Fluidfoil fence

Patent metadata

Field	Value
Publication number	US-10273807-B2
Application number	US-201514630142-A
Country	US
Kind code	B2
Filing date	Feb 24, 2015
Priority date	Mar 19, 2014
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A fluidfoil comprises a main body and a fence, wherein the fence has different lean angles with respect to the main body at different chordwise positions, and wherein the fence is divided along its chordwise extent into at least two portions, where a first portion nearer a leading edge of the fence has a smaller lean angle than a second portion further from the leading edge, and wherein all portions are either anhedral or dihedral.

First claim

The invention claimed is:

1. A fluidfoil comprising:
a main body; and
a fence having different lean angles with respect to the main body at different chordwise positions, the fence comprising:
a first portion that is nearest a leading edge of the fence;
a second portion that is immediately adjacent the first portion and is spanwise shorter than the first portion; and
a third portion that is immediately adjacent the second portion and on a chordwise side thereof remote from the first portion,

wherein the first portion has the same lean angle as the second portion, and the third portion has a greater lean angle than the first and second portions.

2. A fluidfoil according to claim 1 , wherein the fence is divided along its chordwise extent such that the third portion is divided from the second portion and there is a step-wise discontinuity between the second and third portions.

3. A fluidfoil according to claim 1 , wherein the second and third portions have complimentary ramp regions which meet to smoothly join those portions.

4. A fluidfoil according to claim 1 where the fluidfoil is an open-rotor propeller blade.

5. A gas turbine engine comprising one or more fluidfoils in accordance with claim 1 .

6. A gas turbine engine according to claim 5 where the gas turbine engine is an open rotor engine.

7. A method of managing the flow tip momentum transfer from the pressure side to the suction side along the tip of a fluidfoil comprising use of a fluidfoil according to claim 1 .

8. A fluidfoil comprising:
a main body; and
a fence having different lean angles with respect to the main body at different chordwise positions,
wherein the fence is divided along its chordwise extent into at least two portions, where a first portion nearer a leading edge of the fence has a smaller lean angle than a second portion further from the leading edge, the first and second portions are immediately adjacent and integral with each other, and all portions of the fence are anhedral.

Assignees

• Rolls Royce Plc

Inventors

• Bianchi Stefano

Classifications

• B64C11/18

  Aerodynamic features · CPC title

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• F01D1/26

  traversed by the working-fluid substantially axially · CPC title

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• F04D29/667

  by influencing the flow pattern, e.g. suppression of turbulence · CPC title