Airplane detection system

• US 5,508,697 A
• Filed: 11/19/1993
• Issued: 04/16/1996
• Est. Priority Date: 03/19/1992
• Status: Expired due to Fees

• Current Assignee: Nippon Signal Company Limited
• Original Assignee: Nippon Signal Company Limited
• Inventors: Inaba, Kiyoaki, Kato, Masakazu, Sakai, Masayoshi, Futsuhara, Koichi
• Primary Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US08/150,086
• Time in Patent Office: 879 Days
• Field of Search: 340/933, 340/953, 340/947, 340/958, 340/988, 340/990, 340/901-903, 364/439, 364/449, 364/460, 364/461, 342/29, 342/36, 342/32
• US Class Current: 340/933
• CPC Class Codes: B26D 5/32 with the record carrier formed by the work itself
• CPC Class Codes: D04C 5/26 Auxiliary devices
• CPC Class Codes: D06H 7/16 specially adapted for cutting lace or embroidery shearing, e.g. cutting loose threads, D06C
• CPC Class Codes: D06H 7/22 Severing by heat or by chemical agents by laser beam B23K26/402
• CPC Class Codes: G01S 13/04 Systems determining presence of a target based on relative movement of target G01S13/56
• CPC Class Codes: G01V 3/12 operating with electromagnetic waves operating with millimetre waves G01V8/005

Abstract

The present invention relates to an airplane detection system to surely detect an airplane moving along a runway or a taxiway. The system employs a wheel detection sensor for providing a wheel detected output when emitted electromagnetic waves are blocked by the wheels of the airplane and a fuselage detection sensor for providing a fuselage detected output when receiving the reflection of the emitted electromagnetic waves from the fuselage of the airplane. According to the output signals from both the sensors, the system detects the airplane.

Claims

1. An airplane detection system comprising:

wheel detection means including an energy transmission type sensor with a first pair of wave transmitter and wave receiver arranged on each side of a runway,

said wheel detection means providing an output to indicate presence of an airplane when electromagnetic waves emitted from the wave transmitter of the first pair are blocked and energy received by the wave receiver of the first pair becomes lower than a first predetermined level;

fuselage detection means including a radar type energy reflection sensor with a second pair of wave transmitter and wave receiver arranged on the side of the runway wherein said wave transmitter of the wheel detection means is arranged,

said fuselage detection means providing an output to indicate presence of the airplane when a reflection of electromagnetic waves emitted from the wave transmitter of the second pair is received by the wave receiver of the second pair and energy of the reflection received by the wave receiver of the second pair becomes higher than a second predetermined level; and

decision means for determining whether or not there is an airplane on the runway according to the output conditions of the wheel detection means and the fuselage detection means,

wherein the decision means includes a nose wheel detected signal generator for generating a nose wheel detected signal according to the detection signals from the wheel detection means and fuselage detection means, a main wheel passage detected signal generator for generating a main wheel passage detected signal according to the detection signal from the fuselage detection means, and a self-hold circuit for generating and self-holding a decision signal to indicate the presence of an airplane upon receiving the nose wheel detected signal from the nose wheel detected signal generator and resetting the decision signal in response to the main wheel passage detected signal from the main wheel passage detected signal generator.

2. The airplane detection system according to claim 1, wherein the nose wheel detected signal generator has a first waveform shaping circuit for shaping the waveform of the output of the wheel detection means, an inverter for inverting an output of the first wave form shaping circuit, a second wave form shaping circuit for shaping the waveform of the output of the fuselage detection means, a delay circuit for delaying an output of the second waveform shaping circuit by a predetermined time, and an AND circuit for providing the nose wheel detected signal according to an AND of the outputs of the inverter and delay circuit.

3. The airplane detection system according to claim 2, wherein the nose wheel detected signal generator has a differentiating circuit for differentiating the output of the inverter and providing the differentiated output to the AND circuit.

4. The airplane detection system according to claim 2, wherein the first waveform shaping circuit has a delay circuit having a delay time necessary for removing chattering components from the signal provided by the wheel detection means, and a level tester having a threshold level necessary for extracting an output signal provided by the wheel detection means equal to or below the threshold level.

5. The airplane detection system according to claim 2, wherein the second waveform shaping circuit has a delay circuit having a delay time necessary for removing chattering components from the signal provided by the fuselage detection means, and a level tester having a threshold level necessary for removing noise from the signal provided by the fuselage detection means.

6. The airplane detection system according to claim 1, wherein the main wheel passage detected signal generator has a level tester for providing an output when the output of the fuselage detection means is above a predetermined level, and an inverter for inverting the output of the level tester and providing the inverted output to the self-hold circuit.

7. The airplane detection system according to claim 2, having an OR circuit for providing an OR of the output of the second waveform shaping circuit and the output of the self-hold circuit, an output of the OR circuit being used as the decision signal to indicate whether or not there is an airplane.

8. The airplane detection system according to claim 1, wherein said wave transmitter of said first pair is also said wave transmitter of said second pair.