power Sys

Inventors

• Okazaki Hirofumi
• Orii Akihito

Classifications

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title

• F02C3/30

  Adding water, steam or other fluids {for influencing combustion, e.g. to obtain cleaner exhaust gases (F02C7/141, F02C7/30, F01D21/00, F01K21/04, F23D11/10 take precedence)} · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F23D11/102

  in an internal mixing chamber · CPC title

• F23R3/286

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title