Patent US4000028A successfully refreshed from Google Patents.
Patent US4145608A successfully refreshed from Google Patents.
US4145608A
Expired / Lapsed
US
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Rotational reference position detecting apparatus
Assignee: Denso Corp
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Filing: 1977-09-14
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Granted: 1979-03-20
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Expires: 1997-09-14
Abstract
Abstract A crankshaft rotational reference position detecting apparatus is adapted for use with ignition timing control systems for internal combustion engines. The apparatus comprises a rotor disk fixedly mounted on the crankshaft of an engine and having rotational angle information indicating slits and a rotational reference position indicating mark which are formed along the periphery thereof, a first sensor for detecting each rotational angle information indicating slit and generating a first pulse signal corresponding thereto, the first sensor producing no first pulse signal when a rotational reference position is detected, a second sensor located at a position displaced from the first sensor in a desired rotational direction and adapted to generate a second pulse signal delayed in phase from the first pulse signal, a storage device responsive to the second pulse signals to store the output level of the first sensor, and a detection circuit responsive to a change in the output of the storage device which is indicative of the detection of the rotational reference position by the first sensor so as to generate a reference position detection pulse. In the event that the rotor disk is rotated in the reverse direction, the detection of the rotational reference position does not result in the generation of any reference position detection pulse.
Inventors
- 👤 Shinji Shirasaki
- 👤 Takashi Yamada
- 👤 Hiroyasu Fukaya
- 👤 Yukio Sakakibara
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 18:08
CPC Classifications
F; F02; F02P; F02P7/00; F02P7/06; F02P7/073; G; G01; G01D; G01D5/00; G01D5/12; G01D5/244; G01D5/24404; G01D5/245; G01D5/2454; G01D5/2455; G01D5/2457; G01D5/26; G01D5/32; G01D5/34; G01D5/36
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
188 words
A rotational reference position detecting apparatus for use in an engine system comprising: a rotor disk coupled with an engine to be rotated thereby; a plurality of equispaced means provided on said rotor disk circularly except at a position indicative of the rotational reference position of said engine; a first sensor, positioned adjacent to said rotor disk, for generating a first signal which changes the signal level thereof in response to the passing of each of said equispaced means; a second sensor positioned adjacent to said rotor disk for generating a second signal which changes the signal level thereof in response to the passing of each of said equispaced means, said second sensor being apart from said first sensor such that the level change of said first signal precedes the level change of said second signal; and a detection circuit, connected to said first and second sensors, for generating a reference pulse by detecting the signal level of said first signal at each level change of said second signal, said reference pulse representing that said engine is rotated in a predetermined direction and to said rotational reference position.
Claim 2
Dependent Claim
188 words
A rotational reference position detecting apparatus for use in an engine system comprising: a rotor disk coupled with an engine to be rotated thereby; a plurality of equispaced means provided on said rotor disk circularly except at a position indicative of the rotational reference position of said engine; a first sensor, positioned adjacent to said rotor disk, for generating a first signal which changes the signal level thereof in response to the passing of each of said equispaced means; a second sensor positioned adjacent to said rotor disk for generating a second signal which changes the signal level thereof in response to the passing of each of said equispaced means, said second sensor being apart from said first sensor such that the level change of said first signal precedes the level change of said second signal; and a detection circuit, connected to said first and second sensors, for generating a reference pulse by detecting the signal level of said first signal at each level change of said second signal, said reference pulse representing that said engine is rotated in a predetermined direction and to said rotational reference position.
Claim 3
Dependent Claim
56 words
A rotational reference position detecting apparatus according to claim 1, wherein said plurality of equispaced means include 359 slits each of which extends radially, and wherein each of said first and second sensors includes a photo emitter and a photo receiver which are positioned respectively at one and the other side surfaces of said rotor disk.
Claim 4
Dependent Claim
150 words
A rotational reference position detecting apparatus according to claim 1, wherein said detection circuit includes: a store circuit, connected to said first and second sensors, for storing the signal level of said first signal at each level change of said second signal; a clock circuit for generating a train of clock pulses at a fixed frequency which is higher than the highest one of said first signal; a shift circuit, connected to said store and clock circuits and having a plurality of output terminals, for sequentially producing output signals indicative of said first signal stored by said store circuit at said output terminals in response to said clock pulses; and a logic circuit, connected to said shift register, for subjecting some of said sequentially produced output signals to a predetermined logical operation to thereby produce said reference pulse which has a time width shorter than that of said first signal.
Claim 5
Dependent Claim
234 words
A rotational reference position detecting apparatus for use in an engine system comprising: a rotor disk coupled with the crankshaft of an engine to be rotated therewith and circularly provided with a plurality of rotational angle informations each of which is indicative of the unit rotational angle of said crankshaft and with a reference position information which is indicative of the rotational reference position of said crankshaft, said reference position information having a predetermined width which is two times wider than that of each of said rotational angle informations; a first sensor, positioned to face said rotational angle informations and said reference position information, for generating a first pulse signal only when each of said rotational angle informations passes therethrough; a second sensor, positioned to face said rotational angle informations and said reference position information, for generating a second pulse signal only when each of said rotational angle informations passes therethrough, said second sensor being positioned apart from said first sensor so that said second pulse signal is started to be generated after said first pulse signal is started to be generated; and a detection circuit, connected to said first and second sensors, for generating a reference pulse by detecting the absence of said first pulse signal at the start of said second pulse signal, said reference pulse indicating that said engine is rotated in a predetermined direction and to said rotational reference position.
Claim 6
Dependent Claim
234 words
A rotational reference position detecting apparatus for use in an engine system comprising: a rotor disk coupled with the crankshaft of an engine to be rotated therewith and circularly provided with a plurality of rotational angle informations each of which is indicative of the unit rotational angle of said crankshaft and with a reference position information which is indicative of the rotational reference position of said crankshaft, said reference position information having a predetermined width which is two times wider than that of each of said rotational angle informations; a first sensor, positioned to face said rotational angle informations and said reference position information, for generating a first pulse signal only when each of said rotational angle informations passes therethrough; a second sensor, positioned to face said rotational angle informations and said reference position information, for generating a second pulse signal only when each of said rotational angle informations passes therethrough, said second sensor being positioned apart from said first sensor so that said second pulse signal is started to be generated after said first pulse signal is started to be generated; and a detection circuit, connected to said first and second sensors, for generating a reference pulse by detecting the absence of said first pulse signal at the start of said second pulse signal, said reference pulse indicating that said engine is rotated in a predetermined direction and to said rotational reference position.
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) | 1982-03-19 | 1982-09-18 | 1983-03-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-03-19 | 1986-09-18 | 1987-03-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-03-19 | 1990-09-18 | 1991-03-20 | $7700.00 | Window Closed / Lapsed |