Fairings for power generation machines

Patent metadata

Field	Value
Publication number	US-11527228-B2
Application number	US-201916266411-A
Country	US
Kind code	B2
Filing date	Feb 4, 2019
Priority date	Feb 21, 2018
Publication date	Dec 13, 2022
Grant date	Dec 13, 2022

Abstract

A fairing for a power generation machine, the fairing comprising: a first layer comprising a metallic material; a second layer comprising a composite; and a third layer positioned between the first layer and the second layer, the third layer being configured to attenuate acoustic waves over a predetermined frequency range.

First claim

We claim:

1. A fairing for a power generation machine, the fairing comprising:
a first layer comprising a metallic material and defining a first surface and an opposite second surface, the first layer being configured for coupling the fairing to the power generation machine via one or more fasteners, wherein the first surface of the first layer has a concave shape, and wherein the first layer defines one or more receptacles open to the power generation machine;
a second layer comprising a composite material, wherein the second layer defines a first surface and a second opposite surface, the second surface of the second layer defining an external surface of the fairing, the second surface of the second layer having a convex shape; and
a third layer positioned within the one or more receptacles, the third layer being configured to attenuate acoustic waves over a predetermined frequency range.

2. A fairing as claimed in claim 1 , wherein the second layer defines a plurality of apertures and the third layer defines a plurality of cavities, the plurality of apertures and cavities are aligned and define a plurality of Helmholtz resonators.

3. A fairing as claimed in claim 2 , wherein the third layer comprises a honeycomb structure.

4. A fairing as claimed in claim 1 , wherein the third layer comprises a wire mesh arranged to form a plurality of loops, wherein the wire is selected to attenuate the acoustic waves over the predetermined frequency range by converting acoustic energy to thermal energy.

5. A fairing as claimed in claim 1 , wherein the third layer is bonded to the first layer.

6. A fairing as claimed in claim 1 , wherein the first surface of the first layer comprises a portion that is shaped to match a surface of the power generation machine, the portion for being adhered to the power generation machine.

7. A fairing as claimed in claim 1 , wherein the second layer defines a first surface and a second opposite surface, the second surface of the second layer defining an external surface of the fairing.

8. A fairing as claimed in claim 1 , wherein the first layer is configured to enable the fairing to comply with ISO2685:1998.

9. A fairing as claimed in claim 1 , wherein the second layer comprises no protrusions extending from the second surface of the second layer to minimize excrescence drag.

10. A fairing as claimed in claim 1 , wherein the metallic material of the first layer comprises aluminium or titanium.

11. A fairing as claimed in claim 1 , wherein the composite material of the second layer comprises a carbon composite or an oxide ceramic matrix composite.

12. Apparatus comprising: a power generation machine; and a fairing as claimed in claim 1 , the first layer of the fairing being coupled to the power generation machine.

13. Apparatus as claimed in claim 12 , wherein the power generation machine is a gas turbine engine.

14. Apparatus as claimed in claim 12 , wherein the power generation machine is an electrical machine.

Assignees

• Rolls Royce Plc

Inventors

• Peace Richard
• Taylor-Tibbott Oliver C
• Marshall John G

Classifications

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• G10K11/168 Primary

  Plural layers of different materials, e.g. sandwiches · CPC title

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F02K1/827

  Sound absorbing structures or liners · CPC title