CA2597403A1 - Aircraft communications system and related method for communicating between portable wireless communications device and ground - Google Patents
Aircraft communications system and related method for communicating between portable wireless communications device and ground Download PDFInfo
- Publication number
- CA2597403A1 CA2597403A1 CA002597403A CA2597403A CA2597403A1 CA 2597403 A1 CA2597403 A1 CA 2597403A1 CA 002597403 A CA002597403 A CA 002597403A CA 2597403 A CA2597403 A CA 2597403A CA 2597403 A1 CA2597403 A1 CA 2597403A1
- Authority
- CA
- Canada
- Prior art keywords
- communications
- aircraft
- access point
- transceiver
- wireless
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/18502—Airborne stations
- H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0015—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
- B64D45/0059—Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by communicating emergency situations to ground control or between crew members
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W12/00—Security arrangements; Authentication; Protecting privacy or anonymity
- H04W12/03—Protecting confidentiality, e.g. by encryption
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W88/00—Devices specially adapted for wireless communication networks, e.g. terminals, base stations or access point devices
- H04W88/08—Access point devices
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W84/00—Network topologies
- H04W84/02—Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
- H04W84/04—Large scale networks; Deep hierarchical networks
- H04W84/06—Airborne or Satellite Networks
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W84/00—Network topologies
- H04W84/02—Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
- H04W84/10—Small scale networks; Flat hierarchical networks
- H04W84/12—WLAN [Wireless Local Area Networks]
Abstract
An aircraft communications system includes a wireless local area network (LAN) access point positioned within the aircraft that receives and transmits wireless communications to and from at least one portable wireless communications device. A control panel is operatively connected to the wireless LAN access point and positioned within the flight deck of the aircraft. A communications transceiver is operative with the control panel and wireless LAN access point and operative for receiving and transmitting a communications signal between the wireless LAN access point and a ground-based transceiver. Communications between the portable wireless communications device and ground-based transceiver can be controlled from the flight deck using the control panel in one non-limiting example.
Claims (10)
1. An aircraft communications system comprising:
a wireless local area network (LAN) access point positioned within the aircraft that is adapted to receive and transmit wireless communications signals with at least one portable wireless communications device;
a control panel operatively connected to the wireless LAN
access point and positioned within the flight deck of the aircraft and controlled by a flight deck crew; and a communications transceiver operative with the control panel and wireless LAN access point and operative for receiving and transmitting a communications signal between the wireless LAN access point and a ground-based transceiver for allowing air-to-ground communications.
a wireless local area network (LAN) access point positioned within the aircraft that is adapted to receive and transmit wireless communications signals with at least one portable wireless communications device;
a control panel operatively connected to the wireless LAN
access point and positioned within the flight deck of the aircraft and controlled by a flight deck crew; and a communications transceiver operative with the control panel and wireless LAN access point and operative for receiving and transmitting a communications signal between the wireless LAN access point and a ground-based transceiver for allowing air-to-ground communications.
2. An aircraft communications system according to claim 1 wherein said wireless LAN access point comprises a communications module that is integrated within said control panel.
3. An aircraft communications system according to claim 1 wherein said communications transceiver is operative for communicating with a scrambling ICE aircraft.
4. An aircraft communications system according to claim 1 wherein said communications transceiver comprises one of a HF, VHF or UHF transceiver.
5. An aircraft communications system according to claim 1, and further comprising a mission operations center that receives and transmits a communications signal to and from the communications transceiver positioned on the aircraft.
6. An aircraft communications system according to claim 1 wherein said control panel includes an aural or visual alert indicative of a wireless transmission of a communication signal from the at least one portable wireless communications device.
7. An aircraft communications system according to claim 1, wherein said WLAN access point is operative to transmit and receive communications signals in accordance with a Voice over Internet Protocol (VoIP).
8. A method of communicating between an aircraft and ground, which comprises:
transmitting a communications signal between a wireless local area network (LAN) access point positioned within the aircraft and at least one portable wireless communications device positioned within the aircraft;
transmitting the communications signal between a ground-based communications transceiver and a communications transceiver on the aircraft that is operatively connected to the wireless LAN access point; and controlling the communications signals to and from the portable wireless communications device and the ground-based transceiver and the communications transceiver on the aircraft through a control panel located in the flight deck.
transmitting a communications signal between a wireless local area network (LAN) access point positioned within the aircraft and at least one portable wireless communications device positioned within the aircraft;
transmitting the communications signal between a ground-based communications transceiver and a communications transceiver on the aircraft that is operatively connected to the wireless LAN access point; and controlling the communications signals to and from the portable wireless communications device and the ground-based transceiver and the communications transceiver on the aircraft through a control panel located in the flight deck.
9. A method according to claim 8 and which further comprises integrating the wireless LAN access point within the control panel as a communications module.
10. A method according to claim 8 and which further comprises indicating a wireless transmission of a communications signal from a portable wireless communications device on the aircraft by indicating an aural or visual alert at the control panel in the flight deck.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US65216605P | 2005-02-11 | 2005-02-11 | |
US60/652,166 | 2005-02-11 | ||
US11/158,575 US7328012B2 (en) | 2005-02-11 | 2005-06-22 | Aircraft communications system and related method for communicating between portable wireless communications device and ground |
US11/158,575 | 2005-06-22 | ||
PCT/US2006/003988 WO2006086259A2 (en) | 2005-02-11 | 2006-02-06 | Aircraft communications system and related method for communicating between portable wireless communications device and ground |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2597403A1 true CA2597403A1 (en) | 2006-08-17 |
CA2597403C CA2597403C (en) | 2010-04-13 |
Family
ID=36793588
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2597403A Active CA2597403C (en) | 2005-02-11 | 2006-02-06 | Aircraft communications system and related method for communicating between portable wireless communications device and ground |
Country Status (7)
Country | Link |
---|---|
US (1) | US7328012B2 (en) |
EP (1) | EP1854311B8 (en) |
JP (1) | JP4642866B2 (en) |
CN (1) | CN101156468B (en) |
CA (1) | CA2597403C (en) |
TW (1) | TWI336456B (en) |
WO (1) | WO2006086259A2 (en) |
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2005
- 2005-06-22 US US11/158,575 patent/US7328012B2/en active Active
-
2006
- 2006-02-06 JP JP2007555143A patent/JP4642866B2/en not_active Expired - Fee Related
- 2006-02-06 WO PCT/US2006/003988 patent/WO2006086259A2/en active Application Filing
- 2006-02-06 CA CA2597403A patent/CA2597403C/en active Active
- 2006-02-06 EP EP06748191.1A patent/EP1854311B8/en active Active
- 2006-02-06 CN CN2006800115085A patent/CN101156468B/en not_active Expired - Fee Related
- 2006-02-10 TW TW095104653A patent/TWI336456B/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CN101156468A (en) | 2008-04-02 |
US7328012B2 (en) | 2008-02-05 |
TW200704213A (en) | 2007-01-16 |
WO2006086259A3 (en) | 2007-01-04 |
JP4642866B2 (en) | 2011-03-02 |
CN101156468B (en) | 2011-04-13 |
EP1854311A2 (en) | 2007-11-14 |
CA2597403C (en) | 2010-04-13 |
US20060183474A1 (en) | 2006-08-17 |
WO2006086259A2 (en) | 2006-08-17 |
WO2006086259A8 (en) | 2007-09-20 |
EP1854311B8 (en) | 2014-10-29 |
TWI336456B (en) | 2011-01-21 |
JP2008545283A (en) | 2008-12-11 |
EP1854311B1 (en) | 2014-10-08 |
EP1854311A4 (en) | 2012-10-10 |
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