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Steerable windowed enclosuresA gyro-stabilized mechanism that is to be carried on a vehicle, such as a helicopter, is provided with a protective enclosure consisting of a dome, usually of glass fibre reinforced plastic. The dome must be provided with a window transparent to the radiation involved, and this must be steered with the mechanism so that they remain in register with one another. Prior art structures employ elongated windows of sufficiently large size to accommodate the tilting and rolling of the mechanism, while pan movements are accommodated by rotating the entire dome. The invention provides a structure employing a small window that can be steered or slaved with the mechanism by rotation of the part of the dome including the window relative to the other part, which has the pan or yaw rotation motor connected to it. This rotation between the dome parts takes place in a skew plane disposed at as small a skew angle to the vertical as is possible, the compensation for the resulting transverse movement of the window being effected by a programmed rotation of the dome about the pan axis. Optically flat glass can then be used for the window, it can be coated to reduce reflections, etc, and it can also be wiped in operation to remove moisture. A broadcast antenna can be mounted on the part of the dome out of the line-of-sight of the apparatus.
Document ID
19910021828
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
John N Leavitt
(International Superconductivity Technology Center Kawasaki, Japan)
Date Acquired
August 14, 2013
Publication Date
April 11, 1989
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Avionics and Aircraft Instrumentation
Report/Patent Number
Patent Number: INT-PATENT-1-262-653
Accession Number
91N31142
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
4,821,043 | CA 1261653
Patent Application
107,438 | CA 521276
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