US5675327A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Optoelectronic device for assistance in the piloting of an aircraft
Assignee: Thales Avionics SAS
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Filing: 1995-10-04
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Granted: 1997-10-07
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Expires: 2015-10-04
Abstract
Abstract The disclosed optoelectronic device is designed to facilitate the piloting of an aircraft under conditions of poor visibility, notably during landing at the stage when the aircraft approaches a runway. It consists of a collimator which displays, in addition to the artificial skyline, miniature aircraft index and attitude bars, a slope scale positioned across and on either side of the artificial skyline, at the position of the selected course chosen by the pilot. This slope scale, depicted in the form of a line of dots spaced out at one slope degree, enables the pilot to be presented simultaneously with information on selected course and slope and enables the determining of pitch attitude with high precision.
Inventors
- 👤 Philippe Coirier
- 👤 Alain Goujon
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 11:54
CPC Classifications
G; G02; G02B; G02B27/00; G02B27/01; G01; G01C; G01C23/00; G01C23/005; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0653; G05D1/0676
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
169 words
An optoelectronic device for assistance in the piloting of an aircraft that is provided with a navigation system determining, inter alia, the heading, the pitch attitude and the roll attitude as well as the ground speed vector of the aircraft, and with a collimator for displaying an artificial skyline graduated with a heading scale and surrounded by attitude bars giving a zero roll attitude and slope reference, a reticule identifying the ground speed vector and a fixed reticule formed by a miniature aircraft index identifying the heading and the pitch and roll attitudes of the aircraft with respect to the artificial skyline, wherein said device comprises means for the display, on the collimator, of a slope scale positioned across and on either side of the artificial skyline, at the position of the selected course chosen by the pilot; wherein the ground speed vector reticule visually identifies orientation of the ground speed vector in terms of course and slope relative to the slope scale which also identifies the selected course.
Claim 2
Dependent Claim
169 words
An optoelectronic device for assistance in the piloting of an aircraft that is provided with a navigation system determining, inter alia, the heading, the pitch attitude and the roll attitude as well as the ground speed vector of the aircraft, and with a collimator for displaying an artificial skyline graduated with a heading scale and surrounded by attitude bars giving a zero roll attitude and slope reference, a reticule identifying the ground speed vector and a fixed reticule formed by a miniature aircraft index identifying the heading and the pitch and roll attitudes of the aircraft with respect to the artificial skyline, wherein said device comprises means for the display, on the collimator, of a slope scale positioned across and on either side of the artificial skyline, at the position of the selected course chosen by the pilot; wherein the ground speed vector reticule visually identifies orientation of the ground speed vector in terms of course and slope relative to the slope scale which also identifies the selected course.
Claim 3
Dependent Claim
16 words
A device according to claim 1, wherein said slope scale is perpendicular to the artificial skyline.
Claim 4
Dependent Claim
38 words
A device according to claim 1, wherein said means to display a slope scale at the location of the heading of the selected course displays a line of dots across and on either side of the artificial skyline.
Claim 5
Dependent Claim
27 words
A device according to claim 3, wherein the dots of said line of dots are evenly spaced out at a graduation pitch smaller than one slope degree.
Claim 6
Dependent Claim
53 words
A device according to claim 3, wherein the dots of said line of dots are evenly spaced out at a pitch of one slope degree and wherein the dots at every fifth slope degree have a size greater than that of the remaining dots to facilitate the ease of reading of the scale.
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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) | 2000-10-06 | 2001-04-07 | 2001-10-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2004-10-06 | 2005-04-07 | 2005-10-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2008-10-06 | 2009-04-07 | 2009-10-07 | $7700.00 | Window Closed / Lapsed |