US4091656A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Detonation analyzer for piston engine
Assignee: Honeywell International Inc
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Filing: 1977-05-12
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Granted: 1978-05-30
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Expires: 1997-05-12
Abstract
Abstract An analyzer adapted to be mounted in a operable aircraft and including an oscilloscopic display of the detonation characteristics of each cylinder of an internal combustion engine. The signal input to the oscilloscope is derived from vibration sensors attached to the engine spark plugs. The synchronizing signal input to the oscilloscope is derived from pulses generated at the primary circuit of the engine magneto. Solid state electronic circuits are used throughout and switching provides the capability to separately study the characteristics of each cylinder.
Inventors
- 👤 Arthur L. Altemose, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 09:14
CPC Classifications
G; G01; G01L; G01L23/00; G01L23/22; G01L23/221; G01L23/225
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
338 words
Apparatus for analyzing the detonation vibrations within each cylinder of an internal combustion engine having a rotating crankshaft, pistons connected thereto and spark plugs energized by a magneto for cyclically igniting the air-fuel mixture within each of said cylinders, said apparatus comprising: a multiplicity of vibration sensors, one of said sensors being in contact with each cylinder of the engine being analyzed, each of said sensors providing an output signal that is an electronic replica of the vibrations going on within said cylinder; a switch for selectively sampling the output of one of said multiplicity of vibration sensors; first electronic circuitry means connected to the output of said switch means, said electronic circuitry means serving to amplify and filter the signal from the selected vibration sensor whereby the frequency band associated with the detonation phenomenon are amplified more than other frequencies; an oscilloscope having a visual display and including a signal input terminal and a synchronizing pulse input terminal, said signal input terminal being supplied by the output from said first electronic circuit means; and second electronic circuitry means for generating a wave train of synchronizing pulses for injection into the synchronizing pulse input terminal of said oscilloscope, said second electronic circuitry means including: a pulse generator connected to the output of said magneto and providing a conditioned output pulse each time said magneto ignites an engine cylinder, a stepping counter having as many outputs as there are cylinders in the engine, said counter receiving conditioned pulses from said pulse generator at the engine firing rate, a timing source producing a reset pulse in coincidence with the attainment of top-dead-center by the piston of number one cylinder of said engine, said reset pulse being used to return said stepping counter to its initial state, and a switch for selecting one of the outputs of said stepping counter, said selection being for the purpose of obtaining a synchronizing pulse input for said oscilloscope, said synchronizing pulses being coincident with the passing of ignition pulses to the cylinder spark plugs.
Claim 2
Dependent Claim
338 words
Apparatus for analyzing the detonation vibrations within each cylinder of an internal combustion engine having a rotating crankshaft, pistons connected thereto and spark plugs energized by a magneto for cyclically igniting the air-fuel mixture within each of said cylinders, said apparatus comprising: a multiplicity of vibration sensors, one of said sensors being in contact with each cylinder of the engine being analyzed, each of said sensors providing an output signal that is an electronic replica of the vibrations going on within said cylinder; a switch for selectively sampling the output of one of said multiplicity of vibration sensors; first electronic circuitry means connected to the output of said switch means, said electronic circuitry means serving to amplify and filter the signal from the selected vibration sensor whereby the frequency band associated with the detonation phenomenon are amplified more than other frequencies; an oscilloscope having a visual display and including a signal input terminal and a synchronizing pulse input terminal, said signal input terminal being supplied by the output from said first electronic circuit means; and second electronic circuitry means for generating a wave train of synchronizing pulses for injection into the synchronizing pulse input terminal of said oscilloscope, said second electronic circuitry means including: a pulse generator connected to the output of said magneto and providing a conditioned output pulse each time said magneto ignites an engine cylinder, a stepping counter having as many outputs as there are cylinders in the engine, said counter receiving conditioned pulses from said pulse generator at the engine firing rate, a timing source producing a reset pulse in coincidence with the attainment of top-dead-center by the piston of number one cylinder of said engine, said reset pulse being used to return said stepping counter to its initial state, and a switch for selecting one of the outputs of said stepping counter, said selection being for the purpose of obtaining a synchronizing pulse input for said oscilloscope, said synchronizing pulses being coincident with the passing of ignition pulses to the cylinder spark plugs.
Claim 3
Dependent Claim
35 words
The apparatus as described in claim 1 wherein the oscilloscope is an instrument having the capability to function under reduced atmospheric pressure conditions equivalent to those found at 30,000 ft. altitude above mean sea level.
Claim 4
Dependent Claim
36 words
The apparatus as described in claim 1 wherein the first electronic circuit means includes a linear integrated circuit amplifier having an output serving as the input to a universal active filter of the integrated circuit type.
Claim 5
Dependent Claim
21 words
The apparatus as described in claim 1 and including self contained batteries for powering both first and second electronic circuitry means.
Claim 6
Dependent Claim
14 words
The apparatus as described in claim 1 wherein the vibration sensors are magnetostrictive devices.
Claim 7
Dependent Claim
35 words
The apparatus as described in claim 5 wherein each vibration sensor maintains contact with an engine cylinder through a clamp attaching said sensor to the shell of the spark plug used for igniting said cylinder.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-05-29 | 1981-11-28 | 1982-05-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-05-29 | 1985-11-28 | 1986-05-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-05-29 | 1989-11-28 | 1990-05-30 | $7700.00 | Window Closed / Lapsed |