US4006472A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft altitude alerting device
Assignee: Safe Flight Instrument LLC
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Filing: 1975-05-07
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Granted: 1977-02-01
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Expires: 1995-05-07
Abstract
Abstract The drive for the indicator mechanism of an altimeter is connected so as to drive altitude marker means, the relative position of such marker means being indicative of altitude. The marker means has a marker which may be implemented by a slot formed therein to reference this position. Sensor means is mounted in proximity to and for movement relative to the marker means. The sensor means is manually set to a position relative to the marker means by means of an altitude alert setting device, the set position representing an altitude at which an alerting signal is desired. When the marker means is driven by the altimeter mechanism so that the marker arrives opposite the sensor means, thus indicating that the marker means and the sensor means are both at positions representing the same altitude, a signal is generated by the sensor means which is used to appropriately actuate a signal device indicating that the alerting altitude has been reached.
Inventors
- 👤 Leonard M. Greene
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 06:18
CPC Classifications
G; G01; G01C; G01C5/00; G01C5/005
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
168 words
An altitude alerting device mounted in an aircraft for providing a signal indicating when the aircraft has reached a predetermined alerting altitude comprising: means for indicating the altitude of the aircraft, altitude marker means mechanically driven by said altitude indicating means, said marker means comprising first and second similar discs rotatably driven by the indicating means, a radial marker being formed in each of said discs, which markers are positioned in accordance with the indicated altitude, first and second sensors positioned in proximity to said first and second discs respectively, means for rotatably supporting said sensors for positioning about the rotation axes of said first and second discs respectively, means for setting said sensors in positions relative to their associated discs about the rotation axes of said discs, representing said predetermined altitude, said first disc and sensor providing a coarse altitude scale, said second disc and sensor providing a fine altitude scale, and signaling means for generating an alerting signal in response to an output from said sensors.
Claim 2
Dependent Claim
168 words
An altitude alerting device mounted in an aircraft for providing a signal indicating when the aircraft has reached a predetermined alerting altitude comprising: means for indicating the altitude of the aircraft, altitude marker means mechanically driven by said altitude indicating means, said marker means comprising first and second similar discs rotatably driven by the indicating means, a radial marker being formed in each of said discs, which markers are positioned in accordance with the indicated altitude, first and second sensors positioned in proximity to said first and second discs respectively, means for rotatably supporting said sensors for positioning about the rotation axes of said first and second discs respectively, means for setting said sensors in positions relative to their associated discs about the rotation axes of said discs, representing said predetermined altitude, said first disc and sensor providing a coarse altitude scale, said second disc and sensor providing a fine altitude scale, and signaling means for generating an alerting signal in response to an output from said sensors.
Claim 3
Dependent Claim
25 words
The device of claim 1 wherein is included a coincidence detector for providing a signal to said signaling means when said sensors have simultaneous outputs.
Claim 4
Dependent Claim
207 words
An altitude alerting device mounted in an aircraft for providing a signal indicating when the aircraft has reached a predetermined altitude comprising: an altimeter having an indicator mechanism providing a mechanical signal in accordance with aircraft altitude, altitude marker means comprising first and second discs, each of said discs having a radial slot formed therein, means for supporting said discs for rotation about a predetermined axis, said discs being rotatably driven by said mechanical signal to position said slots about said predetermined axis in accordance with aircraft altitude, sensor means comprising first and second photo-electric detectors positioned proximate to said first and second discs respectively, said first and second detectors and discs representing "coarse" and "fine" altitude positions respectively, means for setting said photo-electric detectors in positions about said predetermined axis relative to said discs in accordance with said predetermined altitude, signaling means for generating said signal indicating that the aircraft has reached the predetermined altitude, coincidence detector means responsive to simultaneous outputs from both of said photo-electric detectors for actuating said signaling means when both said first photo-electric detector and said first disc are in corresponding positions about said axis and said second photo-electric detector and said second disc are in corresponding positions about said axis.
Claim 5
Dependent Claim
207 words
An altitude alerting device mounted in an aircraft for providing a signal indicating when the aircraft has reached a predetermined altitude comprising: an altimeter having an indicator mechanism providing a mechanical signal in accordance with aircraft altitude, altitude marker means comprising first and second discs, each of said discs having a radial slot formed therein, means for supporting said discs for rotation about a predetermined axis, said discs being rotatably driven by said mechanical signal to position said slots about said predetermined axis in accordance with aircraft altitude, sensor means comprising first and second photo-electric detectors positioned proximate to said first and second discs respectively, said first and second detectors and discs representing "coarse" and "fine" altitude positions respectively, means for setting said photo-electric detectors in positions about said predetermined axis relative to said discs in accordance with said predetermined altitude, signaling means for generating said signal indicating that the aircraft has reached the predetermined altitude, coincidence detector means responsive to simultaneous outputs from both of said photo-electric detectors for actuating said signaling means when both said first photo-electric detector and said first disc are in corresponding positions about said axis and said second photo-electric detector and said second disc are in corresponding positions about said axis.
Claim 6
Dependent Claim
24 words
The device of claim 3 and further including stop means for limiting the range of travel of said first detector about said predetermined axis.
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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) | 1980-02-01 | 1980-08-02 | 1981-02-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-02-01 | 1984-08-02 | 1985-02-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-02-01 | 1988-08-02 | 1989-02-01 | $7700.00 | Window Closed / Lapsed |