Patent US4061297A successfully refreshed from Google Patents.
US4061297A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Approach range monitor
Assignee: AirData Inc
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Filing: 1975-06-06
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Granted: 1977-12-06
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Expires: 1995-06-06
Abstract
Abstract An area navigation system capable of operating during an ILS approach to provide the pilot range and bearing with respect to the outer and middle markers for a front course approach, and with respect to the final approach fix and the end of the runway for a back course approach. The system operates by automatically connecting the # 2 NAV receiver to the RNAV during ILS operation while the ILS localizer converter is connected to the # 1 NAV receiver. At the same time the RNAV is disconnected from the left side indicator so this may be used for the localizer.
Inventors
- 👤 George B. Foster
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 11:54
CPC Classifications
G; G01; G01S; G01S5/00; G01S5/02; G01S5/12; G01S1/00; G01S1/02; G01S1/08
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
196 words
In an aircraft navigation system having first and second NAV receivers, at least one DME receiver, a localizer converter, a left-right steering display, and an RNAV computer, means to select reception of range and bearing to Waypoint information signals to a Waypoint station and means responsive to the range and bearing to Waypoint information signals to display said range and/or bearing of the aircraft to the selected Waypoint, the improvement comprising first switch means for selectively coupling said first or second receiver to the RNAV computer; means coupling said DME receiver to said RNAV computer; means coupling said first NAV receiver to said localizer converter; and second switch means simultaneously operable with said first switch means for selectively coupling the output of said RNAV computer or said localizer converter to said steering display, said first NAV receiver being coupled to said RNAV computer when said RNAV computer output is connected to said steering indicator and said second NAV receiver being connected to said RNAV computer when said localizer converter output is connected to said steering display, and wherein said range and bearing to Waypoint is displayed when said second NAV receiver is connected to said RNAV.
Claim 2
Dependent Claim
196 words
In an aircraft navigation system having first and second NAV receivers, at least one DME receiver, a localizer converter, a left-right steering display, and an RNAV computer, means to select reception of range and bearing to Waypoint information signals to a Waypoint station and means responsive to the range and bearing to Waypoint information signals to display said range and/or bearing of the aircraft to the selected Waypoint, the improvement comprising first switch means for selectively coupling said first or second receiver to the RNAV computer; means coupling said DME receiver to said RNAV computer; means coupling said first NAV receiver to said localizer converter; and second switch means simultaneously operable with said first switch means for selectively coupling the output of said RNAV computer or said localizer converter to said steering display, said first NAV receiver being coupled to said RNAV computer when said RNAV computer output is connected to said steering indicator and said second NAV receiver being connected to said RNAV computer when said localizer converter output is connected to said steering display, and wherein said range and bearing to Waypoint is displayed when said second NAV receiver is connected to said RNAV.
Claim 3
Dependent Claim
89 words
Apparatus as defined in claim 1 further including first and second means for tuning the first and second NAV receivers; and third switch means simultaneously operable with said first and second switch means for selectively coupling said first and second tuning means to said DME receiver, said first tuning means being coupled to said DME receiver when said first NAV receiver is coupled to said RNAV computer, and said second tuning means being coupled to said DME receiver when said second NAV receiver is coupled to said RNAV computer.
Claim 4
Dependent Claim
36 words
Apparatus as defined in claim 1 further including a bearing indicator, and fourth switching means for connecting said second NAV receiver to said bearing indicator when the second NAV receiver is connected to said RNAV computer.
Claim 5
Dependent Claim
18 words
In the aircraft navigation system of claim 1 wherein said first and second NAV receivers are VOR receivers.
Claim 6
Dependent Claim
18 words
In the aircraft navigation system of claim 1 wherein said first and second NAV receivers are TACAN receivers.
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) | 1980-12-05 | 1981-06-06 | 1981-12-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-12-05 | 1985-06-06 | 1985-12-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-12-05 | 1989-06-06 | 1989-12-06 | $7700.00 | Window Closed / Lapsed |