Wireless transducer data capture and retrieval system for aircraft

• US 6,009,356 A
• Filed: 11/12/1996
• Issued: 12/28/1999
• Est. Priority Date: 10/11/1996
• Status: Expired due to Term

• Current Assignee: e-Watch, Inc. (Cision Ltd.)
• Original Assignee: Raytheon TI Systems, Inc. (Rtx Corporation)
• Inventors: Monroe, David A.
• Primary Examiner(s): Louis-Jacques, Jacques H.
• Application Number:
  US08/745,536
• Time in Patent Office: 1,141 Days
• Field of Search: 701/3, 701/14, 701/15, 701/16, 701/35, 701/29, 701/1, 701/2, 364/550, 364/551.01, 364/580, 340/963, 340/439, 340/945, 340/438, 340/436, 73/587
• US Class Current: 701/14
• CPC Class Codes: B64D 45/0053 using visual equipment, e.g. cameras
• CPC Class Codes: B64D 45/0056 detecting passenger or crew behavior by sensors, e.g. biometrics
• CPC Class Codes: B64D 45/0059 by communicating emergency situations to ground control or between crew members
• CPC Class Codes: G01S 3/8006 Multi-channel systems specially adapted for direction-finding, i.e. having a single aerial system capable of giving simultaneous indications of the directions of different signals
• CPC Class Codes: G01S 3/808 using transducers spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems
• CPC Class Codes: G08B 13/19634 Electrical details of the system, e.g. component blocks for carrying out specific functions
• CPC Class Codes: G08B 13/19645 Multiple cameras, each having view on one of a plurality of scenes, e.g. multiple cameras for multi-room surveillance or for tracking an object by view hand-over
• CPC Class Codes: G08B 13/1965 the vehicle being an aircraft
• CPC Class Codes: G08B 13/1966 Wireless systems, other than telephone systems, used to communicate with a camera
• CPC Class Codes: G08B 13/19695 Arrangements wherein non-video detectors start video recording or forwarding but do not generate an alarm themselves
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

A wireless safety and surveillance recorder system for aircraft incorporates a plurality of strategically spaced wireless sensors for monitoring critical components and operational characteristics of the aircraft. The captured data and a wireless image are transmitted to a monitor in the cockpit and recorded on a "black box" flight recorder, and may be transmitted to ground control stations for real time or near real time surveillance. The system may include a second recorder for providing redundancy and may include redundant sensors.

Claims

1. A wireless data collection and transmission system for monitoring extraneous occurrences on board an aircraft in order to permit reconstruction of a catastrophic event whether or not the aircraft stays intact throughout the event, the system providing in flight data monitor, collection, display and recording of audio and visual information, the system comprising:

a. a plurality of event sensors positioned at strategic locations about the aircraft, each adapted for monitoring a selected condition aboard the aircraft, each said sensor adapted for generating a unique data signal representing a specific condition to be monitored;

b. an integrated, dedicated power supply associated with each sensor, whereby each said sensor will continue generating said unique data signal when disconnected from aircraft power;

c. a wireless transmitter adapted for transmitting the unique data signal from each said sensor;

d. a wireless receiver located on the aircraft for receiving and processing each of the plurality of unique signals, whereby each said sensor will continue to transmit the unique data signal in the event the monitored location is separated from a portion of the aircraft wherein the wireless receiver is located.

2. The system of claim 1, wherein one of said data signals is an analog data signal and wherein one of said data signals is a digital data signal, the receiver system further including an analog to digital converter for converting the analog data signal into a converted digital data signal, the multiplexer subsystem adapted for multiplexing the converted digital data signal and the digital data signal into a combined digital data signal.

3. The system of claim 1, wherein one of said data signals is an analog data signal and wherein one of said data signals is a digital data signal, the receiver system further including a digital to analog converter for converting the digital data signal into a converted analog data signal, the multiplexer subsystem adapted for multiplexing the converted digital data signal and the analog data signal into a combined analog data signal.

4. The system of claim 1, the aircraft including a plurality of engines, and the data sensor devices including an array of performance sensors associated with each engine and a local engine multiplexer subsystem associated with each array of performance sensors for producing a combined engine performance data signal for each engine.

5. The system of claim 1, wherein the receiver system further includes a monitor for displaying the processed signal.

6. The system of claim 1, wherein the receiver system further includes a recorder for capturing the processed output signal in a retrievable format.

7. The system of claim 6, wherein the recorder is a single-channel analog recorder.

8. The system of claim 6, wherein the recorder is a digital memory device.

9. The system of claim 1, wherein the receiver system further includes an additional transmitter adapted for wireless transmission of the data signal to a remote location, whereby the data output signal may be downloaded from the system.

10. The system of claim 9, wherein the system further includes a receiver adapted for receiving wireless transmission of uploaded data signals from a remote location, whereby an uploaded data signal may be uploaded onto the system from a remote location.

11. The system of claim 1, further including traditional sensors in combination with the wireless sensors.

12. The system of claim 1, wherein said wireless sensors are adapted for transmitting the data signal to the receiver system via wireless radio frequency transmission.

13. The system of claim 12, wherein each wireless sensor includes a transmitter for generating a data signal to be transmitted and the receiver system includes a receiver device for accepting the transmitted data signal.

14. The system of claim 1, wherein each sensor includes a transmitter for generating a data signal on a unique frequency and wherein the receiver system comprises a dedicated receiver for each of the plurality of transmitted data signals.

15. The system of claim 14, further including means for multiplexing the plurality of transmitted data signals for generating a combination data signal incorporating all of said plurality of data signals.

16. The system of claim 14 further including a single receiver system adapted for receiving the plurality of transmitted data signals.

17. The system of claim 1, said receiver system further including a self-contained power supply.

18. The system of claim 1, further including the wireless sensors each adapted for monitoring a selected condition on board the aircraft, each sensor adapted for generating a unique data signal representing the specific condition to be monitored, and wherein said receiver system is adapted for receiving the plurality of data signals from the plurality of sensors and for combining said data signals for producing a combined output signal.

19. The system of claim 1, further including a second receiver system independent of said first mentioned receiver system for providing redundancy.

20. The system of claim 1, further including a second plurality of wireless sensors in parallel with said first mentioned plurality of wireless sensors for providing redundancy.

21. The system of claim 1, further including a monitor hardwired to said plurality of sensors.

22. The system of claim 1, further including a monitor having a receiver for receiving the data transmitted by the transmitter.