Liquid-capturing shaft
US-10113429-B2 · Oct 30, 2018 · US
US10612415B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10612415-B2 |
| Application number | US-201715689412-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 29, 2017 |
| Priority date | Aug 29, 2017 |
| Publication date | Apr 7, 2020 |
| Grant date | Apr 7, 2020 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An assembly for rotational equipment includes a stationary structure and a rotating structure. The stationary structure is configured with a first fluid conduit. The rotating structure is configured with a second fluid conduit and a fluid scoop for the second fluid conduit. The second fluid conduit is fluidly coupled with the first fluid conduit through an annular plenum formed by and radially between the stationary structure and the rotating structure. The fluid scoop projects radially into the annular plenum.
Opening claim text (preview).
What is claimed is: 1. An assembly for rotational equipment, comprising: a stationary structure configured with a first fluid conduit; and a rotating structure configured with a second fluid conduit and a fluid scoop for the second fluid conduit, the second fluid conduit fluidly coupled with the first fluid conduit through an annular plenum formed by and radially between the stationary structure and the rotating structure, and the fluid scoop projecting radially into the annular plenum; the rotating structure comprising a first shaft, a second shaft and a hub; and the hub connecting the first shaft to the second shaft, and the hub comprising the second fluid conduit and the fluid scoop; and a gas turbine engine including the first shaft; and a device connected to and driven by the second shaft, the device arranged outside of the gas turbine engine. 2. The assembly of claim 1 , wherein the fluid scoop is adapted to direct fluid, within the annular plenum, into the second fluid conduit; and the annular plenum is adapted to receive the fluid therewithin from the first fluid conduit. 3. The assembly of claim 1 , wherein the fluid scoop is arranged at an inlet of the second fluid conduit. 4. The assembly of claim 1 , wherein the fluid scoop has a tubular body with a beveled edge portion. 5. The assembly of claim 4 , wherein the fluid scoop further has a projection that projects out from the tubular body and into a slot in the hub. 6. The assembly of claim 1 , wherein the first fluid conduit extends radially within the stationary structure to an outlet orifice in a radial inner surface of the stationary structure; the second fluid conduit extends radially within the rotating structure to an inlet orifice in a radial outer surface of the rotating structure; and the annular plenum extends radially from the radial inner surface to the radial outer surface. 7. The assembly of claim 1 , further comprising a fluid nozzle configured and rotatable with the rotating structure, the fluid nozzle fluidly coupled with an outlet of the second fluid conduit. 8. The assembly of claim 1 , wherein the rotating structure is further configured with a third fluid conduit and a second fluid scoop for the third fluid conduit, the third fluid conduit is fluidly coupled with the first fluid conduit through the annular plenum, and the second fluid scoop projects radially into the annular plenum. 9. The assembly of claim 8 , further comprising a fluid device fluidly coupled with the second fluid conduit and the third fluid conduit. 10. The assembly of claim 1 , wherein the hub further comprises a fluid nozzle fluidly coupled with an outlet of the second fluid conduit. 11. The assembly of claim 1 , wherein the rotating structure further comprises a first rotating assembly that includes the first shaft and a rotor configured with a plurality of rotor blades. 12. The assembly of claim 1 , further comprising: a gas turbine engine including the first shaft; and a transmission connected to the second shaft. 13. The assembly of claim 12 , further comprising a generator driven by the second shaft through the transmission. 14. The assembly of claim 1 , further comprising a seal device adapted to seal an annular gap between the stationary structure and the rotating structure. 15. The assembly of claim 14 , wherein the seal device comprises an O-ring. 16. The assembly of claim 14 , further comprising a second seal device adapted to seal a second annular gap between the stationary structure and the rotating structure, wherein the annular plenum is located axially, relative to a rotational axis of the rotating structure, between the seal device and the second seal device. 17. An assembly for rotational equipment, comprising: a stationary structure configured with a first fluid conduit; a hub comprising a hub base, a second fluid conduit and a fluid scoop at an inlet of the second fluid conduit, the second fluid conduit fluidly coupled with the first fluid conduit through an annular plenum that extends radially from the hub to the stationary structure, and the fluid scoop projecting radially out from the hub base and into the annular plenum, wherein the fluid scoop is adapted to direct fluid, which is received within the annular plenum from the first fluid conduit, into the second fluid conduit; and a first shaft and a second shaft, the first shaft connected to the second shaft through the hub; and a gas turbine engine including the first shaft; and a device connected to and driven by the second shaft, the device arranged outside of the gas turbine engine. 18. The assembly of claim 17 , wherein the scoop fluidly divides the annular plenum into a pair of circumferentially adjacent sub-plenums.
with rotary distributing member (combined with oil pump F16N13/22) · CPC title
Ducts · CPC title
Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title
Turbines · CPC title
Shaft to shaft connections · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.