US4390861A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Cockpit display system to reduce vertigo
Assignee: Singer Co
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Filing: 1981-03-11
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Granted: 1983-06-28
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Expires: 2001-03-11
Abstract
Abstract The disclosures gives a system for indicating visually to a pilot within his normal field of view, so that the pilot need not turn his head, both the identity of a knob or switch which the pilot's hand is touching and also the setting of that switch. The arrangement prevents spatial disorientation, or pilot's "vertigo", by informing the pilot the identity as well as the present setting of a switch located remotely in his cockpit, outside of his normal field of view, without the pilot having to turn his head to look at the switch.
Inventors
- 👤 Edwin Cohen
- 👤 Jack A. Maynard
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 06:56
CPC Classifications
G; G06; G06F; G06F3/00; G06F3/14; G06F3/147; G09; G09G; G09G3/00; G09G3/04
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
184 words
An anti-vertigo cockpit display system for preventing spatial disorientation by indicating, within a pilot's normal field of view, the identity and the setting of a plurality of predetermined functions controlled by separate control switch means located out of the pilot's normal field of view, comprising: a single display means, for displaying a selected one of the functions, located within the pilot's normal field of view so that it may be viewed without it being necessary to turn the pilot's head, the control switch means each having a single knob located out of the pilot's normal field of view, system logic circuit means connected with each of said single knobs to energize said display means when a selected single knob is touched by the pilot's hand, said display means being adapted to reveal both the entire present setting and the identity of the function connected with said selected single knob, so that said pilot is informed without moving his eyes from his normal field of view, and so that said present setting can be altered by adjusting said single knob of said control switch means.
Claim 2
Dependent Claim
184 words
An anti-vertigo cockpit display system for preventing spatial disorientation by indicating, within a pilot's normal field of view, the identity and the setting of a plurality of predetermined functions controlled by separate control switch means located out of the pilot's normal field of view, comprising: a single display means, for displaying a selected one of the functions, located within the pilot's normal field of view so that it may be viewed without it being necessary to turn the pilot's head, the control switch means each having a single knob located out of the pilot's normal field of view, system logic circuit means connected with each of said single knobs to energize said display means when a selected single knob is touched by the pilot's hand, said display means being adapted to reveal both the entire present setting and the identity of the function connected with said selected single knob, so that said pilot is informed without moving his eyes from his normal field of view, and so that said present setting can be altered by adjusting said single knob of said control switch means.
Claim 3
Dependent Claim
37 words
An anti-vertigo cockpit display system as set forth in claim 1 wherein said display means includes separate display devices, one for said identity of the predetermined function and the other for the present setting of said function.
Claim 4
Dependent Claim
37 words
An anti-vertigo cockpit display system as set forth in claim 1 in which said system logic circuit means includes an information interchange means to maintain coded characters for identifying each of predetermined functions by said display means.
Claim 5
Dependent Claim
38 words
An anti-vertigo cockpit display system as set forth in claim 3 wherein said system logic circuit means includes selection means having means to match information encoded with desired information so that only meaningful information is selected and displayed.
Claim 6
Dependent Claim
39 words
An anti-vertigo cockpit display system as set forth in claim 4 wherein said selection means includes a plurality of AND gates, and decoding conversion means to match said coded characters of said information interchange means to said display means.
Claim 7
Dependent Claim
30 words
An anti-vertigo cockpit display system as set forth in claim 5 including separate decoding conversion means to match selected encoded information to a setting display part of said display means.
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) | 1986-06-27 | 1986-12-27 | 1987-06-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-06-27 | 1990-12-27 | 1991-06-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-06-27 | 1994-12-27 | 1995-06-28 | $7700.00 | Window Closed / Lapsed |