Method and apparatus for wireless electromagnetic communication within a contained electromagnetic field

• US 5,230,085 A
• Filed: 04/05/1991
• Issued: 07/20/1993
• Est. Priority Date: 04/05/1991
• Status: Expired due to Fees

• Current Assignee: E-Systems Incorporated (Rtx Corporation)
• Original Assignee: E-Systems Incorporated (Rtx Corporation)
• Inventors: Loposer, Thomas L.
• Primary Examiner(s): Pascal, Robert J.
• Assistant Examiner(s): Lee, Benny T.
• Application Number:
  US07/680,743
• Time in Patent Office: 837 Days
• Field of Search: 333/236, 333/237, 333/240, 333/245, 343/705, 343/711, 343/719, 343/905, 455/41, 455/55, 455/14, 455/15, 379/55
• US Class Current: 455/41.2
• CPC Class Codes: H04B 5/266 One coil at each side, e.g. with primary and secondary coils
• CPC Class Codes: H04B 5/48 Transceivers

Abstract

Wireless electromagnetic communication between a primary transceiver and one or more secondary transceivers located within an enclosed structure may be effectuated by forming a multi-conductor electromagnetic transmission line within the structure. Communications are effectuated by utilizing the enclosing structure itself as one conductor in a multi-conductor transmission line. One or more other conductors are then placed within and insulated from the structure to complete the communications transmission line. A primary communications transceiver and a matched terminating load are connected to the ends of the transmission line to form a contained electromagnetic field. Use of a matched terminating load minimizes standing waves and provides for substantially constant electromagnetic field strength within the structure. Each secondary transceiver located within the contained electromagnetic field communicates with other secondary transceivers or the primary transceiver by inserting or extracting electromagnetic energy from the transmission line.

Claims

1. A method for electromagnetic communication within an enclosed conductive vehicle fuselage comprising the steps of:

disposing a conductive line supported within and insulated from the conductive vehicle fuselage to form a multi-conductor electromagnetic transmission line within the conductive fuselage wherein the conductive structure comprises one conductor of the multi-conductor transmission line and the conductive line comprises another conductor;

coupling a primary transceiver between the conductive fuselage and the conductive line of said multi-conductor transmission line;

terminating the multi-conductor transmission line with a matched load impedance coupled between the conductive fuselage and the conductive line; and

positioning at least one secondary transceiver within the conductive fuselage for communication with the primary transceiver by means of said multi-conductor transmission line.

2. The method of electromagnetic communications as in claim 1 wherein the step of forming a multi-conductor electromagnetic transmission line includes forming a transmission line within an aircraft fuselage.

3. An electromagnetic communication system for transmission and reception of communication signals within a conductive vehicle fuselage, comprising:

a multi-conductor transmission line wherein the fuselage comprises an outer conductor of said transmission line and wherein said transmission line further includes an inner conductor positioned within an insulated from said fuselage;

a matched load impedance coupled to the multi-conductor transmission line between the fuselage and the inner conductor;

first transceiver means coupled to the multi-conductor transmission line between the fuselage and the inner conductor; and

at least one second transceiver means positioned within the fuselage for communication with the first transceiver means over said multi-conductor transmission line.

4. The electromagnetic communications system as in claim 3 wherein the conductive vehicle fuselage comprises an aircraft fuselage.

5. Apparatus for electromagnetic communication comprising an electrically conductive metallic enclosure and a conducting element insulated from and supported within the metallic enclosure, said metallic enclosure and said conducting element jointly defining a multi-conductor electromagnetic transmission line having a characteristic impedance, a primary radio frequency transceiver connected between the metallic enclosure and said conducting element, a terminating impedance load connected between the metallic enclosure and said conducting element, wherein the impedance of said terminating impedance matches the characteristic impedance of the transmission line, and at least one secondary transceiver positioned within the metallic enclosure for communications over the multi-conductor transmission line with the primary transceiver.

6. The apparatus for electromagnetic communications as in claim 5 wherein the metallic enclosure comprises the metallic enclosure for a transport vehicle.

7. A method for providing radio communications between a primary transceiver and at least one secondary transceiver located within an enclosing metallic structure for a transport vehicle, comprising the steps of:

disposing a conductor supported within and insulated from the metallic structure of the transport vehicle to form a multi-conductor transmission line comprised of the enclosing metallic structure and the conductor supported and insulated from the structure;

coupling the primary transceiver between the metallic structure and a first end of said conductor;

coupling a matched load impedance to the transmission line between the metallic structure and a second end of said conductor; and

positioning each secondary transceiver within the enclosing metallic structure of the transport vehicle to communicate with the primary transceiver over the transmission line.

8. An electromagnetic communication system for radio frequency communications between a primary transceiver and at least one secondary transceiver positioned within a metallic structure for a transport vehicle, comprising:

a multi-conductor electromagnetic transmission line, the metallic structure of the transport vehicle comprising a first conductor of said transmission line, and wherein said transmission line further includes a second conductor positioned within and insulated from the metallic structure;

a matched load impedance connected between the metallic structure and the second conductor;

means for connecting the primary transceiver between the metallic structure and the second conductor, whereby the primary transceiver and each secondary transceiver positioned within the transport vehicle communicate by means of the multi-conductor transmission line.

9. The electromagnetic communications systems as in claim 8 wherein in response to an electromagnetic wave generated by the primary transceiver, the multi-conductor transmission line and the matched load impedance propagates an electromagnetic field which is contained within the metallic structure.

10. The electromagnetic communications systems as in claim 9 wherein the contained electromagnetic field has a substantially uniform field strength.

11. The electromagnetic communications systems as in claim 9 wherein the contained electromagnetic field generated within the metallic structure has a substantially minimal standing wave ratio.

12. The electromagnetic communications system as in claim 8 wherein the metallic structure comprises a fuselage and the transport vehicle comprises an aircraft.