Dual stage shock strut with removable second stage fluid chamber

US9541151B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9541151-B2
Application numberUS-201514620006-A
CountryUS
Kind codeB2
Filing dateFeb 11, 2015
Priority dateFeb 11, 2015
Publication dateJan 10, 2017
Grant dateJan 10, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In various embodiments, a two stage shock strut for use in a landing gear assembly may comprise a first cylinder, a fill port, a first stage piston head, a second cylinder, a second stage piston head, and a bleed tube. The first cylinder may define a first volume. The fill port valve may be in fluid communication with the first cylinder and configured to receive hydraulic fluid. The first stage piston head may be in fluid communication with the first volume. The second cylinder may comprise a metering pin. The metering pin may be in fluid communication with the first volume and a second volume defined by the second cylinder. The metering pin may be configured to receive the hydraulic fluid from the first volume and purge gas from the second volume. The second stage piston head may be in fluid communication with the second volume.

First claim

Opening claim text (preview).

What is claimed is: 1. A two stage shock strut for use in a landing gear assembly, comprising: a first cylinder defining a first volume; a fill port valve in fluid communication with the first cylinder and configured to receive hydraulic fluid; a first stage piston head in fluid communication with the first volume; a second cylinder comprising a metering pin, the metering pin in fluid communication with the first volume and a second volume defined by the second cylinder, wherein the metering pin is configured to receive the hydraulic fluid from the first volume and purge gas from the second volume; a second stage piston head in fluid communication with the second volume, wherein the hydraulic fluid supplied through the metering pin is configured to translate the second stage piston head to a second fully compressed position; and a bleed tube in fluid communication with at least one of the metering pin and the second volume, wherein the hydraulic fluid supplied through the fill port valve is exhausted through the bleed tube. 2. The two stage shock strut of claim 1 , wherein the metering pin is integrally formed in the second cylinder. 3. The two stage shock strut of claim 2 , further comprising an air charge port in fluid communication with the first fluid chamber, wherein gas may be pumped into the first fluid chamber via the air charge port. 4. The two stage shock strut of claim 2 , further comprising an air charge port in fluid communication with a fourth fluid chamber, wherein the gas may be pumped into the fourth fluid chamber via the air charge port. 5. The two stage shock strut of claim 1 , wherein the bleed tube is operatively coupled to a hydraulic bleed port. 6. The two stage shock strut of claim 5 , wherein the hydraulic bleed port is opened for bleeding at least one of the hydraulic fluid or a mixture of gas and the hydraulic fluid during a maintenance operation. 7. The two stage shock strut of claim 6 , wherein in response to the bleeding the second stage piston head is translated to the second fully compressed position. 8. The two stage shock strut of claim 1 , wherein the bleed tube defines a hole positioned within a second fluid chamber such that at least one of the hydraulic fluid or a mixture of gas and the hydraulic fluid is displaced between the second fluid chamber and the bleed tube via the hole. 9. The two stage shock strut of claim 1 , wherein the hydraulic fluid supplied through the fill port valve is configured to exert a force on the first stage piston head in response to a maintenance operation, and wherein the first stage piston head is configured to translate to a first fully compressed position in response to the force. 10. The two stage shock strut of claim 1 , wherein the two stage shock strut is configured to achieve a fully compressed configuration in response to a maintenance operation. 11. A second stage fluid chamber sub-assembly for use in a dual stage shock strut, comprising: a cylinder defining a volume; a piston head in fluid communication with the volume, the piston head separating the volume into a first chamber and a second chamber; a metering pin in fluid communication with the volume and configured to conduct hydraulic fluid to the volume to exert a force on the piston head in response to a maintenance operation; a bleed tube in fluid communication with the volume and configured to purge gas from the volume in response to the maintenance operation, the bleed tube extending into the first chamber and into the second chamber. 12. The second stage fluid chamber sub-assembly of claim 11 , wherein the bleed tube is operatively coupled to a hydraulic bleed port that is opened to purge the gas in response to the maintenance operation. 13. The second stage fluid chamber sub-assembly of claim 11 , wherein the piston head is translated to a fully compressed configuration in response to the hydraulic fluid being pressurized during the maintenance operation. 14. The second stage fluid chamber sub-assembly of claim 11 , wherein the cylinder comprises an air charge port configured to receive the gas in response to the maintenance operation. 15. The second stage fluid chamber sub-assembly of claim 14 , wherein the piston head is configured to translate to an extended configuration in response to receiving the gas in response to the maintenance operation.

Assignees

Inventors

Classifications

  • Drainage arrangements · CPC title

  • Devices with one or more members moving linearly to and fro in chambers, any throttling effect being immaterial, i.e. damping by viscous shear effect only (F16F9/53 takes precedence) · CPC title

  • F16F9/063Primary

    comprising a hollow piston rod · CPC title

  • Oleo legs · CPC title

  • F16F9/3271Primary

    Assembly or repair · CPC title

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What does patent US9541151B2 cover?
In various embodiments, a two stage shock strut for use in a landing gear assembly may comprise a first cylinder, a fill port, a first stage piston head, a second cylinder, a second stage piston head, and a bleed tube. The first cylinder may define a first volume. The fill port valve may be in fluid communication with the first cylinder and configured to receive hydraulic fluid. The first stage…
Who is the assignee on this patent?
Goodrich Corp
What technology area does this patent fall under?
Primary CPC classification F16F9/063. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 10 2017 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).