Turbine engine imminent failure monitor

• US 5,552,711 A
• Filed: 11/10/1994
• Issued: 09/03/1996
• Est. Priority Date: 11/10/1994
• Status: Expired due to Term

• Current Assignee: Thierry Deegan, William Dimarco
• Original Assignee: Thierry Deegan, William Dimarco
• Inventors: DiMarco, William, Deegan, Thierry
• Primary Examiner(s): Wieder, Kenneth A.
• Assistant Examiner(s): BROWN, GLENN WARNER
• Application Number:
  US08/336,929
• Time in Patent Office: 663 Days
• Field of Search: 324/378, 324/459, 324/464, 324/501, 324/555, 73/116, 250/336.1, 415/118, 340/627, 340/628, 340/629, 340/631
• US Class Current: 324/464
• CPC Class Codes: G01M 15/102 by monitoring exhaust gases

Abstract

This invention is a method for determining when combustion cans or turbine blades are failing in gas turbine engines. It measures the specific ions emitted by hot spots of can and blade material when they have failed or are failing. The invention relies on the electromagnetic energy radiated by ions that are created as combustion gas erodes and ionizes the materials in these hot spots. Acceleration by the earth magnetic field and by acoustic and mechanical forces normally present in combustion machinery cause these charged particles to radiate identifiable electromagnetic emissions. The frequency of the radiation, being a function of the charge and mass of the particles, allows free ions in the exhaust stream to be identified. The device operates by measuring the electromagnetic spectrum and relating detected frequencies to the mass of the ions from can liner and blade materials. The device can be used in fixed installations such as power plants, ships and aircraft. It can be coupled to vibration measurement equipment for additional indications of failure.

Claims

1. A method of measuring the imminent failure of an engine which produces an electromagnetic radiation spectrum including electromagnetic radiation from moving ions which form as a result of deteriorating engine components, comprising measuring said electromagnetic radiation, determining the spectrum of said electromagnetic radiation and processing said electromagnetic radiation spectrum to identify the ions which are indicative of the deteriorating engine components.

2. The method of claim 1 including the step of shutting down said engine upon sensing ions from said engine components above a predetermined level.

3. The method of claim 1 wherein said engine is a gas turbine and said engine components include combustion cans, turbine blades and turbine casings.

4. A device for measuring imminent failure of an engine which produces an electromagnetic radiation spectrum including electromagnetic radiation from moving ions which form as a result of deteriorating engine components, comprising means for measuring said electromagnetic radiation to obtain the spectrum thereof and means for processing said electromagnetic radiation spectrum to identify the ions which are indicative of the deteriorating engine components.

5. The device of claim 4 wherein said engine is a gas turbine and said engine components include combustion cans, turbine blades and turbine casings.

6. The device of claim 4 wherein said spectrum is the result of acceleration of the ions by ambient magnetic and hydrodynamic forces.

7. The device of claim 4 wherein the means for measuring said electromagnetic radiation is provided with sensors having directionality so as to reduce the influence of ambient electromagnetic noise arriving at said sensors from directions other than that of said engine emission source.