Method and device for measuring the number of revolutions in turbo aggregates for motors

• US 5,635,646 A
• Filed: 07/20/1995
• Issued: 06/03/1997
• Est. Priority Date: 01/22/1993
• Status: Expired due to Fees

• Current Assignee: F Wennstrom System AB
• Original Assignee: F Wennstrom System AB
• Inventors: Eriksson, Lennart
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): MILLER, ROSE MARY
• Application Number:
  US08/492,055
• Time in Patent Office: 684 Days
• Field of Search: 73/488, 73/660, 73/659, 73/658, 73/506, 73/518, 324/160, 324/161, 324/163, 324/166, 324/76.23, 324/76.24, 364/565, 364/426.01, 455/296, 455/306, 455/340, 377/19, 377/23, 388/922
• US Class Current: 73/660
• CPC Class Codes: G01P 3/48 by measuring frequency of generated current or voltage in general G01R23/00

Abstract

A method measures the rotational speed of an engine turbocharger. A microphone picks up sound generated by the rotation of the turbocharger and a microphone signal containing signal components is supplied. Low-frequency signal components are filtered out from the microphone signal generated by engine operation including noise from valves, fans and gas flows. An electronic bandpass filter is tuned to the remaining signal component having the highest amplitude in the filtered microphone signal and the frequency of the remaining signal component having the highest amplitude is determined. With a knowledge of the turbocharger geometry, the value of the frequency of the remaining signal component having the highest amplitude is converted to the rotational speed of the turbocharger.

Claims

1. A method for measuring the rotational speed of an engine turbocharger, the method comprising the steps of:

picking up sound generated by rotation of the turbocharger with a microphone and supplying a microphone signal containing signal components;

filtering out low-frequency signal components from the microphone signal generated by engine operation including noise from valves, fans and gas flows;

tuning an electronic bandpass filter to the remaining signal component having the highest amplitude in the filtered microphone signal;

determining the frequency of the remaining signal component having the highest amplitude;

with a knowledge of the turbocharger geometry, converting the value of the frequency of the remaining signal component having the highest amplitude to the rotational speed of the turbocharger;

tuning an electronic tuning fork to the remaining signal component having the highest amplitude;

determining the frequency of the tuning fork; and

,

with a knowledge of the turbocharger geometry, converting the value of tuning fork frequency to the rotational speed of the turbocharger.

2. A device for measuring the rotational speed of an engine turbocharger, the device comprising:

a microphone placed in the proximity of the turbocharger to supply a microphone signal;

a first amplifier connected to said microphone for amplifying said microphone signal;

high-pass filter means for filtering out low-frequency signal components from said microphone signal such as signal components generated by valves, fans and gas flows which are picked up by said microphone as the engine runs;

a bandpass filter connected to a high-pass filter;

tuning circuit means for tuning said bandpass filter to said remaining component having the highest amplitude;

an analog detector connected to said bandpass filter for detecting said amplitude and providing an analog detector output signal;

a frequency converter for converting said output signal into pulses which are fed to said tuning circuit means;

said tuning circuit means including means for counting said pulses;

a second amplifier which, following tuning of said bandpass filter to said remaining component having the highest amplitude, matches said output signal whose pulses are counted in said tuning circuit means; and

,

means for indicating and counting the number of blades on the turbine and determining the rotational speed utilizing knowledge of the geometry of the turbocharger.

3. The device of claim 2, said tuning circuit means comprising a programmable logic unit, a digital/analog converter and a voltage controlled oscillator;

and, said programmable logic unit including means for counting said pulses.

4. The device of claim 3, said means for indicating and counting the number of blades on the turbine being connected to said programable logic unit and comprising:

at least one display;

a power stage connected between said programmable logic unit and said display; and

, a plurality of function keys.

5. The device of claim 4, further comprising an electronic tuning fork, which is programmed into said programable logic unit if the signal from said bandpass filter is of insufficient amplitude or varies excessively.