Aircraft anti-theft system

• US 5,479,162 A
• Filed: 07/09/1993
• Issued: 12/26/1995
• Est. Priority Date: 07/09/1993
• Status: Expired due to Fees

• Current Assignee: Hawker Beechcraft Services (Textron Inc)
• Original Assignee: United Beechcraft, Inc.
• Inventors: Barger, Randall R., Saliga, Thomas V.
• Primary Examiner(s): Peng, John K.
• Assistant Examiner(s): Lee, Benjamin C.
• Application Number:
  US08/089,299
• Time in Patent Office: 900 Days
• Field of Search: 340/945, 340/541, 340/426, 340/428, 340/430, 340/310.02, 340/310.03, 340/538, 340/825.31, 340/825.32, 307/10.3, 307/10.4, 307/10.5, 307/10.6, 361/171, 361/172, 180/270, 180/287
• US Class Current: 340/945
• CPC Class Codes: B60R 25/04 operating on the propulsion system, e.g. engine or drive motor
• CPC Class Codes: B60R 25/2009 Antitheft state indicator
• CPC Class Codes: B60R 25/25 using biometry
• CPC Class Codes: B60R 25/252 Fingerprint recognition

Abstract

An anti-theft system that can be retrofitted onto existing aircraft disables the starter motor of an engine or engines a predetermined time after the aircraft is taken out of service and re-enables starting only after the pilot has provided adequate identification (e.g. by entering a personal identification number at a cockpit keyboard). The predetermined time interval is selected to be long enough to ensure that the system does not impose a flight hazard by preventing in-flight re-starts. In a preferred version of the system, a drop in the output voltage of the aircraft'"'"'s main electric power system is used as an indication that the aircraft is out of service. To simplify installation on existing aircraft, the system provides for communication among various functional elements over a pre-existing part of the aircraft (e.g. by imposing AC tones on a starter motor control line).

Claims

1. An anti-theft system installed on an aircraft comprising a pressurized cabin separated from other portions of the aircraft by a plurality of bulkheads, a main electric power system supplied by a starting battery or by a generator driven by an engine, and a starter control line having a first end connected to a start switch within the cabin and a second end connected to a starter relay located intermediate the cabin and the engine, the engine being startable by an electric starter motor powered by the main electric power system when the starter relay operates the starter motor, the system installed without penetrating any of the bulkheads, the system comprising:

operator-identification apparatus situated within the cabin, the operator-identification apparatus generating an input code, the operator-identification apparatus operatively connected to a first communication apparatus situated within the cabin and in turn operatively connected to the first end of the starter control line, and

a second communication apparatus connected to the second end of the starter control line, the second communication apparatus controlling a starter relay control apparatus having a first, locked, state in which the relay is prohibited from operating the starter motor, the starter relay control apparatus having a second, unlocked, state in which the relay operates the starter motor

wherein the first communication apparatus sends a first code signal, corresponding to the input code, as an alternating electric voltage on the starter control line, to the second communication apparatus, the second communication apparatus unlocking the starter relay control apparatus only if the first code signal matches an access code stored in the second communication apparatus.

2. The system of claim 1 wherein the alternating voltage has a frequency between 25 and 50 kHz.

3. The system of claim 2 wherein the alternating voltage has a frequency of 31 kHz.

4. The system of claim 1 wherein the starter relay control apparatus comprises

voltage measurement apparatus sensing a voltage output of the main electrical power system,

timer apparatus responsive to the voltage measurement apparatus, the timer apparatus supplying a latch control signal to a latch apparatus at the end of an interval of predetermined duration during which the voltage output has a persistent value of zero volts, and

the latch apparatus acting responsive to the latch control signal to place the starter relay control in the locked state.

5. The system of claim 4 wherein the timer apparatus and the latch apparatus are powered by an exhaustible electrical power source separate from the main electrical power system.

6. The system of claim 1 wherein the aircraft is a fixed-wing airplane having two or more wings, the airplane having a plurality of said electrically started engines, each of the engines operatively connected to a separate start switch by a separate starter control line, and wherein each of the starter control lines comprises a wire disposed within one of the wings.

7. An anti-theft system installed on an aircraft,

the aircraft comprising a cabin, a bulkhead separating the cabin from an engine, a main electric power system supplied by a starting battery or by a generator driven by the engine, and a starter control line having a first end in the cabin and a second end adjacent a starter relay controlling an electric starter motor powered by the main electric power system to engage and turn the engine, the engine being startable if the starter relay is enabled, the engine being unstartable if the starter relay is disabled,

the system comprising,

sensing means sensing a persistence measurand indicating an out-of-service status,

timing apparatus responsive to the sensing means and supplying a first latch control signal to a latch apparatus after a predetermined time interval during which the out-of-service status persists,

the latch apparatus located intermediate the cabin and the starter relay and operably connected to the starter relay, the latch apparatus responsive both to the first latch control signal and to a second latch control signal, the latch apparatus disabling the starter relay in response to the first latch control signal, the latch apparatus enabling the starter relay in response to the second latch control signal,

operator-identification apparatus within the cabin, the operator-identification apparatus generating an input code and transmitting the input code over the starter control line to a comparison apparatus,

the comparison apparatus receiving the input code, comparing the input code with an access code stored in the comparison apparatus, and supplying the second latch control signal to the latch apparatus if the input code matches the stored access code.

8. The system of claim 7 wherein the aircraft comprises a plurality of engines, each of the engines separately equipped with a said electric starter motor, a said starter motor relay and a said latch apparatus.