Low visibility runway monitor

• US 4,481,516 A
• Filed: 09/29/1982
• Issued: 11/06/1984
• Est. Priority Date: 10/27/1980
• Status: Expired due to Fees

• Current Assignee: Paul E. Michelotti
• Original Assignee: Paul E. Michelotti
• Inventors: Michelotti, Paul E.
• Primary Examiner(s): Groody, James J.
• Application Number:
  US06/428,196
• Time in Patent Office: 769 Days
• Field of Search: 340/38 R, 340/38 P, 340/38 S, 340/552, 340/553, 340/26, 340/27 R, 340/933, 340/947, 340/942, 340/943, 340/953, 377/9, 343/17.7, 343/5 PD
• US Class Current: 340/933
• CPC Class Codes: G08G 5/0026 located on the ground
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

A runway collision avoidance system having warning devices is provided for the safety of aircraft taxiing, taking off, and landing. The system is capable of detecting ground traffic and obstacles including aircraft, maintenance vehicles and wildlife that may encroach upon an active runway during low visibility conditions or when visual observation is impaired. The system includes an electromagnetic transmitter positioned beyond one end of a runway which directs a continuous beam of high frequency radio signals, for example microwaves, longitudinally along the full length of the runway. A plurality of electromagnetic receivers positioned beyond the other end of the runway pick up the transmitted signals and apply them to a balance circuit and then to a comparator circuit. With a clear runway, the transmitted signals are received without interruption and the receiver outputs remain balanced or equal. However, should an obstruction occur on the runway, an attenuation is produced in one or more of the receivers and a warning output is generated by the comparator circuit. The comparator warning output is utilized to activate aural and visual indicators in the control tower as well as warning lights positioned at appropriate points near the runway.

Claims

1. A runway collision avoidance system for use in conjunction with a runway of the type having an elongated landing surface including an approach end, and at least one intersecting taxiway, and defining an aircraft approach path extending from the approach end along the axis of the runway, for providing a warning to aircraft when an obstruction is on the runway, comprising:

an electromagnetic wave transmitter having an antenna array positioned beyond one end of the runway, said antenna array being positioned to horizontally cover substantially the full width of the runway, said transmitter and antenna array directing electromagnetic wave energy substantially across the entire width and longitudinally along the entire length of the runway;

a plurality of electromagnetic wave receivers each having an antenna arranged in a horizontal array at the other end of the runway which covers substantially the entire width of the runway, said array receiving electromagnetic wave energy directed down said runway by said transmitter;

balance circuit means coupled to the outputs of said receivers for adjusting the outputs of said receivers to a common value in the absence of an obstacle on the runway;

comparator circuit means coupled to said balance circuit means for generating a warning signal when the output of one or more of said receivers varies beyond a predetermined amount from said common value due to the presence of an obstacle on the runway; and

light indicator means responsive to said warning signal for providing an indication that an obstruction is present on the runway.

2. A runway collision avoidance system as defined in claim 1 wherein said light indicator means comprise at least one high intensity warning light positioned near the approach end of the runway, directed toward and viewable from the aircraft approach path.

3. A runway collision avoidance system as defined in claim 1 wherein said light indicator means further comprise at least one low intensity warning light positioned at the intersection of the taxiway and the runway and viewable from the taxiway, said low intensity light being coupled to and actuated by said comparator circuit means.