US4711512A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Compact head-up display
Assignee: ERIM International Inc
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Filing: 1985-07-12
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Granted: 1987-12-08
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Expires: 2005-07-12
Abstract
Abstract A compact head-up display comprising a combiner which combines light energy from an outside view with light energy transmitted within the combiner and diffracted out by means of an upper diffraction grating. The head-up display disclosed further comprises an image source, a collimating lens, and a lower diffraction grating for diffracting the collimated light energy into the combiner.
Inventors
- 👤 Juris Upatnieks
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 14:48
CPC Classifications
G; G02; G02B; G02B27/00; G02B27/01; G02B27/0101; G02B27/0103; B; B60; B60K; B60K35/00; B60K35/20; B60K35/21; B60K35/22; B60K35/23; B60K35/235; B60K35/50; B60K35/53; G02B27/42; G02B27/4272; B60K2360/00; B60K2360/20; B60K2360/33; B60K2360/334; G02B2027/0112; G02B2027/0116; G02B27/0149; G02B2027/0165; G02B6/00; G02B6/0001; G02B6/0011; G02B6/0013; G02B6/0015; G02B6/0016; G02B6/0033; G02B6/0035; G02B6/0038
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
226 words
A head-up display for use in an aircraft cockpit having a windshield, comprising: source means for producing collimated light wavefronts of an image to be displayed to the pilot; an elongated optical element having a first end disposed in the path of the collimated light wavefronts produced by the source means, a second end disposed in the field of view of the pilot through the windshield, and operative to internally reflect optical wavefronts from the first end to the second end; a first diffractive element supported at the first end of the optical element so that the collimated light wavefronts produced by the source means are incident upon the first diffractive element, the first diffractive element being operative to diffract the light wavefronts into the optical element, and a second diffractive element supported at the second end of the optical element operative to diffract the light wavefronts, diffracted into the optical element by the first diffractive element, out of the optical element in the direction of the pilot's eye, while retaining the collimation thereof, the second end of the optical element and the second diffractive element being substantially transparent to light incident on the optical element from the field of view of the pilot through the windshield, whereby the pilot views in the image produced by the source means superimposed on his view through the windshield.
Claim 2
Dependent Claim
226 words
A head-up display for use in an aircraft cockpit having a windshield, comprising: source means for producing collimated light wavefronts of an image to be displayed to the pilot; an elongated optical element having a first end disposed in the path of the collimated light wavefronts produced by the source means, a second end disposed in the field of view of the pilot through the windshield, and operative to internally reflect optical wavefronts from the first end to the second end; a first diffractive element supported at the first end of the optical element so that the collimated light wavefronts produced by the source means are incident upon the first diffractive element, the first diffractive element being operative to diffract the light wavefronts into the optical element, and a second diffractive element supported at the second end of the optical element operative to diffract the light wavefronts, diffracted into the optical element by the first diffractive element, out of the optical element in the direction of the pilot's eye, while retaining the collimation thereof, the second end of the optical element and the second diffractive element being substantially transparent to light incident on the optical element from the field of view of the pilot through the windshield, whereby the pilot views in the image produced by the source means superimposed on his view through the windshield.
Claim 3
Dependent Claim
30 words
The head-up display of claim 1, wherein the elongated optical element has two parallel planar external surfaces, one directed toward the pilot and the other directed away from the pilot.
Claim 4
Dependent Claim
16 words
The head-up display of claim 2, wherein both of said diffractive elements are transmission diffraction gratings.
Claim 5
Dependent Claim
16 words
The head-up display of claim 2, wherein both of said diffractive elements are reflection diffraction gratings.
Claim 6
Dependent Claim
26 words
The head-up display of claim 2, wherein the first diffractive element is a transmission diffraction grating and the second diffractive element is a reflection diffraction grating.
Claim 7
Dependent Claim
26 words
The head-up display of claim 2, wherein the first diffractive element is a reflection diffraction grating and the second diffractive element is a transmission diffraction grating.
Claim 8
Dependent Claim
234 words
A head-up display for use in an aircraft cockpit having a windshield, comprising: source means for producing collimated light wavefronts of an image to be displayed to the pilot, comprising a cathode ray tube image source and means operative to collimate the image produced by the cathode ray tube image source; a relatively thin optical element having a first portion disposed to intercept the collimated light wavefronts produced by the source means, a second portion disposed in the field of view of the pilot when looking in a forward direction, and operative to transmit light wavefronts from the first portion to the second portion by total internal reflection; a first transmission diffraction grating at the first portion of the optical element, operative to diffract the collimated light wavefronts into the optical element; and a second transmission diffraction grating at the second portion of the optical element, operative to diffract the wavefronts, diffracted into the optical element by the first diffractive element, out of the optical element in the direction of the pilot's eye, the second portion of the optical element and the second transmission diffraction grating being substantially transparent to light incident the second portion of the optical element from the direction of the field of view of the pilot when looking in the forward direction, whereby the pilot views the image produced by the source means superimposed on his view through the windshield.
Claim 9
Dependent Claim
234 words
A head-up display for use in an aircraft cockpit having a windshield, comprising: source means for producing collimated light wavefronts of an image to be displayed to the pilot, comprising a cathode ray tube image source and means operative to collimate the image produced by the cathode ray tube image source; a relatively thin optical element having a first portion disposed to intercept the collimated light wavefronts produced by the source means, a second portion disposed in the field of view of the pilot when looking in a forward direction, and operative to transmit light wavefronts from the first portion to the second portion by total internal reflection; a first transmission diffraction grating at the first portion of the optical element, operative to diffract the collimated light wavefronts into the optical element; and a second transmission diffraction grating at the second portion of the optical element, operative to diffract the wavefronts, diffracted into the optical element by the first diffractive element, out of the optical element in the direction of the pilot's eye, the second portion of the optical element and the second transmission diffraction grating being substantially transparent to light incident the second portion of the optical element from the direction of the field of view of the pilot when looking in the forward direction, whereby the pilot views the image produced by the source means superimposed on his view through the windshield.
Claim 10
Dependent Claim
13 words
The head-up display of claim 7, wherein the windshield comprises the optical element.
References Cited (Backward Citations)
US4309070A
Cited
US4314283A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-12-07 | 1991-06-08 | 1991-12-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-12-07 | 1995-06-08 | 1995-12-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-12-07 | 1999-06-08 | 1999-12-08 | $7700.00 | Window Closed / Lapsed |