Patent US4903017A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4903017A Expired / Lapsed US ⏱️ 0.0 years remaining

Aircraft display devices

Assignee: BAE Systems Electronics Ltd
•
Filing: 1989-03-20
•
Granted: 1990-02-20
•
Expires: 2009-03-20
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A display device for use as an attitude display in an aircraft comprising a circular array (5) of selectively activatable display elements, the elements being disposed in equally angularly spaced radially extending lines, each line having the same number of elements with corresponding elements in the different lines at the same radial distance from the center of the array (5); and a controller (3) for selectively activating said display elements in accordance with aircraft attitude whereby the selected elements form a visible pattern indicative of the aircraft attitude.

Inventors

  • 👤 Frank R. Wooller

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 18:24
CPC Classifications
G; G01; G01C; G01C23/00; G01C23/005

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 245 words
A display device for an aircraft, comprising: (A) a circular array including a multitude of selectively activatable display elements, the array having an outer periphery bounding a circular display area having a center, (i) the elements being disposed in equally angularly spaced lines extending radially from the center of the display area, each radial line having at least four, and the same number of, elements with corresponding elements in the different radial lines at the same radial distance from the center of the display area, (ii) the elements along each radial line occupying a major proportion of the radial line, (iii) each said element subtending an angle of substantially the same magnitude at the center of the display area and having a radial dimension of substantially the same magnitude, and (iv) each said element being arranged to be substantially contiguous with each adjacent element; and (B) means for selectively activating said display elements in accordance with aircraft attitude whereby the selected elements form a visible area and line pattern indicative of the aircraft attitude, said means for selectively activating said display elements activating elements in a segmental area defined by a chord joining extremities of an arcuate portion of the outer periphery of the array, said chord moving with respect to the array in a direction normal to its length to depict changes in pitch of the aircraft and changing its angle with respect to the array to depict changes in roll of the aircraft.
Claim 2
Dependent Claim 245 words
A display device for an aircraft, comprising: (A) a circular array including a multitude of selectively activatable display elements, the array having an outer periphery bounding a circular display area having a center, (i) the elements being disposed in equally angularly spaced lines extending radially from the center of the display area, each radial line having at least four, and the same number of, elements with corresponding elements in the different radial lines at the same radial distance from the center of the display area, (ii) the elements along each radial line occupying a major proportion of the radial line, (iii) each said element subtending an angle of substantially the same magnitude at the center of the display area and having a radial dimension of substantially the same magnitude, and (iv) each said element being arranged to be substantially contiguous with each adjacent element; and (B) means for selectively activating said display elements in accordance with aircraft attitude whereby the selected elements form a visible area and line pattern indicative of the aircraft attitude, said means for selectively activating said display elements activating elements in a segmental area defined by a chord joining extremities of an arcuate portion of the outer periphery of the array, said chord moving with respect to the array in a direction normal to its length to depict changes in pitch of the aircraft and changing its angle with respect to the array to depict changes in roll of the aircraft.
Claim 3
Dependent Claim 27 words
A display device according to claim 1, wherein said radially extending lines have inner ends defining a central space in which there are no said display elements.
Claim 4
Dependent Claim 27 words
A display device according to claim 1, wherein said display elements activated in said segmental area are alternate ones of said display elements in said segmental area.
Claim 5
Dependent Claim 34 words
A display device according to claim 1 wherein said means for activating is arranged to activate selected ones of said display elements to indicate the orientation of the aircraft with respect to the array.
Claim 6
Dependent Claim 27 words
A display device according to claim 1 wherein said means for activating is arranged to activate selected ones of said display elements to indicate the aircraft heading.
Claim 7
Dependent Claim 32 words
A display device according to claim 1 wherein said means for activating is arranged to activate selected ones of said display elements to indicate the direction of the ground from the aircraft.
Claim 8
Dependent Claim 47 words
A display device according to claim 1 wherein said means for activating is arranged to activate selected ones of said display elements to display at least one line substantially parallel to the chord of the displayed segment to indicate a given degree of pitch of the aircraft.
Claim 9
Dependent Claim 29 words
A display device according to claim 2 wherein a permanent marking is provided in said central space to indicate the orientation of the aircraft with respect to the array.
Claim 10
Dependent Claim 23 words
A display device according to claim 1 having at least one permanent marking positioned outside said array to assist in indicating aircraft attitude.

References Cited (Backward Citations)

US3018661A Cited
GB2131225A Cited
US4583094A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-02-19 1993-08-21 1994-02-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-02-19 1997-08-21 1998-02-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-02-19 2001-08-21 2002-02-20 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag