Recovering fuel vapour from aircraft fuel tank
US-2024092499-A1 · Mar 21, 2024 · US
US2018319514A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018319514-A1 |
| Application number | US-201815961070-A |
| Country | US |
| Kind code | A1 |
| Filing date | Apr 24, 2018 |
| Priority date | May 4, 2017 |
| Publication date | Nov 8, 2018 |
| Grant date | — |
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Official abstract text for this publication.
A fluid coupler includes a housing with an inlet port and an outlet port, a piston disposed in the housing and configured to control fluid flow between the inlet port and the outlet port, and a piston retainer disposed in the housing. A piston may include at least one radially-extending support member, and the radially-extending support member may include an aperture. The at least one radially-extending support member may be substantially planar.
Opening claim text (preview).
What is claimed is: 1 . A fluid coupler, comprising: a housing including an inlet port and an outlet port; a piston disposed in the housing and configured to control fluid flow between the inlet port and the outlet port; and a piston retainer disposed in the housing; wherein the piston includes at least one radially-extending support member, and a radially-extending support member of the at least one radially-extending support member includes an aperture. 2 . The fluid coupler of claim 1 , wherein the at least one radially-extending support member is substantially planar. 3 . The fluid coupler of claim 1 , wherein the at least one radially-extending support member is substantially parallel to a plane defined by an axial direction and a radial direction relative to a central axis of the piston. 4 . The fluid coupler of claim 1 , wherein the at least one radially-extending support member includes four radially-extending support members. 5 . The fluid coupler of claim 1 , wherein the aperture includes a first portion and a second portion, and the first portion includes a greater axial extent than the first portion. 6 . The fluid coupler of claim 1 , wherein the aperture includes a radial extent that is at least half as a radial extent of the radially-extending support member. 7 . The fluid coupler of claim 1 , wherein the piston is keyed with a connecting member; and the connecting member is disposed at partially in an inner portion of the piston and at least partially in a collar of the piston retainer. 8 . The fluid coupler of claim 1 , wherein the piston is configured to translate within the housing and is prevented from rotating relative to the housing. 9 . The fluid coupler of claim 1 , including a fluid straightener. 10 . The fluid coupler of claim 9 , wherein the piston is configured as the fluid straightener, the at least one radially-extending support member includes at least six radially-extending support members equally circumferentially-spaced about at least one of (i) an inner surface of an outer wall of the piston and (ii) an inner portion of the piston. 11 . A piston for a fluid coupler, the piston comprising: an outer wall including a cylindrical configuration; an inner portion; and a plurality of support members extending between the cylindrical outer wall and the inner portion; wherein at least one of the plurality of support members includes an aperture. 12 . The piston of claim 11 , wherein the at least one support member is radially-extending and is substantially planar. 13 . The piston of claim 11 , wherein the at least one support member is substantially parallel to a plane defined by an axial direction and a radial direction relative to a central axis of the piston. 14 . The piston of claim 11 , wherein the plurality of support members includes at least three support members. 15 . The piston of claim 11 , wherein the aperture includes a first portion and a second portion, and the first portion includes a greater axial extent than the first portion. 16 . The piston of claim 15 , the second portion includes a greater radial extent than the first portion. 17 . The piston of claim 15 , wherein the first portion is disposed at a first distance from the outer wall, the second portion is disposed at a second distance from the outer wall, and the second distance is greater than the first distance. 18 . The fluid coupler of claim 11 , wherein the aperture includes an L-shaped configuration. 19 . The fluid coupler of claim 11 , wherein the aperture includes a radial extent that is at least half as great as a radial extent of the at least one support member. 20 . The fluid coupler of claim 11 , wherein the inner portion includes a recess configured to engage a key of a connecting member.
Means to inhibit the introduction of too small or too big filler nozzles · CPC title
Tank inlets (B60K15/077 takes precedence) · CPC title
Liquid-handling installations specially adapted for fuelling stationary aircraft · CPC title
Resilient supports (B60K5/1241 - B60K5/1291 take precedence) · CPC title
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