| 摘要 |
PROBLEM TO BE SOLVED: To solve defects in a conventional aircraft antenna configuration by providing an antenna assembly which fits into an opening currently existing in an air craft in a part of an aircraft body that is not conventionally used for mounting an antenna. SOLUTION: A conformal load-bearing antenna assembly comprises a pan shaped to fit within an aircraft window opening, an antenna element disposed within the pan, and a connection for coupling a signal to the antenna element. COPYRIGHT: (C)2005,JPO&NCIPI
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