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US4170489A Expired / Lapsed US ⏱️ 0.0 years remaining

Process for cleaning jet engine nozzles

Assignee: Teledyne Inc
•
Filing: 1978-07-24
•
Granted: 1979-10-09
•
Expires: 1998-07-24
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Abstract

Abstract A process is provided for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine. The process involves dispensing a detergent and water solution under sufficient pressure through the fuel nozzles themselves to scrub residue fuel varnish and carbon from the fuel nozzles and from the guide vanes of a jet engine of an aircraft; without the need for removing the engine from the aircraft, or for removing the nozzles from the engine. The process serves to wet down the surfaces of the fuel nozzles and guide vanes with a detergent solution for a period of time (that is about 20 minutes), and then to scour the surfaces with a pulsating detergent spray, and finally to purge and dry the surfaces with a pressurized air stream.

Inventors

  • 👤 Harve W. Magnus
  • 👤 Vincent J. Masur

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 13:26
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/002; F02; F02B; F02B77/00; F02B77/04

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 47 words
A process for cleaning the fuel nozzles and guide vanes of jet engines, and the like, which comprises disconnecting the fuel system of the engine from the fuel nozzles; introducing a pressurized stream of cleaning solution into the fuel nozzles to be emitted through the fuel nozzles.
Claim 2
Dependent Claim 47 words
A process for cleaning the fuel nozzles and guide vanes of jet engines, and the like, which comprises disconnecting the fuel system of the engine from the fuel nozzles; introducing a pressurized stream of cleaning solution into the fuel nozzles to be emitted through the fuel nozzles.
Claim 3
Dependent Claim 52 words
The process defined in claim 1, and which includes a first step of initially introducing the cleaning solution at relatively low pressure into the fuel nozzles for wetting purposes, and a second step after a predetermined time interval for subsequently introducing a cleaning solution at relatively high pressure into the fuel nozzles.
Claim 4
Dependent Claim 31 words
The process defined in claim 2, and which includes a step of causing the relatively high pressure stream of cleaning solution to be introduced as intermittent bursts into the fuel nozzles.
Claim 5
Dependent Claim 34 words
The process defined in claim 1, and which includes a step of subsequently introducing an air stream into the fuel nozzles of the engine to be emitted through the fuel nozzles for drying purposes.
Claim 6
Dependent Claim 23 words
The process defined in claim 1, in which the pressurized stream of cleaning solution is introduced to the fuel nozzles as intermittent bursts.
Claim 7
Dependent Claim 34 words
The process defined in claim 5, and which includes the step of subsequently introducing an air stream to the fuel nozzles of the engine to be emitted through the fuel nozzles for drying purposes.

References Cited (Backward Citations)

US1584505A Cited
US2689456A Cited
FR1099311A Cited
US4095418A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-10-08 1983-04-09 1983-10-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-10-08 1987-04-09 1987-10-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-10-08 1991-04-09 1991-10-09 $7700.00 Window Closed / Lapsed

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