Method and apparatus for determining an interfering field strength in an aircraft
View Patent ↗The disclosed embodiments relates to a method and an apparatus for determining the interfering field strength in an aircraft and the impairment of an electric system in the aircraft including cables between the outer shell and the interior panelling of the fuselage for transmitting signals within the aircraft. In order to enable direct and reliable determination of interfering field strength in an aircraft and assessment of the electromagnetic vulnerability of the communications system in the aircraft depending on the results of the determination, either a predetermined transmission signal is fed in at least one leaky line between outer shell and panelling of the fuselage and the reception signal that is irradiated by the leaky line is received with a receiver, or a predetermined transmission signal is transmitted with a transmitter and the reception signal is extracted from the leaky line. Subsequently the amplitudes of the transmission and the reception signals are compared with each other.
1. A method for determining an interfering field strength in an aircraft and an impairment of an electric system in the aircraft comprising cables between an outer shell and a panelling of the aircraft fuselage for transmitting signals in the aircraft, the method comprising:
either feeding a predetermined transmission signal in at least one leaky line between the outer shell and panelling of the fuselage and receiving with a receiver a reception signal that is irradiated by the at least one leaky line,
or transmitting a predetermined transmission signal with a transmitter and extracting a reception signal from the leaky line and
comparing amplitudes of the transmission and the reception signals.
2. Method according to claim 1 wherein additionally amplitudes of detected data with and without the panelling are compared to each other.
3. Method according to claim 1 , wherein the amplitude of the transmission signal and/or the reception signal is calibrated in V/m.
4. An apparatus for determining an interfering field strength in an aircraft and an impairment of an electric system in the aircraft comprising:
at least one leaky line between an outer shell and a panelling of a fuselage,
at least one transmitter for transmitting a predetermined transmission signal and
at least one receiver for receiving an irradiation signal, wherein
either the transmitter is coupled to the leaky line for feeding the predetermined transmission signal in the leaky line,
or the receiver is coupled to the leaky line for extracting a reception signal from the leaky line and
a comparator for comparing the amplitudes of the transmission and reception signals.
5. Apparatus according to claim 4 , wherein the comparator is a two-port network analyzer.
6. Apparatus according to claim 4 , wherein the antenna of the receiver comprises a leaky line.
7. Apparatus according to claim 4 , wherein the receiver comprises a mobile antenna, the geometrical dimensions of which are small in comparison to the longitudinal dimension of the leaky line.
8. Apparatus according to claim 4 , wherein an assemblage of leaky lines is disposed in the aircraft between the outer shell and panelling in parallel to the aircraft axis.
9. Apparatus according to claim 8 , wherein the leaky lines are uniformly distributed over the circumference of the fuselage and pairs of adjacent leaky lines mutually have an identical distance from each other.
10. Apparatus according to claim 8 , wherein transverse lines are disposed in addition to the assemblage of leaky lines in parallel to the aircraft axis so as to subdivide the fuselage into a grid of longitude and latitude coordinates.
11. Apparatus according to claim 8 wherein the individual leaky lines are each coupled to an individual transmitter or receiver.