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US3300777A Expired / Lapsed US ⏱️ 0.0 years remaining

Visual identification of aircraft

Assignee: BAC AND BRITISH AEROSPACE
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Filing: 1964-10-26
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Granted: 1967-01-24
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Expires: 1984-10-26
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Abstract

Abstract 1,021,867. Television. ENGLISH ELECTRIC AVIATION Ltd. Oct. 28, 1964 [Oct. 28, 1963], No. 42504/63. Heading H4F. An aircraft having in its airframe a window 9 which is transparent to visible and infra-red radiation from an object to be identified, e.g. a foreign aircraft 3, has mounted within the airframe an angularly adjustable plane reflector 8 arranged to reflect radiation passing through the window, a radar or infra-red tracking equipment 4, 5 for following the course of the object to be identified, a servo-mechanism 6 controlled by the tracking equipment to drive the reflector 8 through an angle which is half the relative angular movement of the object so that the beam of radiant energy received from the object is reflected along a fixed path to a telescope objective 11, e.g. a parabolic mirror, from where it is reflected back through holes in the centre of the reflector 8 and servomechanism 6 and focused directly on to the photo-cathode of a vidicon camera 12. A receiver 14 may be connected by a closed circuit television link 13 to camera 12, the receiver having a manual control 15 for centralization, by way of further servo-commands, and magnification of the image. The dimensions of the object may be ascertained by comparison with a scale superimposed electroncally on the display, the overall magnification being known and the range of the object being available in the radar. In a further embodiment, Fig. 2, shown, a laser is used to illuminate the object, its narrow coherent light beam passing through a hole in mirror 11 and being reflected from plane mirror 8 on to the object.

Inventors

  • 👤 Tarr Richard James Clifford

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 11:33
CPC Classifications
G; G01; G01S; G01S7/00; G01S7/02; G01S7/04; G01S7/06; G01S13/00; G01S13/66; G01S13/68; G01S13/86; G01S13/865; G01S13/867

Claims Analysis

Total Claims: 1
Claim 1
Independent Claim 197 words
AN AIRCRAFT HAVING AN OPTICALLY FLAT GLASS PLATE SUBSTANTIALLY FLUSH WITH THE SURFACE OF THE AIRCRAFT BODY, AN ANGULARLY ADJUSTABLE PLANE REFLECTOR WHICH IS ARRANGED TO REFLECT RADIATION PASSING THROUGH THE SAID GLASS PLATE, RADAR TRACKING EQUIPMENT FOR FOLLOWING THE COURSE OF THE OBJECT TO BE IDENTIFIED, A SERVO MECHANISM CONTROLLED BY THE TRACKING EQUIPMENT TO STEER THE REFLECTOR SO THAT RADIATION RECEIVED FROM THE OBJECT IS REFLECTIVE ALONG A FIXED PATH WITHIN AND RELATIVE TO THE SAID AIRCRAFT BODY, A TELESCOPE FIXED WITH RESPECT TO THE AIRFRAME AND HAVING ITS OPTICAL AXIS COINCIDENT WITH THE FIXED PATH OF REFLECTED RADIATION ESTABLISHED BY THE SAID REFLECTOR, THE TELESCOPE INCLUDING A PARABOLIC MIRROR, AN ELECTRONIC CAMERA TUBE FIXED WITH RESPECT TO THE SAID AIRCRAFT BODY AND MOUNTED WITH ITS PHOTOCATHODE IN THE FOCAL PLANE OF THE PARABOLIC MIRROR, FOR PROVIDING A TELEVISION SIGNAL REPRESENTING AN IMAGE OF THE OBJECT, A TELEVISION RECEIVER ARRANGED FOR OBSERVATION WITHIN THE CRAFT, AND CLOSED CIRCUIT TELEVISION LINK CONNECTING THE CAMERA TUBE TO THE RECEIVER, A MANUAL CONTROL FOR CENTRALIZING THE IMAGE OF THE OBJECT ON THE RECEIVER, AND MANUAL MEANS FOR CONTROLLING THE ELECTRONIC MAGNIFICATION OF THE IMAGE DISPLAYED BY THE RECEIVER.

References Cited (Backward Citations)

US2705319A Cited
US3019292A Cited
US3053932A Cited
US3211046A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1970-01-23 1970-07-25 1971-01-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1974-01-23 1974-07-25 1975-01-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1978-01-23 1978-07-25 1979-01-24 $7700.00 Window Closed / Lapsed

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