Turbocharger
US-2015056065-A1 · Feb 26, 2015 · US
US10830248B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10830248-B2 |
| Application number | US-201515311045-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 28, 2015 |
| Priority date | May 15, 2014 |
| Publication date | Nov 10, 2020 |
| Grant date | Nov 10, 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 air-flow circuit for air flow through a bearing enclosure of a turbine engine, the air-flow circuit including a supply system arranged such as to supply the air into the bearing enclosure; a discharge system arranged such as to discharge at least some of the air from the bearing enclosure; an oil-removal system connected to the discharge system, the oil-removal system being capable of reducing the amount of lubricant contained in the air coming from the discharge system; and a compressor arranged between the discharge system and the oil-removal system, the compressor being capable of increasing the air pressure at the intake of the oil-removal system.
Opening claim text (preview).
The invention claimed is: 1. A turbine engine comprising a bearing enclosure, said bearing enclosure being delimited between a rotor rotatably movable about a reference axis and a stator including a bearing bracket to which a bearing laying against said rotor is mounted, said bearing enclosure including a system for feeding lubricant to said bearing and a recovery system for recovering lubricant, said bearing enclosure including an air-flow circuit for an air flow through said bearing enclosure of the turbine engine in which the lubricant can be injected, the air-flow circuit including: an air supply system arranged to supply air into the bearing enclosure; a discharge system arranged to discharge at least some of the air-lubricant mixture contained in the bearing enclosure; an oil-removal system connected to the discharge system, the oil-removal system being capable of separating the lubricant from the air contained in the air-lubricant mixture coming from the discharge system, and a compressor disposed between the discharge system and the oil-removal system, the compressor being capable of increasing the pressure of the air-lubricant mixture at an intake of the oil-removal system; a drawing system containing air at atmospheric pressure, the supply system of the air-flow circuit being connected to the drawing system. 2. The turbine engine according to claim 1 , wherein the oil-removal system generates a head loss, the compressor being capable of compensating for at least some of the head loss generated by the oil-removal system. 3. The turbine engine according to claim 1 , wherein the compressor is a centrifugal compressor. 4. The turbine engine according to claim 1 , wherein the compressor is a positive displacement compressor. 5. The turbine engine according to claim 1 , wherein the compressor includes at least one rotating shaft, the air-flow circuit further including a power transmission system configured to rotatably drive the rotating shaft of the compressor. 6. The turbine engine according to claim 5 , wherein the power transmission system includes an accessory gear box capable of transmitting the movement of a radial shaft of the turbine engine to the rotating shaft of the compressor, the accessory gear box including: a power take-off member capable of meshing with a radial shaft of the turbine engine; and at least one kinematic chain capable of transmitting the rotational movement of the power take-off member to the rotating shaft of the compressor, the kinematic chain including a central shaft connected to the power take-off member through a gear, the central shaft being arranged to transmit the movement of the power take-off member to the rotating shaft of the compressor. 7. The turbine engine according to claim 6 , wherein the central shaft includes a distal end, the compressor being attached to the distal end of the central shaft.
using lubrication pumps · CPC title
Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus (oil separators for separating oil from exhaust steam F22G) · CPC title
Closed-circuit lubricating systems not provided for in groups F01M1/02 - F01M1/10 · CPC title
with pumps sucking air or blow-by gases from the crankcase · CPC title
Dry-sumps · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.