Radio frequency (RF) feedthrough system and method

• US 9,882,270 B2
• Filed: 02/07/2017
• Issued: 01/30/2018
• Est. Priority Date: 05/12/2015
• Status: Active Grant

• Current Assignee: Appareo Systems LLC (AGCO Corporation)
• Original Assignee: Appareo Systems LLC (AGCO Corporation)
• Inventors: Allen, Robert M., Thurow, Bradley R., Johnson, Jeffrey L.
• Primary Examiner(s): AKINYEMI, AJIBOLA A
• Application Number:
  US15/426,975
• Publication Number:
  US 20170149122A1
• Time in Patent Office: 357 Days
• Field of Search: 455 901
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H04B 1/082 to be used in vehicles H04B1/086 takes precedence; holding or mounting accessories B60R11/02
• CPC Class Codes: H04B 1/3822 specially adapted for use in vehicles H04B1/3827 takes precedence
• CPC Class Codes: H04B 1/525 with means for reducing leakage of transmitter signal into the receiver
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An aviation transponder system comprising a permanently-mounted antenna, a permanently-mounted receiver module comprising a receiver, a signal splitter, and an external connector, and a portable receiver module, wherein a signal received on the permanently-mounted antenna is passed to the signal splitter of the permanently-mounted receiver module, wherein the signal splitter splits the signal such that the signal is sent to both the receiver and to the external connector, and wherein the portable receiver module is connected to the external connector, whereby the permanently-mounted antenna is used by the receiver of the permanently-mounted receiver module and fed through the permanently-mounted receiver module and made available to the portable receiver module through the external connector.

Claims

1. An aviation transponder system comprising:

a permanently-mounted antenna;

a circulator connected to said antenna;

a signal splitter connected to said circulator;

a receiver connected to said signal splitter;

said circulator selectively directing received signals whereby the receiver is selectively isolated from high-power transmitted signals;

a plurality of PIN limiter diodes directly connected to the circulator and adapted for limiting current passing from said permanently-mounted antenna to said receiver in said second mode of operation;

said permanently-mounted antenna, said permanently-mounted receiver module and the circulator comprising an aviation transponder system; and

said transponder system being configured for adding an external portable device that can receive input information from an existing antenna and send output information to a display unit.

2. The aviation transponder system of claim 1, which includes:

an external connector connecting the signal splitter with the receiver; and

wherein the permanently-mounted antenna is used by the receiver and received RF signals are fed through the external connector to the receiver.

3. The aviation transponder system of claim 1, wherein the receiver is permanently-mounted.

4. The aviation transponder system of claim 1, wherein the receiver is portable.

5. The aviation transponder system of claim 1 wherein the receiver is a communications (COM) receiver.

6. The aviation transponder system of claim 1, which includes:

the receiver comprising a permanently-mounted navigation (NAV) receiver; and

a portable receiver comprising a portable navigation (NAV) receiver.

7. The aviation transponder system of claim 6, wherein the permanently-mounted receiver is an ADS-B receiver and the portable receiver is a portable ADS-B receiver.

8. The aviation transponder system of claim 6, wherein the receivers are equipped with Global Navigation Satellite Systems (GNSSs).

9. The aviation transponder system of claim 1, which includes:

said circulator having operating modes configured for;

a) sending signals from the transmitter to the permanently-mounted antenna in a first mode of operation; and

b) taking signals received on the external antenna and routing them to the receiver in a second mode of operation.

10. An aviation transponder system comprising:

a permanently-mounted antenna;

a circulator connected to said antenna;

a signal splitter connected to said circulator;

a receiver connected to said signal splitter;

said circulator selectively directing received signals whereby the receiver is selectively isolated from high-power transmitted signals;

an external connector connecting the signal splitter with the receiver;

the permanently-mounted antenna being used by the receiver and received RF signals being fed through the external connector to the receiver;

said receiver being GNSS-equipped;

said circulator having operating modes configured for;

a) sending signals from the transmitter to the permanently-mounted antenna in a first mode of operation; and

b) taking signals received on the external antenna and routing them to the receiver in a second mode of operation;

a plurality of PIN limiter diodes directly connected to the circulator and adapted for limiting current passing from said permanently-mounted antenna to said receiver in said second mode of operation;

said permanently-mounted antenna, said permanently-mounted receiver and the circulator comprising an aviation transponder system; and

said transponder system being configured for adding an external portable device that can receive input information from an existing antenna and send output information to a display unit.

11. The aviation transponder system of claim 10, wherein the receiver is permanently-mounted.

12. The aviation transponder system of claim 10, wherein the receiver is portable.

13. The aviation transponder system of claim 10, wherein the receiver is a communications (COM) receiver.

14. The aviation transponder system of claim 10, which includes:

the receiver comprising a permanently-mounted navigation (NAV) receiver; and

a portable receiver comprising a portable navigation (NAV) receiver.

15. The aviation transponder system of claim 14, wherein the receivers are ADS-B receivers.

16. A method of passing RF signals through a transponder, which includes the steps of:

providing said transponder with a permanently-mounted antenna;

providing a circulator connected to said antenna;

providing a signal splitter connected to said circulator;

providing a receiver connected to said signal splitter;

providing an external connector connected to said signal splitter;

providing a receiver connected to said signal splitter through said external connector, said receiver being adapted for receiving RF signals from said signal splitter through said external connector;

providing a plurality of PIN limiter diodes directly connected to the circulator and adapted for limiting current passing from said permanently-mounted antenna to said receiver in said second mode of operation;

providing said permanently-mounted antenna, said permanently-mounted receiver and the circulator comprising an aviation transponder system; and

providing said transponder system being configured for adding an external portable device that can receive input information from an existing antenna and send output information to a display unit.

17. The method according to claim 16, which includes the additional steps of:

providing a GNSS component in said transponder; and

deriving GNSS-based positions with said GNSS component.