Aircraft low pressure tire warning system having comparator circuit for each axle pair of a four wheel bogie configuration

• US 4,283,707 A
• Filed: 07/12/1979
• Issued: 08/11/1981
• Est. Priority Date: 07/12/1979
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Church, Royce F.
• Primary Examiner(s): Caldwell, Sr., John W.
• Assistant Examiner(s): Nowicki, Joseph E.
• Application Number:
  US06/057,137
• Time in Patent Office: 761 Days
• Field of Search: 340/27 R, 340/58, 73/146.3, 73/146.4, 73/146.5, 200/61.22, 200/61.25, 244/100 A, 244/103 R, 244/104 FP
• US Class Current: 340/442
• CPC Class Codes: B60C 2200/02 for aircrafts
• CPC Class Codes: B60C 23/0401 characterised by the type of alarm
• CPC Class Codes: B60C 23/043 using transformer type signal transducers, e.g. rotary transformers

Abstract

An aircraft low tire pressure sensing and cockpit display and warning system utilizing axle wheel pair comparator circuitry to provide signals representative of pressures of the axle wheel pair less than a predetermined value, e.g. 15 percent less than a preset value determined by tire requirements or a difference between axle wheel pair pressures greater than a given value, e.g. 25 psi. In the event of tire master warning lamp illumination on the flight deck warning display, further push button interrogation and identification of the axle pair causing the warning can be made by a crew member on the flight deck warning display.

Claims

1. In an aircraft low pressure tire warning system having a flight deck warning display and first and second pressure transducers associated with first and second tires respectively of an axle pair:

means responsive to said first and second pressure transducers for providing first and second signals representative of said first and second tires;

a tire pressure signal processor and comparator circuit responsive to said first and second signals for providing signals representative of pressure conditions of said tires less than a preselected percentage of a preset value and further providing signals representative of wheel pair pressure differentials greater than a given value; and

said tire pressure signal processor and comparator circuit including a logic gate having an output terminal for providing a tire pressure warning signal in the event that at least one of said first and second tire pressures is less than a preselected percentage of a preset value or said first and second tire pressure differentials exceed a given value.

2. In combination:

a first wheel pair having tire pressures and a tire pressure differential;

a first tire pressure signal processor and comparator circuit for providing a first warning signal under the conditions of at least one of the tire pressures is less than a preselected percentage of a preset value or the tire pressure differential of said first wheel pair exceed a given value;

a second wheel pair having tire pressures and a tire pressure differential;

a second tire pressure signal processor and comparator circuit for providing a second warning signal under the conditions of at least one of the tire pressures is less than said preselected percentage of a preset value or the tire pressure differential of said second wheel pair exceed said given value; and

,

a tire master warning circuit having an OR gate responsive to the presence of said first or second warning signals for illuminating a tire master warning light.

3. The invention according to claim 2 further including warning lamp switching means associated with each of said first and second wheel pairs for identifying the wheel pair causing said tire master warning light to illuminate in the event of the presence of said first or second warning signals.