Patent US3824535A successfully refreshed from Google Patents.
US3824535A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Head-up display apparatus including means for displaying three dimensional aircraft vertical path line
Assignee: Bendix Corp
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Filing: 1972-09-28
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Granted: 1974-07-16
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Expires: 1992-09-28
Abstract
Abstract In combination with head-up display apparatus for displaying aircraft navigational symbology to the pilot of the craft as a real world infinity overlay, means for displaying a three dimensional aircraft vertical path line appearing to the pilot to extend from a point just forward of the craft on out to infinity.
Inventors
- 👤 R Rover
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 06:31
CPC Classifications
G; G08; G08G; G08G5/00; G08G5/20; G08G5/21; G02; G02B; G02B27/00; G02B27/01; G02B27/0101; G02B27/0149; B; B60; B60K; B60K2360/00; B60K2360/20; B60K2360/33; B60K2360/334; G02B2027/0154; G02B2027/0156; G02B2027/0169; G02B27/0179; G02B2027/0187
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
269 words
Low profile head-up display apparatus for displaying an image including aircraft navigational symbology and an aircraft vertical path line to the pilot of the craft, comprising: means for generating the image including a cathode ray tube with a phosphor plane on which the image is generated, and a face plate having an outer surface and an inner surface adjacent the phosphor plane for transferring the image to said outer surface; a curved combiner which is viewed by the pilot; means disposed between the image generating means and the combiner for transmitting the image away from the generating means and for rotating said image into alignment with the optical axis of the combiner including a U-shaped image conduit having an input surface disposed in intimate contact with the face plate outer surface and rotating the symbology at the outer surface to a conduit outer surface in alignment with the optical axis of the combiner; means arranged with the transmitting and rotating means for transmitting the aircraft navigational symbology to the combiner so that said symbology appears as a real world infinity overlay including a contour element having an input surface disposed in intimate contact with the conduit outer surface and a curved output surface; means arranged with the transmitting means for transmitting the vertical path line to the combiner so that said line appears to extend from a point just forward of the craft to a point at infinity including a wedge having an input surface which is curved to match the curved output surface of the contour element and is in intimate contact therewith, and a sloping output surface.
Claim 2
Dependent Claim
269 words
Low profile head-up display apparatus for displaying an image including aircraft navigational symbology and an aircraft vertical path line to the pilot of the craft, comprising: means for generating the image including a cathode ray tube with a phosphor plane on which the image is generated, and a face plate having an outer surface and an inner surface adjacent the phosphor plane for transferring the image to said outer surface; a curved combiner which is viewed by the pilot; means disposed between the image generating means and the combiner for transmitting the image away from the generating means and for rotating said image into alignment with the optical axis of the combiner including a U-shaped image conduit having an input surface disposed in intimate contact with the face plate outer surface and rotating the symbology at the outer surface to a conduit outer surface in alignment with the optical axis of the combiner; means arranged with the transmitting and rotating means for transmitting the aircraft navigational symbology to the combiner so that said symbology appears as a real world infinity overlay including a contour element having an input surface disposed in intimate contact with the conduit outer surface and a curved output surface; means arranged with the transmitting means for transmitting the vertical path line to the combiner so that said line appears to extend from a point just forward of the craft to a point at infinity including a wedge having an input surface which is curved to match the curved output surface of the contour element and is in intimate contact therewith, and a sloping output surface.
Claim 3
Dependent Claim
44 words
Apparatus as described by claim 1, wherein: the contour element has an input surface disposed in intimate contact with the conduit output surface and a curved output surface; and the contour element transfers the symbology from its input surface to its curved output surface.
Claim 4
Dependent Claim
25 words
Apparatus as described by claim 1, wherein: the curvature of the contour element matches the curvature of the combiner for focusing the symbology at infinity.
Claim 5
Dependent Claim
23 words
Apparatus as described by claim 1, wherein: the curved output surface has a slot for receiving the curved input surface of the wedge.
Claim 6
Dependent Claim
29 words
Apparatus as described by claim 4, including: means coupled to the wedge for displacing the wedge within the slot as a function of angle of attack of the aircraft.
Claim 7
Dependent Claim
144 words
Apparatus as described by claim 1, wherein: the means for generating the image, the means disposed between the image generating means and the combiner for transmitting the image away from the generating means and for rotating said image into alignment with the optical axis of the combiner, the means arranged with the transmitting and rotating means for transmitting the aircraft navigational symbology to the combiner so that said symbology appears as a real world infinity overlay, and the means arranged with the transmitting means for transmitting the vertical path line to the combiner so that said line appears to extend from a point just forward of the craft to a point at infinity are arranged within a housing disposed atop the aircraft instrument panel; and the combiner is supported by the housing and external thereto, and in optical arrangement with all of said means.
Claim 8
Dependent Claim
24 words
Apparatus as described by claim 6, wherein: the combiner is pivotally supported by the bracket so as to be pivotable to an out-of-view position.
Claim 9
Dependent Claim
37 words
Apparatus as described by claim 6, including: handle means for supporting the last mentioned means within the housing and operable for selectively removing sAid means from the optical arrangement and for replacing said means in the arrangement.
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) | 1977-07-15 | 1978-01-14 | 1978-07-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1981-07-15 | 1982-01-14 | 1982-07-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1985-07-15 | 1986-01-14 | 1986-07-16 | $7700.00 | Window Closed / Lapsed |