IP Library Granted Patent US 7,516,607
Granted Patent B2
US 7,516,607 · App. 11/311,835 · Granted Apr 14, 2009

Method and apparatus for mixing substances

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Quick Facts
Patent No.
US 7,516,607
App. No.
11/311,835
Granted
Apr 14, 2009
Kind
B2
Abstract

A combustor assembly for a gas powered turbine includes a premix section to mix a first selected volume of fuel with a selected oxidizer. The premix section includes an injector plate that includes a porosity according to selected characteristics, such as pore size, pore density, pore distribution, and other selected characteristics. Therefore, the fuel may be provided through the porous plate to the premix area in a selected uniform flux.

Claims (16)

1. A system for allowing a substantially even flux of a fuel into a combustor for a power plant, comprising:

a mixing area operable to allow mixing of a selected volume of fuel and a selected volume of an oxidizer;

an injection plate having a plurality of fibers and pores between the plurality of fibers to provide a selected flux of fuel to the mixing area, wherein the plurality of fibers are steel; and

a fuel supply to supply the selected volume of fuel to an upstream side of the injection plate, a selected pressure on the upstream side enabling the fuel to be urged through said plurality of pores into said mixing area.

2. A system for allowing a substantially even flux of a fuel into a combustor for a power plant, comprising:

a mixing area operable to allow of a selected volume of fuel and a selected volume of an oxidizer;

an injection plate having a plurality of fibers and pores between the plurality of fibers to provide a selected flux of fuel to the mixing area, wherein the plurality of fibers includes first fibers of a first material and second fibers of a second, different material; and

a fuel supply to supply the selected volume of fuel to an upstream side of the injection plate, a selected pressure on the upstream side enabling the fuel to be urged through said plurality of pores into said mixing area.

3. A system for allowing a substantially even flux of a fuel into a combustor for a power plant, comprising:

a mixing area operable to allow mixing of a selected volume of fuel and a selected volume of an oxidizer;

an injection plate having a plurality of fibers and pores between the plurality of fibers to provide a selected flux of fuel to the mixing area, wherein the plurality of fibers includes a first fiber layer and a second fiber layer that each include first fibers having a unidirectional orientation and second fibers that are unidirectionally oriented about 90°relative to the first fibers, and the first fibers and the second fibers of the second fiber layer are transversely oriented relative to the respective first fibers and second fibers of the first fiber layer; and

a fuel supply to supply the selected volume of fuel to an upstream side of the injection plate, a selected pressure on the upstream side enabling the fuel to be urged through said plurality of pores into said mixing area.

4. A system for allowing a substantially even flux of a fuel into a combustor for a power plant, comprising:

a mixing area operable to allow mixing of a selected volume of fuel and a selected volume of an oxidizer;

an injection plate having a plurality of fibers and pores between the plurality of fibers to provide a selected flux of fuel to the mixing area, wherein the plurality of fibers include a first fibers and second fibers that are sinter-bonded to the first fibers; and

a fuel supply to supply the selected volume of fuel to an upstream side of the injection plate, a selected pressure on the upstream side enabling the fuel to be urged through said plurality of pores into said mixing area.

Assignments (5)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0109 →
LICENSE Recorded Aug 5, 2016
From: UNITED TECHNOLOGIES CORPORATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION, SUCCESSOR OF RPW ACQUISITION LLC)
Reel/Frame 039595/0315 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Jun 17, 2016
From: AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 039197/0125 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 10, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 030774/0529 →