Tire pressure communication devices

• US 4,237,445 A
• Filed: 07/30/1979
• Issued: 12/02/1980
• Est. Priority Date: 07/30/1979
• Status: Expired due to Term

• Current Assignee: Loral Corporation (Newell Brands Inc.)
• Original Assignee: Goodyear Aerospace Corporation (Goodyear Tire & Rubber Company)
• Inventors: Crossman, Richard L.
• Primary Examiner(s): Waring, Alvin H.
• Application Number:
  US06/061,580
• Time in Patent Office: 491 Days
• Field of Search: 340/58, 200/61.22, 200/61.25
• US Class Current: 340/448
• CPC Class Codes: B60C 23/0408 transmitting the signals by non-mechanical means from the wheel or tyre to a vehicle body mounted receiver
• CPC Class Codes: B60C 23/0467 Electric contact means, e.g. slip-rings, rollers, brushes

Abstract

Devices for transmitting signals from a rotatable tire to a stationary receiver which correspond to the internal pressure of the tire. In one embodiment, a Bourdon tube communicates with internal tire pressure to regulate the magnetic gap of an electromagnetic induction configuration. Changes in the magnetic gap result in corresponding changes in an output signal strength. In another embodiment of the invention, a bellows is provided in communication with tire pressure for regulating the position of the core of an LVDT. The core position and, accordingly, the output of the LVDT corresponds to tire pressure. In yet another embodiment, strain gauges or other appropriate electrical signal generators are connected to the tire and interconnected with a rotating race. A plurality of ball bearings are maintained in a preloaded condition between the rotating race and a stationary race, the latter race communicating signals to a tire pressure meter or the like.

Claims

1. Apparatus for sensing the pressure of an aircraft tire and for communicating such pressure sensing from a rotating tire to a stationary portion of the aircraft, comprising:

tire pressure sensing means connected to and rotatable with the tire;

signal receiving means comprising a coil fixedly secured to a stationary portion of the aircraft; and

communication means comprising a core positioned and movable within said coil and operatively connected to said sensing means for communicating a signal indicative of tire pressure from said sensing means to said coil.

2. The apparatus according to claim 1 wherein said coil is rotatable with the tire, said coil and said core comprising a linear variable differential transformer.

3. The apparatus according to claim 2 wherein said sensing means comprises a bellows in pressure communication with the tire, said bellows being connected to said core.

9. The apparatus according to claim 1 wherein said sensing means comprises a first set of races, and said signal receiving means comprises a second set of races.

4. Apparatus for sensing the pressure of an aircraft tire and for communicating such pressure sensing from a rotating tire to a stationary portion of the aircraft, comprising:

tire pressure sensing means connected to and rotatable with the tire;

a first electrical coil maintained about a core, said core being fixedly secured to the stationary portion of the aircraft;

a second coil maintained about said core and in inductive communication with said first coil; and

an expandable and contractable circular member connected to and rotatable with the wheel, said member rotating in a path in juxtaposition to said core and operative therewith for completing a magnetic circuit for communicating a signal indicative of the tire pressure from said sensing means to said first and second coils.

7. The apparatus according to claim 4 wherein said sensing means comprises an air pressure inlet in communication between the tire and said member, communicating the pressure of the tire to said member.

8. The apparatus according to claim 7 wherein said member comprises a Bourdon tube.

5. Apparatus for sensing the pressure of an aircraft tire and for communicating such pressure sensing from a rotating tire to a stationary portion of the aircraft, comprising:

tire pressure sensing means comprising a first set of races connected to and rotatable with the tire;

signal receiving means comprising a second set of races fixedly secured to a stationary portion of the aircraft; and

communication means comprising a plurality of ball bearings preloaded between respective pairs of said first and second sets of races, said ball bearings being maintained between said races in four-point contact for communicating a signal indicative of tire pressure from said sensing means to said receiving means.

6. The apparatus according to claim 5 wherein said ball bearings within said races are maintained within an electrically conductive grease.