IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0141024
(2002-05-08)
|
발명자
/ 주소 |
- White, III, Orland Kermit
|
출원인 / 주소 |
- Lockheed Martin Corporation
|
대리인 / 주소 |
Bracewell & Patterson, L.L.P.
|
인용정보 |
피인용 횟수 :
10 인용 특허 :
4 |
초록
▼
A data network includes a plurality of network devices, a plurality of physical. transmission lines each coupled to a respective one of said plurality of network devices, and a network hub coupled to each of said plurality of physical transmission lines. The network hub has a removable and replaceab
A data network includes a plurality of network devices, a plurality of physical. transmission lines each coupled to a respective one of said plurality of network devices, and a network hub coupled to each of said plurality of physical transmission lines. The network hub has a removable and replaceable termination element providing signal connectivity between selected ones of said plurality of transmission lines. In one embodiment, the data network is installed within an aircraft including a fuselage, an empennage connected to the fuselage, a lift-generating surface coupled to the fuselage, and at least one engine for propelling the aircraft.
대표청구항
▼
A data network includes a plurality of network devices, a plurality of physical. transmission lines each coupled to a respective one of said plurality of network devices, and a network hub coupled to each of said plurality of physical transmission lines. The network hub has a removable and replaceab
A data network includes a plurality of network devices, a plurality of physical. transmission lines each coupled to a respective one of said plurality of network devices, and a network hub coupled to each of said plurality of physical transmission lines. The network hub has a removable and replaceable termination element providing signal connectivity between selected ones of said plurality of transmission lines. In one embodiment, the data network is installed within an aircraft including a fuselage, an empennage connected to the fuselage, a lift-generating surface coupled to the fuselage, and at least one engine for propelling the aircraft. 5752638, 19980500, Meeks, 211/070.5; US-5775557, 19980700, Arvidsson; US-5806735, 19980900, Christiansson et al.; US-5826767, 19981000, Chimenti et al.; US-5827036, 19981000, Steffes et al.; US-5845828, 19981200, Settelmayer; US-5850891, 19981200, Olms et al.; US-5884824, 19990300, Spring, Jr.; US-D412882, 19990800, Lundgren; US-5931362, 19990800, Chimenti; US-5951231, 19990900, Allen; US-D416855, 19991100, Englander; US-6000593, 19991200, Chimenti; US-6010048, 20000100, Settelmayer; US-6015074, 20000100, Snavely et al.; US-D422553, 20000400, VonDuyke; US-6085954, 20000700, Bloemer et al.; US-6092972, 20000700, Levi, 224/310; US-6131781, 20001000, Murray; US-6164507, 20001200, Dean et al.; US-6179543, 20010100, Adame et al., 224/310; US-6360930, 20020300, Flickenger, 118/314; US-6427889, 20020800, Levi, 224/315; US-6428263, 20020800, Schellens, 414/462
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