Dual-stage, separated gas/fluid shock strut servicing

US10865848B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10865848-B2
Application numberUS-201715642081-A
CountryUS
Kind codeB2
Filing dateJul 5, 2017
Priority dateJul 5, 2017
Publication dateDec 15, 2020
Grant dateDec 15, 2020

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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A method for servicing a dual-stage, separated gas/fluid shock strut may comprise measuring a servicing temperature, charging a secondary gas chamber with compressed gas, wherein a secondary chamber pressure corresponds to the servicing temperature, pumping oil into the shock strut, and charging a primary gas chamber with compressed gas.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for servicing a dual-stage, separated gas/fluid shock strut, comprising: measuring a servicing temperature; charging a secondary gas chamber with a first quantity of compressed gas, wherein a secondary chamber pressure corresponds to the servicing temperature; pumping an oil into an oil chamber of the dual-stage, separated gas/fluid shock strut subsequent to the secondary gas chamber being charged with the first quantity of compressed gas; and charging a primary gas chamber with a second quantity of compressed gas, wherein the primary gas chamber is fluidly separated from the oil chamber via a first separator piston and the secondary gas chamber is fluidly separated from the oil chamber via a second separator piston. 2. The method of claim 1 , wherein the secondary gas chamber is charged with the second quantity of compressed gas until the secondary chamber pressure corresponds to the servicing temperature as indicated by a secondary chamber servicing chart. 3. The method of claim 1 , further comprising extending the dual-stage, separated gas/fluid shock strut in response to the pumping, wherein the dual-stage, separated gas/fluid shock strut extends such that a shock strut extension and the secondary chamber pressure match an oil servicing reference curve. 4. The method of claim 1 , further comprising: extending the dual-stage, separated gas/fluid shock strut to a shock strut extension corresponding to the secondary chamber pressure, in accordance with an oil servicing reference curve, wherein the oil is pumped into the dual-stage, separated gas/fluid shock strut to a pre-determined pressure. 5. The method of claim 3 , wherein the oil servicing reference curve is provided in the form of at least one of a series of curves or a series of tables for various servicing temperatures. 6. The method of claim 1 , wherein the primary gas chamber is charged with the second quantity of compressed gas until a primary chamber pressure and a shock strut extension correspond to a primary chamber servicing reference curve. 7. The method of claim 1 , further comprising releasing a gas from the primary gas chamber. 8. The method of claim 1 , further comprising releasing a gas from the secondary gas chamber. 9. The method of claim 4 , wherein the pre-determined pressure is about 75 psi (517.1 kPa). 10. A method for servicing a dual-stage, separated gas/fluid shock strut, comprising: charging a secondary gas chamber with a first quantity of compressed gas, wherein a secondary chamber pressure corresponds to a servicing temperature; pumping an oil into an oil chamber of the dual-stage, separated gas/fluid shock strut, wherein the dual-stage, separated gas/fluid shock strut extends until a first shock strut extension and the secondary chamber pressure match an oil servicing reference curve; and charging a primary gas chamber with a second quantity of compressed gas until a second shock strut extension and a primary chamber pressure match a primary chamber servicing reference curve, wherein the primary gas chamber is fluidly separated from the oil chamber via a first separator piston and the secondary gas chamber is fluidly separated from the oil chamber via a second separator piston. 11. The method of claim 10 , wherein at least one of the oil servicing reference curve and the primary chamber servicing reference curve correspond to the servicing temperature. 12. The method of claim 10 , further comprising measuring the servicing temperature. 13. The method of claim 10 , further comprising releasing a gas from the primary gas chamber. 14. The method of claim 10 , further comprising releasing a gas from the secondary gas chamber. 15. A method for servicing a dual-stage, separated gas/fluid shock strut, comprising: charging a secondary gas chamber with a first quantity of compressed gas, wherein a secondary chamber pressure corresponds to a servicing temperature; circulating an oil through an oil chamber of the dual-stage, separated gas/fluid shock strut via an oil charge port and an oil bleed port; extending the dual-stage, separated gas/fluid shock strut to a shock strut extension corresponding to the secondary chamber pressure according to an oil servicing reference curve; closing the oil bleed port; pumping the oil into the oil chamber until an oil chamber pressure reaches a pre-determined pressure while maintaining the shock strut extension; closing the oil charge port; extending the dual-stage, separated gas/fluid shock strut to a fully extended position; and charging a primary gas chamber with a second quantity of compressed gas until a shock strut extension and a primary chamber pressure match a primary chamber servicing reference curve. 16. The method of claim 15 , wherein at least one of the oil servicing reference curve and the primary chamber servicing reference curve correspond to the servicing temperature. 17. The method of claim 15 , further comprising measuring the servicing temperature. 18. The method of claim 15 , wherein the pre-determined pressure comprises about 75 psi (517.1 kPa). 19. The method of claim 15 , further comprising releasing a gas from the primary gas chamber. 20. The method of claim 15 , further comprising releasing a gas from the secondary gas chamber.

Assignees

Inventors

Classifications

  • B64F5/40Primary

    Maintaining or repairing aircraft · CPC title

  • comprising a hollow piston rod · CPC title

  • the spring material being generally enclosed · CPC title

  • Maintenance · CPC title

  • using dampers and springs in combination · CPC title

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What does patent US10865848B2 cover?
A method for servicing a dual-stage, separated gas/fluid shock strut may comprise measuring a servicing temperature, charging a secondary gas chamber with compressed gas, wherein a secondary chamber pressure corresponds to the servicing temperature, pumping oil into the shock strut, and charging a primary gas chamber with compressed gas.
Who is the assignee on this patent?
Goodrich Corp
What technology area does this patent fall under?
Primary CPC classification B64F5/40. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 15 2020 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).