Automatic method to identify aircraft types

• US 4,163,283 A
• Filed: 04/11/1977
• Issued: 07/31/1979
• Est. Priority Date: 04/11/1977
• Status: Expired due to Term

• Current Assignee: Ronald A. Darby
• Original Assignee: Ronald A. Darby
• Inventors: Darby, Ronald A.
• Primary Examiner(s): Krass, Errol A.
• Application Number:
  US05/786,560
• Time in Patent Office: 841 Days
• Field of Search: 235/150.24, 235/150.2, 235/151.32, 235/151.3, 235/92 EV, 235/92 TC, 246/2 S, 246/122 R, 246/167 D, 246/247, 340/386 R, 340/146.3 K, 364/424, 364/436, 364/439, 364/565, 104/26 B
• US Class Current: 701/120
• CPC Class Codes: B64F 1/00 Ground or aircraft-carrier-deck installations specially adapted for captive aircraft B64F3/00
• CPC Class Codes: G01B 7/02 for measuring length, width or thickness G01B7/004, G01B7/12 take precedence
• CPC Class Codes: G01P 3/66 using electric or magnetic means G01P3/80 takes precedence; measuring short time intervals G04F8/00, G04F10/00

Abstract

Two sensors spaced at a known separation produce signal pulses when activated by the wheels of a taxiing aircraft. The signals are transmitted to a processor in which the wheelbase of the aircraft can readily be calculated. Since specific aircraft types have unique wheelbase dimensions and characteristics, the type of aircraft passing the sensors is determined in a processor. Also, the time, direction, and speed of the aircraft can be determined and logged by the processor.

Claims

1. A method to automatically classify the type of aircraft moving on the ground by automatically determining sufficient physical characteristics unique to the landing gear of each given type of aircraft, said characteristics being the nominal major wheelbase, the total number of axles, and the spacing of the main carriage axles, comprising the steps of:

providing a system comprising a sensor set, a data transmission link, a processor, and a data read-out device;

said sensor set comprising two sensor systems located at a known distance apart which are activated by the wheels of the aircraft and produce a sequence of signal pulses, said data transmission link to transmit the signal pulses to the processor, said processor to generate signals representative of the type of aircraft, the location of the sensor set, the time of an event, the direction of travel of the aircraft and the speed of the aircraft in response to time intervals between signal pulses, and wheelbase characteristics from a look-up table in the memory bank of said processor, and said data read-out device to indicate the type of aircraft, the location of the sensor set, time of an event, direction of travel of the aircraft, and the speed of the aircraft.

2. The method of claim 1 including the step of providing a plurality of sensor sets and data transmission links, said sensor sets being located on a plurality of runways and/or taxiways at an airport and said processor generating signals representative of accumulations of selected signals generated by the processor over a selected period of time related to aircraft type and runway and/or taxiway usage, and the taxi-and-hold times between sensor sets.

3. The method of claim 1 including the steps of providing a plurality of sensor sets and data transmission links and additional logic in the processor, making the processor for compatibility with a read-out device comprising a real time display board visually indicating the type of aircraft and direction of travel within various sectors of taxiways and runways.

4. The method of claim 1 including the step of interfacing the process with an automatic noise monitoring system such that the data read-out device indicates the type of aircraft associated with a noise exceedance in the airport environs after take-off or landing on runways implemented with said sensor sets.

5. The method of claim 1 including the step of interfacing the processor with an automatic aircraft noise monitoring system such that the data read-out device indicates the type of aircraft traffic pattern used at a given time and said processor can be interfaced with the the automatic noise system to optimize acoustic tracking of aircraft flights and to assist the noise monitoring system in discriminating aircraft noise events from non-aircraft noise events, such as caused by passes of motorcycles and trucks.

6. Apparatus for determining selected parameters related to aircraft type having characteristic landing gear comprising

first sensing means positioned adjacent a runway or taxiway travelled by the aircraft type for producing pulses upon detecting passage of wheels on the aircraft type past a first known position along the runway or taxiway,

second sensing means positioned adjacent said runway or taxiway and spaced from the first sensing means a known distance along the pathway for producing pulses upon detecting the passage of wheels on the aircraft type past a second known position along the pathway,

data transmission means connected to the first and second sensing means for communicating pulses produced by the first and second sensing means to processor means,

aircraft type processor means connected to the data transmission means for generating signals representative of selected parameters related to the aircraft type in response to time intervals between pulses produced by the sensing means,

data display means connected to the processor means for displaying data representative of the selected parameters related to the aircraft type in response to the signals generated by the processor means.

7. The apparatus of claim 6 wherein

the data display means comprises printer means for generating static characters representative of the selected parameters related to the aircraft type in response to the signals generated by the processor means.

8. The apparatus of claim 6 wherein

the data display means comprises real time display means for generating images representative of the selected parameters related to the aircraft type substantially simultaneously with the passage of the aircraft type along the runway or taxiway in response to the signals generated by the processor means.

9. The apparatus of claim 6 wherein the first and second sensor means comprise

light beam generating means positioned along one side of the runway or taxiway for directing beams of light transversely across the runway or taxiway, and

photocell means positioned along the other side of the pathway for receiving the beams of light generated by the light beam generating means,

wherein the data transmission means is connected to the photocell means for communicating pulses produced by the photocell means upon interruption of the beams of light to the processor means.

10. The apparatus of claim 6 wherein the processor means comprises

identification memory means for storing data correlating known aircraft type identifications with known characteristic wheelbases,

wheelbase calculator means connected to the data transmission means for generating signals representative of the wheelbase of the aircraft type in response to the pulses produced by the sensing means and

comparator means connected to the calculator means and identification memory means for comparing signals generated by the calculator means with the data stored in the identification memory means and generating signals representative of the aircraft type identification corresponding to the aircraft type travelling along the runway or taxiway.

11. The apparatus of claim 10 wherein the processor means further comprises

traffic memory means connected to the comparator means for accumulating and storing data representative of the aircraft type identification signals generated by the comparator means during a selected period of time.

12. The apparatus of claim 6 wherein

the processor means comprises signal conditions means connected to the data transmission means for generating signals representative of the time intervals between pulses produced by the sensing means in response to the pulses communicated by the data transmission means.

13. The apparatus of claim 12 wherein the processor means further comprises

time memory means connected to the signal conditioning means for accumulating and storing data representative of the time interval signals generated by the signal conditioning means during a selected period of time.

14. The apparatus of claim 6 wherein

the data transmission means comprise voice grade telephone lines connected to the first and second sensing means and the processor means.

15. The apparatus of claim 6 wherein the data transmission means comprise

electromagnetic signal transmitting means connected to the first and second sensing means for transmitting electromagnetic signals representative of pulses produced by the first and second sensing means in response to the pulses, and

electromagnetic signal receiving means connected to the processor means for receiving signals transmitted by the electromagnetic signal transmitting means and generating signals representative of the pulses produced by the first and second sensing means in response to the signals received from the electromagnetic signal transmitting means.

16. The apparatus of claim 6 wherein the processor means comprises

speed calculator means connected to the data transmission means for generating signals representative of the speed of the aircraft type in response to the pulses produced by the sensing means.

17. The apparatus of claim 6 wherein the processor means comprises

direction calculator means connected to the data transmission means for generating signals representative of the direction of the aircraft type in response to the pulses produced by the sensing means.

18. The apparatus of claim 6 further comprising noise level sensing means positioned in the vicinity of the airport containing the runway or taxiway for generating signals representative of the noise level produced by the aircraft over the noise level sensing means, and

noise level processor means connected to the noise level sensing means for generating signals representative of various noise exposure parameters, the noise level processor means connected to the aircraft type processor means and data display means for integrating the noise exposure parameter signals and the signals generated by the aircraft type processor means and generating signals representative of the integration of the signals of the type of aircraft generating the noise exposure parameters,

the data display means displaying data representative of the signals generated by the noise level processor and the aircraft type processor in response to said signals.

19. The apparatus of claim 18 wherein the noise processor means connected to the aircraft type processor means comprises

memory means for accumulating and storing data representative of the integrated signals generated by the noise level processor connected to the aircraft type processor during a selected period of time.

20. A method for classifying type of aircraft by determining landing gear characteristics comprising sensing the passage of wheels of the aircraft past a first known position along a runway or taxiway travelled by the aircraft, generating pulse signals in response to the sensed passage of the wheels past the first known position, sensing the passage of wheels of the aircraft past a second known position along the runway or taxiway, the second known position spaced from the first known position a known distance along the runway or taxiway, generating pulse signals in response to the sensed passage of the wheels past the second known position, measuring the time intervals between pulse signals, generating signals representative of selected parameters related to the aircraft in response to the measured time intervals, and displaying data representative of the selected parameters related to the aircraft in response to the signals representative of the selected parameters.

21. The method of claim 20 wherein the process of generating signals representative of selected parameters related to the aircraft comprises

storing data correlating known aircraft type identifications with known characteristic wheelbases,

generating wheelbase signals representative of the wheelbase of the aircraft in response to measured time intervals between signals generated by the wheels passing the first known position and signals generated by the wheels passing the second known position,

comparing the wheelbase signals with the stored data, and

generating signals representative of the aircraft identifications corresponding to the aircraft travelling along a runway or taxiway in response to the comparison.

22. The method of claim 21 further comprising

accumulating data representative of the aircraft identification signals during a selected period of time

storing the data representative of the aircraft identification signals.

23. The method of claims 20 wherein the process of generating signals representative of selected parameters related to the aircraft comprises

generating signals representative of the speed of the aircraft in response to measured time intervals between signals generated by the wheels passing the known positions.

24. The method of claims 20 wherein the process of generating signals representative of selected parameters related to the aircraft comprises

generating signals representative of the direction of the aircraft in response to the sequence of pulse signals generated by the wheels passing the first and second known positions.

25. The method of claim 20 further comprising

sensing the noise produced by the aircraft before or after it traveled along the runway or taxiway,

generating signals representative of the sensed noise levels,

integrating the noise level signals and the signals representative of selected parameters related to the aircraft,

generating signals representative of the integration of the signals thereby relating noise levels caused by the aircraft after departing from the runway or before landing on the runway with the type of aircraft.