US4434391A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Capacitive feedback transducer and closed loop instrument meter mechanism
Assignee: Honeywell Inc
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Filing: 1982-01-15
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Granted: 1984-02-28
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Expires: 2002-01-15
Abstract
Abstract A display pointer is driven back and forth along a predetermined path by a geared-down miniature d.c. servomotor in accordance with a command signal. The path is determined by an elongated printed circuit board base having closely adjacent, elongated, coextensive triangularly shaped plates thereon, constituting stationary capacitor plates of a pair of variable capacitors. The printed circuit board includes a dielectric material which also overlays the triangular plates. A relatively narrow, electrically conductive slider member extends laterally across the triangular plates and is supported by and rides on the printed circuit board and constitutes a common movable capacitor plate for the variable capacitors. The display pointer is attached to and positioned by the slider. The slider in turn is displaced along the printed circuit board by means of a cable and pulley mechanism coupled to the servomotor. The pair of variable capacitors are electrically connected with a pair of diodes in balanced bridge fashion in order to provide a signal proportional to the position of the slider along the path. The position signal is fed back and summed with the command signal to provide an error signal for controlling the servomotor.
Inventors
- 👤 Harold L. Swartz
- 👤 Randal A. Atkeisson
- 👤 Rodney A. Carter
- 👤 Russell C. Parker
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 21:39
CPC Classifications
G; G01; G01D; G01D5/00; G01D5/12; G01D5/14; G01D5/24; G01D5/241; G01D5/2412; G01R; G01R1/00; G01R1/02; G01R1/08
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
236 words
A flight instrument for physically displaying command signals to a pilot, comprising: a case, servomotor means coupled to said case and responsive to said command signals for providing rotational displacement; a capacitive transducer having at least first and second variable capacitors responsive to the rotational displacement of said servomotor means for providing feedback signals to said servomotor means, including; a substrate mounted on said case; a first tapered conductive plate disposed on said substrate; a second tapered conductive plate disposed on said substrate and substantially coextensive with said first conductive plate; conductive means mounted to slide parallel to said substrate in response to the rotational displacement of said servomotor means in operative relationship with said first and second tapered conductive plates; and means for coupling said sliding conductive means to ground; bridge circuit means for providing output signals proportional to the difference in capacitance of said first and second variable capacitors including: first rectifying means and first resistance means which are coupled to said first variable capacitor; second rectifying means, oppositely poled to said first rectifying means, and second resistance means coupled to said second variable capacitor; means for applying an alternating current to said first and second rectifying means; and capacitive filter means coupled between ground and said first and second resistance means; and a pointer coupled to said sliding conductive means, for providing the pilot with a visual display corresponding to said command signals.
Claim 2
Dependent Claim
236 words
A flight instrument for physically displaying command signals to a pilot, comprising: a case, servomotor means coupled to said case and responsive to said command signals for providing rotational displacement; a capacitive transducer having at least first and second variable capacitors responsive to the rotational displacement of said servomotor means for providing feedback signals to said servomotor means, including; a substrate mounted on said case; a first tapered conductive plate disposed on said substrate; a second tapered conductive plate disposed on said substrate and substantially coextensive with said first conductive plate; conductive means mounted to slide parallel to said substrate in response to the rotational displacement of said servomotor means in operative relationship with said first and second tapered conductive plates; and means for coupling said sliding conductive means to ground; bridge circuit means for providing output signals proportional to the difference in capacitance of said first and second variable capacitors including: first rectifying means and first resistance means which are coupled to said first variable capacitor; second rectifying means, oppositely poled to said first rectifying means, and second resistance means coupled to said second variable capacitor; means for applying an alternating current to said first and second rectifying means; and capacitive filter means coupled between ground and said first and second resistance means; and a pointer coupled to said sliding conductive means, for providing the pilot with a visual display corresponding to said command signals.
Claim 3
Dependent Claim
33 words
An apparatus according to claim 1 wherein said means for coupling said sliding conductive means to ground includes ground plate means disposed on said substrate, in operative relationship with said sliding conductive means.
Claim 4
Dependent Claim
17 words
An apparatus according to claim 2 wherein said first and second conductive plates have generally triangular shapes.
Claim 5
Dependent Claim
58 words
An apparatus according to claim 2 wherein said substrate is fabricated from a dielectric material and has first and second substantially parallel surfaces with tapered conductive means, said second tapered conductive means and said ground plate means are disposed on said first and second surfaces in substantially mirror image relationship with a layer of said dielectric material thereover.
Claim 6
Dependent Claim
65 words
An apparatus according to claim 4 wherein said slidable conductive means includes a bifurcated slider having a first portion disposed parallel to said first surface of said substrate and a second portion disposed parallel to said second surface of said substrate, said first and second portions having a slot therebetween and and in operative relationship with said tapered conductive means and said ground plate means.
Claim 7
Dependent Claim
26 words
An apparatus according to claim 5 which includes a roller disposed in said slot of said bifurcated slider to ride along an edge of said substrate.
Claim 8
Dependent Claim
34 words
An apparatus according to claim 6 which further includes at least two pulleys disposed on said substrate and a cable threaded therethrough and coupled to said first and second portions of said bifurcated slider.
Claim 9
Dependent Claim
27 words
An apparatus according to claim 7 wherein an end of said cable is coupled to said bifurcated slider by means for adjusting the tension of said cable.
Claim 10
Dependent Claim
43 words
An apparatus according to claim 2 wherein said first and second rectifying means include diodes disposed upon said substrate, said first and second resistance means include resistors disposed upon said substrate, and said capacitive filter means includes a capacitor disposed upon said substrate.
Claim 11
Dependent Claim
27 words
An apparatus according to claim 1 wherein said servomotor means includes a summing junction for summing the feedback signals from said capacitive transducer with said command signals.
Claim 12
Dependent Claim
32 words
An apparatus according to claim 10 wherein said servomotor means includes means for amplifying the output of said summing junction and driving a d.c. motor coupled to a gear train and pulley.
Claim 13
Dependent Claim
38 words
An apparatus according to claim 11 wherein said sliding conductive means of said capacitive transducer is coupled to said pulley of said servomotor means by at least a pair of pulleys disposed on said substrate and a wire.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-02-27 | 1987-08-29 | 1988-02-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-02-27 | 1991-08-29 | 1992-02-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-02-27 | 1995-08-29 | 1996-02-28 | $7700.00 | Window Closed / Lapsed |