Inlet filter for gas turbine engines using disposable surface adhesive

Patent metadata

Field	Value
Publication number	US-10352239-B2
Application number	US-201615267263-A
Country	US
Kind code	B2
Filing date	Sep 16, 2016
Priority date	Sep 16, 2016
Publication date	Jul 16, 2019
Grant date	Jul 16, 2019

Abstract

A method of filtering air entering the intake opening of a gas turbine engine. A straightening tube provides a straight channel for incoming air flow. A flow redirector provides a path for air flow that is at right angles to the channel provided by the straightening tube and that leads to the intake opening of the engine. A filter at the downstream end of the flow redirector has a pair of rollers for unrolling and re-rolling a roll of adhesive tape, with an exposed section of the adhesive tape blocking the downstream end of the flow redirector and capturing particles in the air flow. The rollers are activated as needed to expose fresh sections of tape.

First claim

What is claimed is:

1. A method of filtering air entering the intake opening of a gas turbine engine of an aircraft, comprising:
installing a straightening tube upstream the intake opening, the straightening tube providing a straight channel for incoming air flow;
interposing a flow redirector between a downstream end of the straightening tube and the intake opening, the flow redirector providing a path for air flow that is at right angles to the channel provided by the straightening tube and that leads to the intake opening of the gas turbine engine; wherein the flow redirector has an upstream end for receiving air flow from the straightening tube and a downstream end opposite the receiving end;
installing a filter at the downstream end of the flow redirector, the filter comprising a first roller for storing and unrolling a roll of adhesive tape and a second roller for re-rolling and storing the roll of adhesive tape;
wherein the first roller and the second roller are spaced across the downstream end of the flow redirector, such that an exposed section of tape passing from the first roller to the second roller blocks the downstream end of the flow redirector with the adhesive side of the tape facing the air flow; and
incrementally unrolling the first roller and rolling the second roller such that a fresh exposed section of the adhesive tape blocks the downstream end of the flow redirector; and
moving the filter away from the downstream end of the flow redirector during flight conditions in which particle filtering is not desired.

2. The method of claim 1 , wherein the step of installing a straightening tube is performed such that the straightening tube is downstream a particle separator.

3. The method of claim 1 , further comprising using an optical sensor to determine the extent to which the exposed section of adhesive tape is loaded with particles.

4. The method of claim 1 , wherein the step of incrementally unrolling the first roller and rolling the second roller is adjusted such that a rate of refreshing the fresh section of adhesive tape is determined by an amount of particles in the intake air.

5. The method of claim 1 , further comprising removing a roll of adhesive tape from the second roller, and replacing it with a new roll of adhesive tape on the first roller.

Assignees

• Southwest Res Inst

Inventors

• Brun Klaus
• Delimont Jacob M

Classifications

• F02C7/052 Primary

  with dust-separation devices · CPC title

• F05D2270/804

  Optical devices · CPC title

• F05D2220/329

  in helicopters · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F05D2260/607

  Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title