System fault detection in electrostatic flow diagnostics

• US 4,587,614 A
• Filed: 12/28/1982
• Issued: 05/06/1986
• Est. Priority Date: 12/28/1982
• 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: Couch, Robert P.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US06/453,965
• Time in Patent Office: 1,225 Days
• Field of Search: 364/431.01, 364/431.02, 364/424, 364/487, 364/507-608, 324/80, 324/464, 73/35, 73/116, 73/660, 371/20, 371/28
• US Class Current: 701/100
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles

Abstract

Diagnostic apparatus which analyzes the waveforms (FIGS. 57-80) of signals provided by electrostatic probes (1, 2, 3) is declared to have a system fault in the event that signals appear on two out of three probes simultaneously. In one embodiment (FIG. 14) the sample number of the digital value which crosses threshold is compared between two adjacent probes. In another embodiment (FIGS. 15-18) default is declared if the signals appear in an approximate time slot (T=1, T=2, T=3).

Claims

1. Electrostatic diagnostic apparatus for distinctly recognizing different events occurring in an operating gas turbine engine, comprising:

a plurality of electrostatic signal means, each including a probe to be disposed in the gas stream of an engine, for providing, when said probe is disposed in the gas stream of an operating engine, a probe signal having amplitude variations indicative of the magnitude of electrostatic charge flowing in the gas stream in the vicinity of said probe, said probes being disposed along the gas stream of said engine spaced apart from one another, whereby electrostatic charge in the gas stream of the engine first flows past a first one of said probes and then flows past a second one of said probes within a range of time thereafter; and

signal processing means connected for response to each of said electrostatic signal means, for providing a system fault signal indicative of failure of said diagnostic apparatus in response to said first and second probes each providing a probe signal in excess of a threshold magnitude in a timed relationship other than within said range of time.

2. Electrostatic diagnostic apparatus for distinctly recognizing different events occurring in an operating gas turbine engine, comprising:

a plurality of electrostatic signal means, each including a probe to be disposed in the gas stream of an engine, for providing, when said probe is disposed in the gas stream of an operating engine, a probe signal having amplitude variations indicative of the magnitude of electrostatic charge flowing in the gas stream in the vicinity of said probe, said probes being spaced apart from one another along the gas stream of said engine, whereby the gas stream of the engine flows past said probes sequentially;

signal processing means connected for respose to each of said electrostatic signal means, for providing a particular engine event identifying signal selected from among a plurality of engine event identifying signals in response to said amplitude variations having characteristics correlated to an engine event corresponding to said particular identifying signal, and for providing a system fault signal indicative of failure of said diagnostic apparatus in response to two of said probes providing a probe signal in excess of a threshold magnitude substantially simultaneously.