Aeronautics and astronautics – Aircraft structure – Details
Patent
1996-09-09
1998-06-02
Mojica, Virna Lissi
Aeronautics and astronautics
Aircraft structure
Details
244132, 244133, 244117A, 89 1817, B64C 112, B64C 3000
Patent
active
057588457
ABSTRACT:
A vehicle having a ceramic radome includes a vehicle body having an opening therein, a ceramic radome sized to cover the opening of the vehicle body, and an attachment structure joining the radome to the vehicle body to cover the opening. The attachment structure has a substantially cylindrically symmetric compliant metallic transition element disposed structurally between the radome and the body. The radome is joined to a first end of the transition element by a first brazed butt-joint. A primary seal is disposed between the transition element and the vehicle body. A spanner nut overlies the transition element and has a first engagement to the transition element. A threaded engagement between the spanner nut and the vehicle body allows the radome/transition element assembly to be attached and tightened to the vehicle body and to be later removed.
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Ek Eric
Sunne Wayne
Alkov Leonard A.
Collins David W.
Lenzen, Jr. Glenn H.
Mojica Virna Lissi
Raytheon Company
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