Machine vibration monitor and method

• US 4,010,637 A
• Filed: 10/06/1975
• Issued: 03/08/1977
• Est. Priority Date: 10/06/1975
• Status: Expired due to Term

• Current Assignee: Lockheed Aircraft Corporation
• Original Assignee: Lockheed Aircraft Corporation
• Inventors: McInturff, Joe A., Rubel, Herbert J., Harwell, Malcolm J.
• Primary Examiner(s): Gill, James J.
• Application Number:
  US05/620,016
• Time in Patent Office: 519 Days
• Field of Search: 73/71.4, 73/71.2, 73/67.2
• US Class Current: 73/658
• CPC Class Codes: G01H 1/003 of rotating machines G01H1/10 takes precedence
• CPC Class Codes: G01P 15/0891 with indication of predetermined acceleration values G01P15/135 takes precedence

Abstract

An accelerometer senses a machine'"'"'s vibration resulting from unbalance of its internal rotors and outputs an electrical signal which is then conditioned by means of an amplifier and uniform level filter. The resulting output signal has individual vibration (frequency) components which are adjusted to match the machine'"'"'s specified vibration limit extending over each of the rotors'"'"' frequency range to achieve a uniform level. A storage oscilloscope is employed to display the conditioned signal.

By utilizing the uniform level filter a normal operating band for the machine can be specified in terms of oscilloscope divisions regardless of the machine'"'"'s operating frequencies. When a signal exceeds the specified band on the oscilloscope the rotor causing the excessive vibration may then be determined by analyzing the individual components. Utilizing relatively uncomplicated electronics, a limit exceedance warning may also be incorporated.

Claims

1. A monitor to measure the vibrating frequency of a machine caused by the unbalance of its internal rotors vibrating at several frequencies to determine in advance an approach of excessive vibration and an incipient failure of the machine comprising:

an accelerometer transducer connected to said machine to receive the total vibration thereof at all operating speeds and produce a single output signal;

an amplifier and uniform level filter connected to said transducer to receive said output signal and raise it to a predetermined substantially constant level over the entire speed range of said machine, said filter having components selected to simultaneously compensate for both the frequency dependence of said signal and the variable displacement allowables of said rotors; and

an oscilloscope adapted to be connected to said filter to receive and display said constant level signal whereby it may be compared with a pre-established reference level of safe operation of said machine.

2. The monitor of claim 1 wherein said single output signal from said accelerator transducer is proportional to the second derivative of the displacement of each fundamental rotor vibration component of said machine.

3. The monitor of claim 1 including a warning indicator adapted to be connected to said filter and preset for actuation by said output signal when the level thereof exceeds said pre-established level.

4. The monitor of claim 1 including an additional filter, a first connection between said additional filter and said uniform filter, a second normally inoperative connection between said additional filter and said oscilloscope, and a switch operative to disconnect said oscilloscope from said uniform filter and simultaneously render said second connection operative, said additional filter being adapted to separate from said constant level signal the signal corresponding to the vibration of each of said rotors.

5. The monitor of claim 3 wherein said warning device is a light energized by a threshold detector preset by a bias voltage.

6. The monitor of claim 3 further including an additional filter adapted to be connected to said uniform level filter and separate from said constant level signal the signal corresponding to the vibration of each of said rotors, and a selector switch operable to connect in the alternative any one of said oscilloscope, said warning indicator and said additional filter to said uniform level filter.

7. The method of detecting imbalance in the rotor system of a machine while operating, consisting essentially of:

generating an electrical output signal related to the vibration acceleration developed in the machine;

converting said electrical output to an electrical signal whose fundamental frequency components are proportional to each of the machine'"'"'s vibration acceleration components;

first conditioning said electrical signal to cause each frequency component to have approximately the same magnitude;

then conditioning said electrical signal to cause the sum of said frequency components to remain substantialy constant over the speed range of the machine; and

comparing said electrical signal thus conditioned to a predetermined reference level.

8. The method of claim 7 including the additional step of registering the results of the comparison aforesaid.

9. The method of claim 7 including the additional step of generating a warning indication when said conditioned signal exceeds said predetermined reference level.

10. The method of claim 7 including the additional step of separating each of the components comprising said conditioned signal prior to comparing said conditional signal to said predetermined reference level.