Capacitive sensors for monitoring loads

• US 8,933,713 B2
• Filed: 10/13/2011
• Issued: 01/13/2015
• Est. Priority Date: 07/19/2010
• Status: Active Grant

• Current Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Goodrich Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Eriksen, Odd Harald Steen, Sanden, Christopher
• Primary Examiner(s): Assouad, Patrick
• Assistant Examiner(s): PRETLOW, DEMETRIUS R
• Application Number:
  US13/272,317
• Publication Number:
  US 20120043417A1
• Time in Patent Office: 1,188 Days
• Field of Search: 324/690, 324658-661, 324/686, 244100 R-100 A, 244/102.SL, 244/102.SS
• US Class Current: 324/686
• CPC Class Codes: B64C 2025/006 Landing gear legs comprising torque arms
• CPC Class Codes: B64C 25/001 Devices not provided for in the groups B64C25/02 - B64C25/68
• CPC Class Codes: B64D 2045/008 Devices for detecting or indicating hard landing
• CPC Class Codes: G01L 1/142 using capacitors
• CPC Class Codes: G01L 5/0014 by using capacitive sensors

Abstract

A sensor for monitoring loads in a landing gear torque linkage includes a main pin having an axial interior bore defined therein. The main pin is configured and adapted to engage a torque link to a strut lug of a landing gear strut. A core pin is mounted axially within an interior bore of the main pin and is spaced radially inwardly from the interior bore for relative displacement with respect to the main pin. A capacitor is included having an inner capacitor plate mounted to the core pin. An outer capacitor plate is mounted to the main pin. Relative displacement of the core pin and the main pin due to loads acting on the torque link and strut lug results in relative displacement of the inner and outer capacitor plates. Signals can thereby be produced indicative of the loads acting on the torque link.

Claims

1. A sensor for monitoring loads in a landing gear torque linkage comprising:

a) a main pin having an axial interior bore defined therein and having a length defined from a first end to an opposed second end thereof, wherein the main pin is configured and adapted to engage a torque link to a strut lug of a landing gear strut;

b) a core pin mounted axially aligned within the interior bore of the main pin and being spaced radially inwardly with a radial clearance from the interior bore for relative displacement with respect to the main pin; and

c) a capacitor having an inner capacitor plate mounted to the core pin, and a first outer capacitor plate mounted to the main pin, such that relative displacement of the core pin and the main pin due to external loading on the main pin results in relative displacement of the inner and first outer capacitor plates, wherein the capacitor is configured to be connected to an electrical circuit to produce a signal indicative of the loads acting on the torque link and strut lug based on changes in capacitance due to relative displacement of the inner and first outer capacitor plates;

d) a second outer capacitor plate mounted to the main pin,

wherein the first outer capacitor plate and the second outer capacitor plate are semi-cylindrical and are aligned circumferentially and axially,

wherein the second outer capacitor plate is configured to be connected to the electrical circuit to produce a signal indicative of an external loading on the main pin based on the relative displacement of the core pin and the main pin, and

wherein the electrical circuit is configured to constructively combine the signal from the inner capacitor plate and the first outer capacitor plate and the signal from the inner capacitor plate and second outer capacitor plate.

2. A sensor as recited in claim 1, further comprising an angle sensor mounted in the axial interior bore of the main pin between the capacitor and the first end of the main pin.

3. A sensor as recited in claim 2, wherein the core pin, capacitor, and angle sensor are mounted proximate the first end of the main pin, and further comprising a second such core pin, capacitor, and angle sensor mounted proximate the second end of the main pin.

4. A torque linkage for bearing and monitoring rotational moments in a landing gear strut comprising:

a) a main pin engaging a torque link to a strut lug, wherein the torque link is configured and adapted to bear rotational moments about a lengthwise axis of the landing gear strut, and wherein the main pin has an axial interior bore defined therein and has a length defined from a first end to an opposed second end thereof;

b) a core pin mounted axially within the interior bore of the main pin and being spaced radially inwardly from the interior bore for relative displacement with respect to the main pin; and

c) a capacitor having an inner capacitor plate mounted to the core pin, and an outer capacitor plate mounted to the main pin, such that relative displacement of the core pin and the main pin due to loads acting on the torque link and strut lug results in relative displacement of the inner and outer capacitor plates, wherein the capacitor is configured and adapted to be connected to an electrical circuit to produce signals indicative of the loads acting on the torque link and strut lug based on the relative displacement of the inner and outer capacitor plates.

5. A torque linkage as recited in claim 4, wherein the interior bore extends along about half of the length of the main pin, wherein the core pin is cantilevered to the interior bore proximate a middle portion of the main pin, and wherein the capacitor is located proximate the second end of the main pin.

6. A torque linkage as recited in claim 4, wherein the capacitor includes a plurality of outer capacitor plates, each capacitor plate being mounted to the main pin and being aligned axially with the inner capacitor plate, and wherein the outer capacitor plates are configured and adapted to be connected to an electrical circuit to produce signals indicative of external loading on the main pin based on the relative displacement of the core pin and the main pin.

7. A torque linkage as recited in claim 6, wherein there are three or more outer capacitor plates configured and adapted to be connected to an electrical circuit to produce signals indicative of magnitude and orientation of external loading on the main pin based on the relative displacement of the core pin and the main pin.

8. A torque linkage as recited in claim 6, wherein the outer capacitor plates are spaced apart evenly circumferentially.