Tail skid shock absorber and indicator

Patent metadata

Field	Value
Publication number	US-10669016-B2
Application number	US-201715493379-A
Country	US
Kind code	B2
Filing date	Apr 21, 2017
Priority date	Apr 21, 2017
Publication date	Jun 2, 2020
Grant date	Jun 2, 2020

Abstract

A tail skid shock absorber including an outer shock absorber canister, a crushable indicator cartridge disposed within the outer shock absorber canister, and an indicator rod coupled to the crushable indicator cartridge so as to move with a portion of the crushable indicator cartridge as a unit.

First claim

What is claimed is:

1. A tail skid shock absorber comprising:
an outer shock absorber canister that includes an elongated tube and an end fitting, the end fitting being configured to couple with one of a tail skid shoe or an airframe, where the end fitting includes an end fitting aperture;
a crushable indicator cartridge disposed within the outer shock absorber canister; and
an indicator rod coupled to the crushable indicator cartridge so as to move with a portion of the crushable indicator cartridge as a unit, where the indicator rod extends through the end fitting aperture, wherein the indicator rod includes at least one graduation that indicates an amount of remaining energy absorption of the tail skid shock absorber.

2. The tail skid shock absorber of claim 1 , wherein the crushable indicator cartridge forms an elongated member that defines a crush core including:
a first plate coupled to the crush core, the indicator rod being coupled to the first plate; and
a second plate coupled to the crush core, the second plate defining an outer surface of the crushable indicator cartridge and including a second plate aperture through which the indicator rod extends, the second plate being separate and distinct from the outer shock absorber canister.

3. The tail skid shock absorber of claim 2 , wherein the indicator rod includes a rod head and the first plate includes a first plate aperture, the indicator rod extends through the first plate aperture where the rod head cooperates with the first plate aperture so that the indicator rod is retained on the first plate.

4. The tail skid shock absorber of claim 2 , wherein the second plate includes fasteners configured to couple the crushable indicator cartridge to an end fitting of the tail skid shock absorber.

5. The tail skid shock absorber of claim 1 , wherein the indicator rod extends through the end fitting aperture to provide a visual indicator of an amount of remaining energy absorption in the crushable indicator cartridge.

6. The tail skid shock absorber of claim 1 , wherein the elongated tube includes a first tube portion and a second tube portion that are moveable relative to each other along a longitudinal axis of the elongated tube.

7. The tail skid shock absorber of claim 1 , wherein the end fitting is removably coupled to the elongated tube so that removal of the end fitting from the elongated tube facilitates replacement of the crushable indicator cartridge.

8. The tail skid shock absorber of claim 1 , wherein the end fitting aperture includes two end fitting apertures symmetrically arranged on the end fitting.

9. The tail skid shock absorber of claim 1 , further comprising an anti-rotation member removably coupled to both the elongated tube and the end fitting.

10. The tail skid shock absorber of claim 1 , wherein the end fitting includes a datum surface adjacent the end fitting aperture where the datum surface defines a measuring point from which a distance the indictor rod protrudes from the end fitting aperture is determined.

11. A crushable indicator cartridge, the crushable indicator cartridge comprising:
an indicator rod;
an elongated member defining a crush core;
a first plate coupled to the crush core, the indicator rod being coupled to the first plate; and
a second plate coupled to the crush core, the second plate defining an outer surface of the crushable indicator cartridge and including a second plate aperture through which the indicator rod extends, where the indicator rod includes graduations that indicate an amount of remaining energy absorption of the tail skid shock absorber;
wherein the crushable indicator cartridge is shaped and sized for insertion into an outer shock absorber canister of a tail skid shock absorber and the second plate is separate and distinct from the outer shock absorber canister.

12. The crushable indicator cartridge of claim 11 , wherein the indicator rod includes a rod head and the first plate includes a first plate aperture, the indicator rod extends through the first plate aperture where the rod head cooperates with the first plate aperture so that the indicator rod is retained on the first plate.

13. The crushable indicator cartridge of claim 11 , wherein the indicator rod and the first plate move as a single unit along a longitudinal axis of the elongated member as the crush core is crushed.

14. The crushable indicator cartridge of claim 11 , wherein the elongated member is configured for insertion to and removal from the outer shock absorber canister of the tail skid shock absorber such that an outer diameter of the elongated member is smaller than an inner diameter of the outer shock absorber canister.

15. The crushable indicator cartridge of claim 11 , wherein the second plate includes fasteners configured to couple the crushable indicator cartridge to an end fitting of a tail skid shock absorber.

16. The crushable indicator cartridge of claim 11 , wherein the second plate includes a fluid drainage groove.

17. A method for indicating an amount of energy absorption remaining in a tail skid shock absorber, the method comprising:
inserting a crushable indicator cartridge into an outer shock absorber canister, where the crushable indicator cartridge includes an indicator rod coupled to the crushable indicator cartridge so as to move with a portion of the crushable indicator cartridge as a unit; and
crushing the crushable indicator cartridge through contact of an airplane tail skid with an object so that the indicator rod extends through an end fitting aperture of an end fitting of the outer shock absorber canister and is exposed from the outer shock absorber canister, where the end fitting couples the tail skid shock absorber to one of a tail skid shoe and an airframe and the indicator rod includes at least one graduation that indicates an amount of remaining energy absorption of the tail skid shock absorber.

18. The method of claim 17 , where an amount of extension of the indicator rod relative to the outer shock absorber canister indicates the amount of energy absorption remaining.

19. The method of claim 17 , wherein the crushable indicator cartridge includes an elongated member that defines a crush core that includes a first plate coupled to the crush core, the indicator rod being coupled to the first plate, and a second plate coupled to the crush core, the second plate defining an outer surface of the crushable indicator cartridge and including a second plate aperture through which the indicator rod extends, and wherein the first plate and the indicator rod move as a unit during crushing of the crushable indicator cartridge.

20. The method of claim 17 , further comprising replacing a crushed crushable indicator cartridge with an uncrushed crushable indicator cartridge when a predetermined amount of energy has been absorbed by the tail skid shock absorber.

Assignees

• Boeing Co

Inventors

• Cusworth James E
• Huested Michael P
• Cottet Justin D

Classifications

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• F16F2236/04

  Compression · CPC title

• B64C25/001 Primary

  Devices not provided for in the groups B64C25/02 - B64C25/68 · CPC title

• F16F7/125

  Units with a telescopic-like action as one member moves into, or out of a second member (F16F7/124, F16F7/127, F16F7/128 take precedence) · CPC title

• B64C2025/005

  Tail skids for fuselage tail strike protection on tricycle landing gear aircraft · CPC title