Aircraft Cabin Blower Startup Control for Contactless Bearing Wear

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Solution Overview

Problem

Cabin blower systems in aircraft suffer from contamination of cabin air with oil and increased wear during start-up due to contactless bearings, which are prone to wear at low operating speeds.

Innovation Solution

A cabin blower system with a contactless bearing arrangement and a reversible variator that controls the direction and speed of rotation to hold the compressor stationary until it reaches the lift-off speed, reducing wear by minimizing time in the wear-inducing regime, and includes a disconnect arrangement to prevent connection until a minimum speed is reached.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If contactless bearings are used in the cabin blower compressor, then air contamination with oil is eliminated, but wear increases during start-up at low operating speeds

Engineering Contradiction:
Improveair contamination with oilVSAvoidbearing wear during start-up
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The system performs preliminary action by accelerating the gas turbine engine to a minimum speed threshold before connecting the variator output to the cabin blower compressor. This ensures that the compressor only starts rotating when the engine is already at a sufficient speed, allowing the contactless bearings to reach their lift-off speed quickly and minimize wear during the start-up phase.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system implements dynamics by using a reversible variator that can operate in both forward and reverse directions, with the controller dynamically adjusting the connection timing based on engine speed. The variator provides a dynamic coupling mechanism that can engage or disengage the compressor from the engine drive, optimizing the start-up process to reduce bearing wear while maintaining contamination-free operation.

Inventive Principle:
Principle #15Dynamics

2Reliability

If the cabin blower compressor is accelerated quickly to lift-off speed, then bearing wear is reduced, but control complexity increases

Engineering Contradiction:
Improvebearing wear reductionVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The controller implements feedback by continuously monitoring the gas turbine engine speed and comparing it against the minimum speed threshold. Based on this feedback, the controller automatically determines when to reverse the variator output direction and when to switch to forward rotation, enabling quick acceleration to lift-off speed while managing control complexity through automated decision-making based on real-time engine conditions.

Inventive Principle:
Principle #23Feedback

3Reliability

If the variator output is held stationary during start-up, then bearing wear is minimized, but the start-up time increases

Engineering Contradiction:
Improvebearing wear minimizationVSAvoidstart-up time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system applies skipping by rapidly transitioning the variator output from reverse to forward direction once the engine reaches the minimum speed threshold. This allows the compressor to quickly skip through the wear-inducing low-speed regime and reach the lift-off speed zone, minimizing both bearing wear and start-up time by rushing through the critical transition phase.

Inventive Principle:
Principle #21Skipping (Rushing through)

Data Source

PatentEP4001115B1Cabin blower system
Publication Date: 2022.11.16 ROLLS ROYCE PLC
  • EP4001115B1 patent drawingFigure 1~2
  • EP4001115B1 patent drawingFigure 3
  • EP4001115B1 patent drawingFigure 4

AI summary

Aircraft cabin blower systems 400 and methods of operating aircraft cabin blower systems are provided. One aircraft cabin blower system 400 comprises: a cabin blower compressor 402 having a contactless bearing arrangement 403; a transmission 410 having a transmission output arranged to drive the cabin blower compressor 402, a first transmission input 414 arranged to receive mechanical power from a gas turbine engine 10, and a second transmission input 418; a reversible variator 415 arranged to receive power from the gas turbine engine 10 and to output mechanical power to the second transmission input 418, the reversible variator 415 operable to output in both forward and reverse directions of rotation; and a controller 425 configured to control an output speed and direction of rotation of the reversible variator 415. A speed of the transmission output is a function of a speed of the first transmission input 414, a speed of the second transmission input 418 and the direction of rotation of the variator output. The second transmission input 418 increases the speed of the transmission output when the variator output rotates in the forward direction and reduces the speed of the transmission output when the variator output rotates in the reverse direction. The controller 425 is configured so that, during a start-up process of the cabin blower system 400, the variator output is controlled to rotate in the reverse direction until a start-up threshold condition is satisfied. The variator output is then reversed to rotate in the forward direction.