Radial Oil Recovery Gutter for Compact Turbomachine Speed Reducers

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Solution Overview

Problem

Current lubrication systems in turbomachines, such as dual flow turbine engines, face challenges in efficiently recovering and evacuating large oil flows, leading to premature wear and decreased efficiency due to insufficient lubrication, and existing oil recovery devices are complex and increase the radial size and manufacturing cost of the turbomachine.

Innovation Solution

A power transmission system with a simplified oil recovery device featuring an annular gutter secured to a fixed housing, including a recovery chamber and a first wall portion to direct oil ejected by centrifugal force towards the chamber, with a radially oriented inlet opening and an annular tab to reduce radial size and facilitate efficient oil recovery.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a complex oil recovery device with multiple walls, fins and bowls is used to prevent oil accumulation and guide oil to the recovery chamber, then oil recovery efficiency is improved, but device complexity and manufacturing cost increase

Engineering Contradiction:
Improveoil recovery efficiencyVSAvoidrecovery device complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The recovery device is segmented into distinct functional zones: a recovery chamber for collecting oil, a first wall portion for guiding oil, and a second wall portion for containing oil. This segmentation allows each component to perform its specific function efficiently while keeping the overall design manageable and manufacturable.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention utilizes the radial dimension effectively by positioning the recovery chamber and wall portions in a radial configuration around the rotor shaft. The inlet opening is radially oriented to receive oil ejected by centrifugal force, and the wall portions are arranged radially to guide and contain the oil flow, optimizing space utilization and recovery efficiency.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Productivity

If a gutter with multiple walls, fins and bowls is used to guide oil to the recovery chamber, then oil recovery effectiveness is improved, but the radial size of the gutter increases

Engineering Contradiction:
Improveoil recovery effectivenessVSAvoidgutter radial size
Core Design Contradiction:
ProductivityVSLength of moving object

Solution Approach 1:

Instead of using a traditional gutter structure that extends radially outward to guide oil, the invention inverts the approach by using radially oriented wall portions that direct oil inward toward the recovery chamber. The first wall portion faces the oil ejection means and directs oil radially inward, while the second wall portion contains the oil flow, eliminating the need for a large radial gutter structure.

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The invention exploits the radial dimension by orienting the inlet opening and wall portions radially to match the centrifugal ejection pattern of the oil. This radial configuration allows the recovery device to intercept oil efficiently without requiring excessive radial space, as the structure follows the natural radial flow path of the oil.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Reliability

If a large oil flow of more than 5000 liters per hour is sent to lubricate the speed reducer, then lubrication efficiency is improved, but the difficulty of recovering and evacuating the oil increases

Engineering Contradiction:
Improvelubrication efficiencyVSAvoidoil recovery system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The recovery device leverages the centrifugal force generated by the rotating outer ring gear to automatically eject oil from the speed reducer toward the recovery chamber. The radially oriented inlet opening and wall portions passively guide the centrifugally ejected oil into the recovery chamber without requiring additional pumps or complex evacuation mechanisms, enabling the system to handle large oil flows efficiently.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention utilizes the hydraulic principle of centrifugal force to move the oil flow. The rotating outer ring gear generates centrifugal force that ejects the lubricating oil radially outward, and the recovery device is configured to intercept and collect this centrifugally ejected oil, converting the kinetic energy of the rotating system into effective oil recovery.

Inventive Principle:
Principle #29Pneumatics and hydraulics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The solution enables quick and efficient recovery and evacuation of large oil flows, reducing the radial size of the recovery system and simplifying its design while maintaining manufacturing feasibility, thus enhancing the turbomachine's efficiency and reducing wear.

Implementation Method 1

a device for recovering oil ejected by centrifugal effect into the turbomachine

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

The oil flows by gravity towards the lower part of the enclosure for its evacuation

Methodology Applied
Scientific EffectGravity: Gravitation

Data Source

PatentUS11125318B2Power transmission system including a lubrication oil recovery device and turbomachine provided with such a power transmission system
Publication Date: 2021.09.21 SAFRAN AIRCRAFT ENGINES SAS
  • US11125318B2 patent drawing
  • US11125318B2 patent drawing
  • US11125318B2 patent drawing

AI summary

The invention concerns a power transmission system of a turbomachine, comprising:a speed reducer (12) comprising a sun gear (15) rotationally secured to a power shaft (5) with a longitudinal axis, an outer ring gear (18) rotating a rotor shaft along the longitudinal axis, and a planet carrier (17), anda device (40) for recovering oil ejected by centrifugal effect and comprising an annular gutter (41) for recovering the ejected oil, the gutter being attached to a fixed annular housing (26) and having a recovery chamber (42) and a first wall portion (43) disposed at least partially facing oil ejection means (30) of the speed reducer for directing the oil to the recovery chamber.According to the invention, the recovery chamber is provided with an inlet opening (45) directed radially outwardly and defined in a plane radially lower than a plane where an outlet port (33) of the ejection means is defined.