Low or flat tire warning system

• US 4,355,298 A
• Filed: 02/17/1981
• Issued: 10/19/1982
• Est. Priority Date: 08/20/1979
• Status: Expired due to Term

• Current Assignee: The Bendix Corporation (Honeywell International Inc.)
• Original Assignee: The Bendix Corporation (Honeywell International Inc.)
• Inventors: Jessup, Gregory M.
• Primary Examiner(s): Waring, Alvin H.
• Application Number:
  US06/234,522
• Time in Patent Office: 609 Days
• Field of Search: 340/58, 200/61.22, 200/61.25, 200/61.26, 73/146, 73/146.2
• US Class Current: 340/444
• CPC Class Codes: B60C 2200/02 for aircrafts
• CPC Class Codes: B60C 23/061 by monitoring wheel speed measuring distance traversed on the ground by vehicles G01C22/00

Abstract

An aircraft low or flat tire flight deck warning system monitors the rotational speed and thus, the condition of the tires. A differential tire rotational speed signal is compared to a variable reference by a comparator which generates a warning signal when the differential signal is greater than or equal to the reference. The reference signal is derived from one of the tire rotation signals or from an independent ground speed signal and is therefore proportional to the rotational speed of a properly inflated tire and to the aircraft ground speed. Separate references and comparators cooperate to generate separate warning signals for distinct dangerous tire conditions. The warning signals are inhibited under a variety of conditions.

Claims

1. An aircraft tire condition warning system for an aircraft bogie with two wheels having tires mounted thereon, said warning system comprising:

a speed sensor associated with one of the wheels for generating a speed signal proportional to the angular velocity of said one wheel;

a speed sensor associated with the other of said two wheels for generating a speed signal proportional to the angular velocity of said other wheel;

means for differencing the two speed signals and for generating a differential signal proportional to the difference in angular velocity therebetween;

means for comparing the two speed signals and for generating a ground speed signal which is the smaller of the two speed signals wherein said ground speed signal is proportional to the aircraft ground speed of a wheel having a properly inflated tire thereon;

means for generating a reference signal by multiplying said ground speed signal times a proportionality constant indicative of a dangerous tire condition, said reference signal thereby varying with the ground speed of the aircraft;

means for comparing said differential signal and said reference signal and for generating a warning signal when said differential signal exceeds said reference signal; and

means for generating an operator identifiable warning indication in response to said warning signal.

2. An aircraft tire condition warning system as defined in claim 1, further including:

means, receiving said reference signal as an indication of aircraft ground speed, for inhibiting said warning signal to said indication generating means if the ground speed of the aircraft is greater than a predetermined maximum or less than a predetermined minimum.

3. An aircraft tire condition warning system as defined in claim 2 further including:

means for inhibiting said warning signal to said indication generating means if the aircraft is executing a turn on the runway.

4. An aircraft tire condition warning system as defined in claim 3, further including:

means for inhibiting said warning signal to said indication generating means if the aircraft is traveling along a sideslope on the runway.

5. An aircraft tire condition warning system as defined in claim 1 which further comprises:

at least one other means for generating at least one other reference signal proportional to said ground speed signal, each of said other reference signals having a different proportionality constant than said reference signal, each of said proportionality constants being indicative of a different dangerous tire condition; and

at least one other means for comparing said differential signal to said other reference signals and for generating at least one other warning signal when said differential signal exceeds said other reference signals.