Aircraft Cabin Blower Drive With One-Way Rotation Decoupling

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Solution Overview

Problem

Current cabin blower systems for aircraft have limited electrical capability when operating in electrical-only mode, as one electrical machine is constrained to rotate with the gas turbine engine, limiting the power rating of the remaining machine and reducing the system's efficiency and weight optimization.

Innovation Solution

The aircraft cabin blower system incorporates a variable drive system with an electric variator and summing gearbox, along with one-way rotation devices that allow free rotation in the forward direction and prevent reverse rotation, enabling independent operation of the electrical machines to enhance power management and efficiency, allowing the system to operate purely electrically or start the gas turbine engine electrically.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If one electrical machine is constrained to rotate with the gas turbine engine, then the system can operate in electrical-only mode, but the power rating of the remaining electrical machine is limited and the system weight and complexity are increased

Engineering Contradiction:
Improveelectrical capabilityVSAvoidsystem complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The system separates the electrical machines from the gas turbine rotation constraint by introducing a one-way rotation device. This allows the electrical machines to be decoupled from the engine's rotational requirements, enabling independent operation and higher power ratings without being constrained by engine speed.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The one-way rotation device acts as an intermediary between the gas turbine engine and the electrical machines. It permits the electrical machines to rotate freely in the forward direction while preventing reverse rotation, thereby mediating the conflict between engine-driven operation and independent electrical operation.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If a one-way rotation device is added to permit free rotation and prevent reverse rotation, then electrical capability is enhanced, but device complexity increases

Engineering Contradiction:
Improveoperational flexibilityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The one-way rotation device provides multiple functions: it allows free rotation during normal operation, enables electrical-only mode by decoupling from the engine, and prevents reverse rotation to protect the system. This multi-functionality justifies the added complexity by delivering several operational benefits from a single component.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Use of energy by moving object

If the system operates in electrical-only mode with limited power rating, then fuel consumption is reduced, but the power capacity is insufficient for the blower compressor

Engineering Contradiction:
Improvefuel efficiencyVSAvoidpower capacity
Core Design Contradiction:
Use of energy by moving objectVSPower

Solution Approach 1:

The system dynamically adapts its operational mode based on power requirements. The electrical machines can operate independently when sufficient power is needed and fuel efficiency is prioritized, while the gas turbine can be engaged when maximum power is required. The one-way rotation device enables this dynamic switching without mechanical constraint.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS11698023B2Aircraft cabin blower system
Publication Date: 2023.07.11 ROLLS ROYCE PLC
  • US11698023B2 patent drawing
  • US11698023B2 patent drawing
  • US11698023B2 patent drawing

AI summary

An aircraft cabin blower system comprises a cabin blower including a compressor configured to provide air to a cabin of the aircraft; a variable drive system configured to drive the compressor and including an electric variator and a summing gearbox; and a main transmission configured, when operating in a blower mode, to receive mechanical power from a gas turbine engine and input mechanical power to the summing gearbox in a forward direction; and configured, when operating in a starter mode, to receive mechanical power from the summing gearbox and input mechanical power to the gas turbine engine. The aircraft cabin blower system further includes a first one-way rotation device adapted to permit free rotation of the main transmission in the forward direction and to prevent rotation of the main transmission in a reverse direction opposite to the forward direction.