Telecommunications – Radiotelephone system – Zoned or cellular telephone system
Reexamination Certificate
1998-12-21
2001-07-31
Trost, William (Department: 2683)
Telecommunications
Radiotelephone system
Zoned or cellular telephone system
C455S427000, C455S574000
Reexamination Certificate
active
06269243
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a device for allowing the use in an aircraft of at least one personal radiocommunication means.
Although the present invention is more particularly appropriate to a mobile telephone, that is to say to a self-contained telecommunication device based on communication techniques used by cellular networks, it can also be applied to other radiocommunication means, such as for example portable computer terminals. In a known manner, such portable terminals make it possible to effect a computer communication, by virtue of their connection to computer networks with the aid of built-in radio modems.
2. Description of the Related Art
It is known that mobile telephones, whose numbers have greatly increased in a short space of time, on account of reduced purchase price and affordable communication costs, are prohibited from use on board aircraft, especially civil transport aircraft, for safety reasons. This prohibition is in fact necessary in order to avoid any electromagnetic interference with electronic systems on board the aircraft, which may occur because the radiocommunication means necessarily operates at high power so that it can be picked up from outside, such interference possibly being, of course, very damaging, in particular during the takeoff and landing of the aircraft.
Additionally, when the passengers of a transport aircraft wish to communicate with their usual contacts, they have to use communication systems provided, if relevant, for this purpose on the aircraft.
Thus, as regards for example telephone communications, specific handsets with which aircraft are generally equipped are often made available to passengers to allow them to call the subscribers of the terrestrial telephone network.
The means of radiocommunication employed for this purpose use:
either geostationary satellites;
or radiocommunication installations provided on the ground and intended for air transport.
Moreover, specific installations have to be set up on the ground in order to cooperate with these radiocommunication means, and especially to transmit telephone communications to the persons called.
On the other hand, it is not possible for a subscriber located on the ground to call a passenger in the aircraft, in particular on account of complex procedures for transmitting a call to said passenger on board the aircraft.
The aforesaid solutions are therefore unsatisfactory, especially since they use complex and expensive installations intended first and foremost for air transport, thus entailing an extremely high communication cost.
Moreover, these solutions have the following drawbacks:
communication means which use ground installations have only limited geographical coverage. Moreover, since several communication systems of different types are in existence, various appropriate items of equipment are necessary on the aircraft to obtain a satisfactory communication field; and
communication means which use geostationary satellites do not have worldwide coverage (the polar regions are, for example, not covered) and the limited number of available channels reduces the communication capacities.
SUMMARY OF THE INVENTION
The object of the present invention is to remedy these drawbacks. It relates to a simple and inexpensive device for allowing the use in a standard and risk-free manner, in an aircraft, of at least one personal radiocommunication means of the type alluded to above, in particular a mobile telephone.
For this purpose, according to the invention, said device is noteworthy in that it comprises:
at least one first antenna able to transmit and pick up, outside the aircraft, electromagnetic waves respectively picked up and transmitted by satellite networks or ground networks, called outside networks;
at least one second antenna able to transmit and pick up, inside the aircraft, electromagnetic waves respectively picked up and transmitted by a passenger's radiocommunication means; and
a transponder which comprises :
a first electromagnetic wave transmission and reception system coupled to said first antenna;
a second electromagnetic wave transmission and reception system coupled to said second antenna;
a central unit which sends, if relevant after matching, signals received by one of said first and second transmission and reception systems to the other transmission and reception system; and
means of authority for compelling said radiocommunication means to operate at reduced power and for controlling the operation thereof.
Thus, by virtue of the invention, any passenger in the aircraft can use a personal radiocommunication means, for example a mobile telephone or a portable terminal, that is to say he can connect up to a telephone network, under the same conditions of service as if he were located on land in his office or his car, and do so without danger of interference with on-board electronic systems, since the operating power of said radiocommunication means is lowered in such a way as not to allow such interference.
Moreover, by virtue of said device in accordance with the invention, the possessor of such a radiocommunication means can not only call an opposite party, but also be called on his personal number, under the same conditions as on the ground, this being irrespective of the geographical position of the aircraft. In particular, said radiocommunication means operates in a standard manner and such operation requires no structural or functional modification thereof.
Within the framework of the present invention, the term transponder is understood to mean any device which makes it possible to establish bidirectional communications between two distinct radio-frequency networks, in this instance said outside network and a radio-frequency network created inside the aircraft by said second antenna and said second transmission and reception system.
Stated otherwise, said transponder makes it possible to create on board the aircraft an environment which is compatible with the collection of radiocommunication means (mobile telephones, etc.) present on board, and to transform this environment, outside the aircraft, into an environment which is compatible with constellations of satellites and/or ground installations forming part of said telephone network.
Moreover, advantageously, said means of authority:
act, by way of said second transmission and reception system and said second antenna, if relevant on a power auto-matching system built into said radiocommunication means; and/or
are built into said central unit, thus making it possible to simplify the device in accordance with the invention.
Furthermore, said device advantageously comprises, for radiocommunication means furnished with accumulator batteries and systems for the electrical charging of batteries, at least one electrical supply means provided in proximity to a passenger seat of the aircraft, it being possible for the electrical charging system of a radiocommunication means to be plugged, with a view to the charging thereof into said electrical supply means.
Moreover, advantageously, said device also comprises a disabling means built, for example, into the central unit and able to transmit inside the aircraft, in the form of electromagnetic waves, transmission prohibition commands to a radiocommunication means, so as to prevent the use of said radiocommunication means when this proves necessary, especially for safety reasons, that is to say essentially at low altitudes in order to minimize any risk of conflict with existing terrestrial cellular telephone networks.
Of course, by virtue of the invention, this prohibition of use is much reduced and is generally limited to a few minutes during the takeoff and landing phases.
REFERENCES:
patent: 5438610 (1995-08-01), Bhagat et al.
patent: 5519761 (1996-05-01), Gilbousen
patent: 5878345 (1999-03-01), Ray et al.
patent: 6002929 (1999-12-01), Bishop et al.
patent: 6002944 (1999-12-01), Beyda
patent: 6047165 (2000-04-01), Wright et al.
patent: 6055425 (2000-04-01), Sinivaara
patent: 6061562 (2000-05-01),
Corbefin Rene
Lemozit Christian
Aerospatiale - Societe Nationale Industrielle
Gesesse Tilahun
Stevens Davis Miller & Mosher LLP
Trost William
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