Servicing of landing gear shock absorbers
US-2017008648-A1 · Jan 12, 2017 · US
US10865848B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10865848-B2 |
| Application number | US-201715642081-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 5, 2017 |
| Priority date | Jul 5, 2017 |
| Publication date | Dec 15, 2020 |
| Grant date | Dec 15, 2020 |
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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.
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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.
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