Dual-Spool Accessory Gearboxes With Interlink for Load Isolation
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Solution Overview
Problem
Dual spool turbine engines face challenges with large accessory gearboxes that compromise fan blade-off case load management, maintainability, and gearbox strength, particularly in electric and hybrid electric applications.
Innovation Solution
The implementation of two separate gearboxes, one for the high spool and one for the low spool, with optimized spur gear spacing and positional arrangements, allowing for modular assembly and independent oil and coolant systems, enhancing maintenance and reducing mass and case punch loads.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If a single large accessory gearbox is used to accommodate dual mechanical off takes, then all accessories can be integrated into one unit, but the gearbox mass and case punch loads increase, compromising fan blade-off case load management and gearbox strength
Solution Approach 1:
The single large accessory gearbox is divided into two separate gearboxes: a high spool gearbox and a low spool gearbox. This segmentation reduces the mass and case punch loads on each individual gearbox, thereby improving fan blade-off case load management while maintaining the capability to accommodate all necessary accessories through the distributed configuration
2Adaptability or versatility
If a single large accessory gearbox is used, then accessories are integrated into one unit, but maintainability deteriorates due to increased complexity and size
Solution Approach 1:
By segmenting the accessory gearbox system into two smaller, independent gearboxes (high spool and low spool), each unit becomes simpler to maintain and repair. The reduced complexity and size of individual gearboxes improve accessibility for maintenance activities while maintaining full accessory functionality across the distributed system
Solution Approach 2:
The low spool gearbox is extracted as a separate, independently maintainable unit from the traditional single gearbox configuration. This extraction allows the low spool gearbox to be removed and serviced independently without affecting the high spool gearbox, significantly improving maintainability
3Adaptability or versatility
If a single large accessory gearbox is used, then dual mechanical off takes are accommodated, but the gearbox mass increases, affecting overall system mass
Solution Approach 1:
The accessory gearbox system is segmented into two separate units that share the load of accommodating dual mechanical off takes. This segmentation reduces the mass of each individual gearbox compared to a single large gearbox, thereby reducing overall system mass while maintaining the capability to accommodate both high and low spool mechanical off takes
4Adaptability or versatility
If a single large accessory gearbox is used, then all accessories are in one unit, but system reliability is reduced due to single point of failure
Solution Approach 1:
The accessory system is segmented into two independent gearbox units with separate oil and coolant systems. This segmentation creates operational independence between the high spool and low spool systems, eliminating single points of failure and improving overall system reliability, as a failure in one gearbox does not necessarily compromise the other
Solution Approach 2:
The low spool gearbox and its associated oil and coolant systems are extracted as independent units from the traditional integrated gearbox design. This extraction creates physical and functional independence between the high and low spool systems, allowing one system to continue operating even if the other fails, thereby improving reliability
Data Source
Figure 1A
Figure 1B
Figure 1C
AI summary
A system (100; 200; 300) includes a turbine engine (110; 310), a low spool gearbox (130; 230; 330), a high spool gearbox (120; 320), and an interlink (328) mechanically coupling the low spool gearbox (130; 230; 330) to the high spool gearbox (120; 320). The turbine engine (110; 310) includes a low-pressure spool and a high-pressure spool. The low spool gearbox (130; 230; 330) is disposed within a core compartment (115) of the turbine engine (110; 310). The low spool gearbox (130; 230; 330) is configured to transfer mechanical power between the low-pressure spool and a first accessory. The high spool gearbox (120; 320) is disposed within the core compartment (115) of the turbine engine (110; 310). The high spool gearbox (120; 320) is configured to transfer mechanical power between the high-pressure spool and a second accessory.