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US4980683A Expired / Lapsed US ⏱️ 0.0 years remaining

Aircraft instrument systems

Assignee: SMITHS INDUSTRIES PUBLIC Ltd A BRITISH Co
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Filing: 1989-11-03
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Granted: 1990-12-25
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Expires: 2009-11-03
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Abstract

Abstract An aircraft collision avoidance instrument system has a display located in the aircraft glareshield in the peripheral field of view of the pilot when the pilot is looking forwardly through the aircraft window. The display has a matrix array of LCD elements which is controlled to provide a continually changing image that is visible in the peripheral field of view of the pilot when a possible collision with another aircraft is likely. The changing image may be arrows moving up or down the display to indicate climb or decend, or a flashing horizontal line to indicate that present height must be maintained. An alphanumeric legend indicative of the collision avoidance action to be taken is also provided by the display. When no collision is likely, the display is used to present other information to the pilot.

Inventors

  • 👤 Peter-Francis O'Sullivan
  • 👤 Keith G. Dougan

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 14:16
CPC Classifications
G; G01; G01S; G01S7/00; G01S7/02; G01S7/04; G01S13/00; G01S13/88; G01S13/93; G01S13/933; G02; G02B; G02B27/00; G02B27/01

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 202 words
An aircraft instrument system for a first aircraft comprising: means to identify when a possible collision with a second aircraft is likely; means for determining the evading action to be taken by the pilot of the first aircraft to avoid collision; means for providing a first signal when the evading action is to climb, and a second signal when the evading action is to descent; visual display means including a matrix array of electrically energizable elements; means mounting said visual display means in the peripheral field of view of the pilot when the pilot is looking forwardly through the aircraft window; means supplying said first and second signals to the visual display means to control the elements in said matrix array to provide a display image of upwardly moving signs and downwardly moving signs respectively such as to produce two alternative changing images on a single display that are visible to the pilot in the pilot's peripheral field of view and that are distinguishable form one another in the pilot's peripheral field of view, thereby to visually advise the pilot of the first aircraft to climb or descent without the need for the pilot to look directly at said visual display means.
Claim 2
Dependent Claim 202 words
An aircraft instrument system for a first aircraft comprising: means to identify when a possible collision with a second aircraft is likely; means for determining the evading action to be taken by the pilot of the first aircraft to avoid collision; means for providing a first signal when the evading action is to climb, and a second signal when the evading action is to descent; visual display means including a matrix array of electrically energizable elements; means mounting said visual display means in the peripheral field of view of the pilot when the pilot is looking forwardly through the aircraft window; means supplying said first and second signals to the visual display means to control the elements in said matrix array to provide a display image of upwardly moving signs and downwardly moving signs respectively such as to produce two alternative changing images on a single display that are visible to the pilot in the pilot's peripheral field of view and that are distinguishable form one another in the pilot's peripheral field of view, thereby to visually advise the pilot of the first aircraft to climb or descent without the need for the pilot to look directly at said visual display means.
Claim 3
Dependent Claim 29 words
An instrument system according to claim 1, wherein the first aircraft has a glareshield, and wherein said mounting the means mounts the visual display means in the aircraft glareshield.
Claim 4
Dependent Claim 12 words
An instrument system according to claim 1, wherein said signs are arrows.
Claim 5
Dependent Claim 32 words
An instrument system according to claim 1, wherein the display means is arranged to provide a flashing representation of a stationary sign when the signal indicates that the pilot should maintain height.
Claim 6
Dependent Claim 15 words
An instrument system according to claim 6, wherein the stationary sign is a horizontal line.
Claim 7
Dependent Claim 31 words
An instrument system according to claim 1, wherein the visual display means also provides a display of an alphanumeric legend indicative of the evading action to be taken by the pilot.
Claim 8
Dependent Claim 34 words
An instrument system according to claim 1, wherein the system includes means for driving the visual display means to represent to the pilot information other than collision avoidance action when no collision is likely.
Claim 9
Dependent Claim 31 words
An instrument system according to claim 1, wherein the system includes an audible indicator which is operable to indicate that collision avoidance information is being presented on the visual display means.

References Cited (Backward Citations)

US3621210A Cited
US3614728A Cited
US3846746A Cited
US3699511A Cited
US4181405A Cited
US4403220A Cited
US4835537A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-12-24 1994-06-25 1994-12-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-12-24 1998-06-25 1998-12-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-12-24 2002-06-25 2002-12-25 $7700.00 Window Closed / Lapsed

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