Airfoil with venturi tube

Patent metadata

Field	Value
Publication number	US-12305530-B2
Application number	US-202418414578-A
Country	US
Kind code	B2
Filing date	Jan 17, 2024
Priority date	Oct 21, 2022
Publication date	May 20, 2025
Grant date	May 20, 2025

Abstract

A method includes forming an airfoil, where the airfoil includes an airfoil wall that has a span between first and second radial ends and defines leading and trailing edges, pressure and suction sides each join the leading and trailing edges, and an internal cavity, the internal cavity is divided into at least first and second sub-cavities that extend over the span, and the first sub-cavity defines a venturi tube. The forming includes i) fabricating a fiber preform of the airfoil around a plurality of mandrels, wherein the mandrel in the first sub-cavity is radially split, and ii) densifying the fiber preform with a ceramic matrix. The airfoil may include an internal cavity that is divided into at least first and second sub-cavities extending over the span, where the first sub-cavity defines a venturi tube.

First claim

What is claimed is:

1. A method comprising:
forming an airfoil, the airfoil including an airfoil wall that has a span between first and second radial ends and defines leading and trailing edges, pressure and suction sides each join the leading and trailing edges, and an internal cavity, the internal cavity is divided into at least first and second sub-cavities that extend over the span, and the first sub-cavity defines a venturi tube,
the forming including i) fabricating a fiber preform of the airfoil around a plurality of mandrels, wherein the mandrel in the first sub-cavity is radially split, and ii) densifying the fiber preform with a ceramic matrix, wherein the venturi tube has a convergent-divergent geometry such that a cross-sectional area of the venturi tube decreases from the first radial end to a location along the span at which the cross-sectional area is at a minimum and the cross-sectional area increases from the location of the minimum to the second radial end, the forming including forming the airfoil wall from ceramic fiber plies that locally build-up a thickness of at least one of the pressure or suction sides of the airfoil wall at the location of the minimum such that the venturi tube tapers in a tangential direction along the span from the first radial end to the location of the minimum and expands in the tangential direction along the span from the location of the minimum to the second radial end.

2. The method as recited in claim 1 , wherein the forming includes using a support shim in the first sub-cavity during densification to prevent collapse of the airfoil wall around the first sub-cavity.

3. The method as recited in claim 1 , wherein the cross-sectional area of the venturi tube is bound by a rib, the trailing edge, and the pressure and suction sides of the airfoil wall.

4. The method as recited in claim 1 , wherein the ceramic fiber plies locally build-up the thickness of both of the pressure and suction sides of the airfoil wall at the location of the minimum.

5. The method as recited in claim 1 , wherein the ceramic fiber plies locally build-up the thickness of only one of the pressure or suction sides of the airfoil wall at the location of the minimum.

Assignees

• Rtx Corp

Inventors

• Banhos Jonas
• Roach James T
• Gao Cheng

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/30

  Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2230/20

  essentially without removing material · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title