Digital data transmission with simultaneous transmission over a single line

Abstract: A method and apparatus for transmitting data over a power line (2) and having particular application for flight control networks. The method enables bi-directional transmission of data over either DC or AC power lines. Transformers (T₃, T₄) used for coupling data onto and from the power lines (2) comprise three windings (L₁, L₂ and L₃) and a ferrite core. Saturation of the core is avoided by arranging for the load current to flow in opposite senses through two (L₁ and L₂) of the windings. By choosing the number of turns of said two windings to be equal, complete cancellation of DC flux inside the core is possible.

Description: This invention relates to data transmission and in particular to a method and apparatus for transmitting digitally-coded data over power supply lines. This manner of data transmission is especially useful for flight control networks in aircraft. The conventional use of triplex or quadruplex systems for flight control necessitates a large number of wires running from flight control computers to the various associated actuators. Combining the power bus and data bus together cuts down the amount of necessary wiring, thus reducing the weight and bulk of the network. An object of the present invention is to provide a method and apparatus for enabling bi-directional data communication on a power supply line, which supply line may be AC or DC. One known technique for achieving communication of data in this way (and shown in fig 1) uses a transformer T₁ for coupling data from a transmitter 1 onto a power line 2. Data is extracted by a second transformer T₂ and receiver 3 further down the power line. This arrangement functions satisfactorily if the supply current is steady. If, however, there is a surge, then the cores of the transformers could be driven into saturation. When this occurs, the transformers are no longer capable of transmitting or receiving the data signal. To increase the transformers' resistance to saturation, it is possible to incorporate an air gap between the core and transformer windings. However this measure results in large and heavy devices which, in the aircraft control network application, is a disadvantage. EP-A-O 355532 discloses a bus configuration for data transfers with a power supply, where the data signals are inputted and outputted through a third winding. In this particular disclosure the power supply voltage is fed through the bus transmission lines to each item of equipment, but the induction coils are specifically disclosed and illustrated as not being wound co-axially. Similarly EP-A-O 365,696 and FR-A-2 612,019 disclose methods of utilising inductive coupling for the transmission of digital information but, as yet, no prior art has illustrated an apparatus or method which significantly reduces the physical size and mass of such apparatus by utilising co-axial data input coils, whilst eliminating the onset of core saturation. The present invention aims to provide a solution to the saturation problem without incurring a weight penalty. The invention therefore comprises apparatus for transferring digital data to and from a power line by inductive coupling, the apparatus comprising a transformer characterised in that said transformer comprises first, second and third co-axial windings, said first and second windings being wound in opposite senses whereby a first DC magnetic field generated by a current flowing in the first winding is opposed by a second DC magnetic field generated by the current flowing in the second winding. For convenience, the two inductances may be wound on a common former. Bifilar windings could be used. The former could be provided with a ferrite core. Preferably the number of turns on each of the two inductances are made substantially equal so that when current flows down the power line and through each inductance, the net magnetic flux inside the former is zero. Hence no saturation of the core can occur. The power line may carry DC or AC power. In the case of an AC supply, then the data rate must be chosen to be greater than the power supply frequency. To prevent saturation of the transformer core by the data, it is preferred that a volts x seconds balance type code is used. An example of such a code is the Manchester code which always returns to zero after each clock cycle. This has a mean voltage value of zero. Some embodiments of the invention will now be described by way of example only with reference to the drawings of which:- Figure 2 is a circuit diagram of data transmission apparatus suitable for performing the method in accordance with the invention, and Figure 3 is a circuit diagram illustrating a particular application of the invention. In Fig 2 a power line is used to transmit digital data from a transmitter 1 to a receiver 3. The transmitter and receiver are conventional logic buffers. A transformer T₃ couples data from the transmitter 1 onto the power line 2 and a second transformer T₄ detects the data and couples it into the receiver 3. The transformers T₃ and T₄ are connected in series with the power line and are of identical construction. A capacitor C₁, connected across the power line 2 shorts out any AC signal or ripple present before it can reach the transformer T₃. A second capacitor C₂ connected across the power line at a point beyond the transformer T₄ prevents the data from being transmitted any further. The power line 2, conveniently comprises a twisted pair and earthed screen. Each transformer is wound on a single former, has a ferrite core, and has three coaxial windings in total L₁, L₂, L₃. Two of the windings L₁ and L₂ are bifilar windings and have the same number of turns. These two windings carry the power and because the current flow through one of them is arranged to be in the opposite sense to that in the other, the net DC magnetic flux through the transformer core will be zero. Hence the transformers can be made small and light without the need for an air gap. The third winding L₃ is connected to the transmitter 1 or receiver 3 as appropriate. The transmitter 1 and receiver 3 may be replaced by a transceiver of a type which can be switched from a receive mode to a transmit mode. Thus bi-directional data communication is possible. Data can be transmitted true and complement and any electro-magnetic fields generated by the data itself cancel, thus producing minimal external fields. If the use of a screen as a power return is thought to be undesirable, then a third conducting line within the screen could be used for this purpose instead. The embodiment of Figure 2 may find applications in airborne systems which use, for example, the Military Standard 1553 data bus with line replaceable units requiring either AC or DC power. Other applications may be domestic, using the mains electricity supply for transmitting data to remote lighting or security locks, for example. Another application of the invention, and exemplified in Figure 3 is the transmission of data around a motor vehicle, said data being transmitted on the 12 VDC supply line. In Figure 3 data is transmitted and received by transceivers 4, 5 and 6 and transformers T₅, T₆ and T₇ by the same method as that disclosed with reference to Figure 2. Again, the cable screen is used as a power return. The transceivers are controlled by microprocessors 7, 8, and 9 respectively and data signals could usefully be employed to control, for example, trafficators, windscreen wipers and dashboard instruments etc, thus reducing the complexity and weight of necessary wiring.

Claims: Apparatus for transferring digital data to and from a power line (2) by inductive coupling, the apparatus comprising a transformer (T₃) characterised in that said transformer (T₃) comprises first, second and third co-axial windings (L₁, L₂, L₃), said first (L₁) and second (L₂) windings being wound in opposite senses whereby a first DC magnetic field generated by a current flowing in the first winding (L₁) is opposed by a second DC magnetic field generated by the current flowing in the second winding (L₂). Apparatus as claimed in Claim 1 in which the first (L₁) and second (L₂) windings are wound on a common former and have an equal number of turns. Apparatus as claimed in either preceding claim in which the digital data is encoded as a volts x seconds balance code. Apparatus as claimed in Claim 3 in which the volts x seconds balance code is a Manchester code. Apparatus as claimed in Claim 2 in which the former has a ferrite core.

Inventors: MOORE COLIN, MOORE, COLIN
Applicants: BRITISH AEROSPACE, BRITISH AEROSPACE PUBLIC LIMITED COMPANY
Application year: 1991
Main classification: H04B3
IPC codes: H04L25, H04B3