IP Library Granted Patent US 9,316,115
Granted Patent B2
US 9,316,115 · App. 12/578,268 · Granted Apr 19, 2016

Turboengine wash system

Inventor: Hubert E. Sales (Houston, TX)
Assignee: EcoServices, LLC
F01D25/002B08B3/02B08B9/00
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,316,115
App. No.
12/578,268
Granted
Apr 19, 2016
Kind
B2
Abstract

A system for cleaning gas turbine engines is described. More specifically, methods and apparatuses for cleaning stationary gas turbines and on-wing turbofan engines found on aircraft are disclosed that includes a trailer-mounted, automated low-pressure water delivery system, additive and detergent injection system, nozzle and manifold technology, and active waste water effluent collector system. The system will deliver the liquid cleaning medium at a specific pressure, temperature and flow rate to optimize the atomization that occurs at the nozzles.

Claims (31)

1. A method for turbine engine cleaning with an engine cleaning apparatus, the method comprising the steps of:

pressurizing an aqueous wash medium with an automated, low-pressure water delivery system operating from 200 psi to 725 psi;

incorporating additives and/or detergents into the wash medium; and

delivering the wash medium into the engine with a plurality of nozzles, wherein said nozzles are arranged on a manifold array, with each nozzle having its own unique characteristics as to droplet size, flowrate, and dispersion spray pattern different from the characteristics of the other nozzles to deliver the wash medium uniquely from each of the plurality of nozzles, wherein at least one nozzle is directed towards the engine core to direct spray toward air flow path through the engine and at least one nozzle is directed toward blades in the engine to directly impinge on pressure and suction side of blades.

2. The method of claim 1 further comprising the step of:

providing a portable power generator that will power the engine cleaning apparatus.

3. The method of claim 1 further comprising the step of:

purging the wash medium from the engine cleaning apparatus.

4. The method of claim 1 further comprising the step of:

controlling the engine cleaning apparatus.

5. The method of claim 1 further comprising the step of:

collecting the aqueous wash medium after said medium transverses the engine through suction of the engine exhaust airflow.

6. The method of claim 5 , further comprising the step of:

treating the collected aqueous wash medium after said medium has been collected.

7. The method of claim 1 , and further comprising the step of:

heating the wash medium prior to delivering the wash medium into the engine.

8. The method of claim 1 , and further comprising the step of:

collecting the wash medium with a collection device comprising an air mist separator adapted to separate liquids and solids from air and positioned such that an airstream exiting the engine contacts the collection device and the collection device separates liquid and solids entrained in the airstream from air.

9. The method of claim 8 , and further comprising the step of:

collecting liquid that contacts the collection device into a reservoir.

10. The method of claim 1 , and further comprising the step of:

placing a trough under the engine so that the trough collects wash medium that drips from the engine.

11. A method for turbine engine cleaning with an engine cleaning apparatus, the method comprising the steps of:

pressurizing an aqueous wash medium with an automated, low-pressure water delivery system operating from 200 psi to 700;

incorporating additives and/or detergents into the wash medium; and

delivering the wash medium into the engine with a plurality of nozzles, wherein said nozzles are arranged on a manifold array, with each nozzle having its own unique characteristics as to droplet size, flowrate, and dispersion spray pattern different from the characteristics of the other nozzles.

12. A method for turbine engine cleaning with an engine cleaning apparatus, the method comprising the steps of:

pressurizing an aqueous wash medium with an automated, low-pressure water delivery system operating from 200 psi to 725 psi;

incorporating additives and/or detergents into the wash medium; and

delivering the wash medium into the engine with a plurality of nozzles, wherein said nozzles are arranged on a manifold array, with each nozzle having its own unique characteristics as to droplet size, flowrate, and dispersion spray pattern different from the characteristics of the other nozzles to deliver the wash medium uniquely from each of the plurality of nozzles; and

controlling the pressure, flow rate, temperature and dispersion from the nozzles and the duration of the wash using a feed-back automation system.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE NAME OF THE 2ND ASSIGNOR PREVIOUSLY RECORDED AT REEL: 025859 FRAME: 0110. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Oct 5, 2017
From: GAS TURBINE EFFICIENCY AB; GAS TURBINE EFFICIENCY SWEDEN AB
To: PRATT & WHITNEY LINE MAINTENANCE SERVICES, INC.
Reel/Frame 044167/0036 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 23, 2015
From: SALES, HUBERT E., JR.
To: GAS TURBINE EFFICIENCY SWEDEN AB
Reel/Frame 037118/0690 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 18, 2013
From: PRATT & WHITNEY LINE MAINTENANCE SERVICES, INC.
To: ECOSERVICES, LLC
Reel/Frame 030238/0298 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 23, 2011
From: GAS TURBINE EFFICIENCY AB; GAS TURBINE EFFICIENCY SWEDEN AS
To: PRATT & WHITNEY LINE MAINTENANCE SERVICES, INC.
Reel/Frame 025859/0110 →
Continuity (3)
Division 11644784 · Dec 22, 2006
Continuation In Part 10536002
Related Publication 20100031977A1 · Feb 11, 2010