Turbine engine debris ingestion monitor

• US 5,070,722 A
• Filed: 09/21/1990
• Issued: 12/10/1991
• Est. Priority Date: 09/21/1990
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Hawman, Michael W., Ritter, Thomas M., Remmers, Timothy M.
• Primary Examiner(s): RAEVIS, ROBERT R
• Application Number:
  US07/586,630
• Time in Patent Office: 445 Days
• Field of Search: 73/23.21, 73/24.03, 73/28.01, 73/28.03, 73/31.04, 73/116, 73/170 R, 340/945, 415/118, 364/424.06
• US Class Current: 73/28.01
• CPC Class Codes: G01N 15/06 Investigating concentration of particle suspensions by weighing G01N5/00; investigating sedimentation of particle suspensions G01N15/04; investigating individual particles G01N15/10
• CPC Class Codes: G01N 29/14 using acoustic emission techniques echo of particles G01N29/046; measuring mechanical vibrations or acoustic waves in solids in general G01H1/00

Abstract

A turbine engine debris ingestion monitor has an acoustic emission sensor 18, 18a mounted on a surface 14, 14a disposed in an air flow stream of a turbine engine 12. The sensor converts acoustic emissions 16, generated by particles of debris 10 impacting on the surface, into an electrical signal. A counting circuit 22 (FIG. 2) processes the signal resulting in an output, indicative of the level of debris ingested into the engine, which is recorded in the aircraft'"'"'s flight data recording system 110.

Claims

1. Apparatus for detecting debris ingested into an air flow stream of a turbine engine during the operation thereof, comprising:

sensor means having a sensor surface disposed in the air flow stream to be struck by the debris for producing a plurality of stress waves indicative of both impact stressed resulting from debris impacts and background stresses resulting from the operation of the engine, and means for converting said stress waves into an analog electrical signal having a plurality of bipolar pulses each indicative of the debris striking said surface;

bandpass filter means receiving said electrical signal and issuing a filtered electrical signal devoid of at least a great proportion of those frequency components of said electrical signal at which the effect of said impact stresses on the amplitude of said electrical signal is indistinguishable from that of said background stresses; and

signal processing means, responsive to said filtered electrical signal for providing an output signal having a plurality of output pulses derived from said bipolar pulses and indicative of a level of debris ingested into the engine.

2. Apparatus according to claim 1 wherein said surface comprises a turbine engine component.

3. Apparatus according to claim 2 wherein said surface comprises a fan strut.

4. Apparatus according to claim 1 wherein said signal processing means comprises:

envelope detector means, responsive to said filtered electrical signal, for providing an envelope signal having a plurality of envelope pulses each indicative of each of said bipolar pulses;

threshold means, responsive to said filtered electrical signal, for providing a threshold signal indicative of stress waves induced by both debris impacts and engine operations;

comparator means, responsive to both envelope signal and said threshold signal, for providing a compared signal having a plurality of compared pluses each indicative of each of said envelope pulses in excess of said threshold signal; and

gate means for providing a periodic gate signal having a plurality of gate pulses, and means for gating said compared signal occurring coincidentally in time with each of said gate pulses for providing said output pulses.

5. Apparatus according to claim 1 further comprising count means, responsive to said output pulses, for providing a cumulative count of said pulses within a fixed time period, said cumulative count having a digital output.

6. Apparatus according to claim 5 further comprising

conversion means, responsive to said digital output, for converting said digital output into an analog output;

and

record means, responsive to said analog output, for recording said analog output.

7. Apparatus according to claim 5 further comprising record means, responsive to said digital output, for recording said digital output.

8. Apparatus according to claim 1 further comprising record means, responsive to said output pulses, for recording said output pulses.