Systems and methods for providing mechanical power to an aircraft accessory with a turbine engine
US-11591967-B2 · Feb 28, 2023 · US
US12540578B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12540578-B2 |
| Application number | US-202418404185-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 4, 2024 |
| Priority date | Jan 4, 2024 |
| Publication date | Feb 3, 2026 |
| Grant date | Feb 3, 2026 |
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A hybrid electric gas turbine engine two speed transmission for a low spool drive including an accessory gearbox in operative communication with a low speed spool motor-generator; a transmission in operative communication with the accessory gearbox and the low speed spool motor-generator; a low speed spool angled gearbox in operative communication with the transmission; and a low speed spool in operative communication with the low speed spool angled gearbox.
Opening claim text (preview).
What is claimed is: 1 . A hybrid electric gas turbine engine two speed transmission for a low spool drive comprising: an accessory gearbox in operative communication with a low speed spool motor-generator; a transmission in operative communication with the accessory gearbox and the low speed spool motor-generator, wherein the transmission comprises a two speed transmission configured for hybrid electric low spool drive applications, the two speed transmission comprises clutch packs and an epicyclic geartrain configured to reduce a speed range at the low speed spool motor-generator; a low speed spool angled gearbox in operative communication with the transmission; and a low speed spool in operative communication with the low speed spool angled gearbox, wherein the accessory gearbox is in operative communication with a first high speed spool motor-generator and a second high speed spool motor-generator, and wherein the accessory gearbox is in operative communication with a high speed spool via a high speed spool angled gearbox. 2 . The hybrid electric gas turbine engine two speed transmission for a low spool drive according to claim 1 , wherein the accessory gearbox is in operative communication with an oil pump and a fuel pump. 3 . The hybrid electric gas turbine engine two speed transmission for a low spool drive according to claim 1 , wherein the transmission and low speed spool angled gearbox are integrally formed sharing a common housing. 4 . The hybrid electric gas turbine engine two speed transmission for a low spool drive according to claim 1 , wherein the transmission is bolted to the accessory gearbox configured as a line removeable unit. 5 . A hybrid electric gas turbine engine two speed transmission for a low spool drive comprising: an engine structure proximate a compressor of the gas turbine engine; a low speed spool towershaft coupled to the engine structure; a low speed spool angled gearbox in operative communication with the towershaft and in operative communication with a low speed spool of the gas turbine engine; a transmission in operative communication with the low speed spool angled gearbox, wherein the transmission comprises a two speed transmission configured for hybrid electric low spool drive applications, the two speed transmission comprises clutch packs and an epicyclic geartrain configured to reduce a speed range at the low speed spool motor-generator; an accessory gearbox in operative communication with the transmission; and a low speed spool motor-generator in operative communication with the accessory gearbox, wherein the accessory gearbox is in operative communication with a first high speed spool motor-generator and a second high speed spool motor-generator, and wherein the accessory gearbox is in operative communication with a high speed spool via a high speed spool angled gearbox. 6 . The hybrid electric gas turbine engine two speed transmission for a low spool drive according to claim 5 , wherein the transmission is bolted to the accessory gearbox configured as a line removeable unit. 7 . The hybrid electric gas turbine engine two speed transmission for a low spool drive according to claim 5 , wherein the transmission and low speed spool angled gearbox are integrally formed sharing a common housing. 8 . A process for a hybrid electric gas turbine engine two speed transmission for a low spool drive comprising: providing an engine structure proximate a compressor of the gas turbine engine; coupling a low speed spool towershaft to the engine structure; coupling a low speed spool angled gearbox in operative communication with the towershaft; coupling the low speed spool angled gearbox in operative communication with a low speed spool of the gas turbine engine; coupling a transmission in operative communication with the low speed spool angled gearbox, configuring the transmission as a two speed transmission configured for hybrid electric low spool drive applications, the two speed transmission comprises clutch packs and an epicyclic geartrain; configuring the clutch packs and epicyclic geartrain to reduce a speed range at the low speed spool motor-generator; coupling an accessory gearbox in operative communication with the transmission; and coupling a low speed spool motor-generator in operative communication with the accessory gearbox, wherein the accessory gearbox is coupled in operative communication with a first high speed spool motor-generator and a second high speed spool motor-generator, and wherein the accessory gearbox is coupled in operative communication with a high speed spool via a high speed spool angled gearbox. 9 . The process of claim 8 , further comprising: integrally forming the transmission and low speed spool angled gearbox sharing a common housing. 10 . The process of claim 8 , further comprising: configuring the two-speed transmission for two operational modes. 11 . The process of claim 8 , wherein the two operational modes comprise: a first operational MODE 1 configured as a direct drive to the low spool motor-generator for high speed operation of the low speed spool; and a second operational MODE 2 configured to provide up to a 3× increase in motor shaft speed wherein the transmission includes a gear ratio of 3.0 which increases motor speed for low speed spool operation selected from the group comprising a ground idle speed and a flight idle speed. 12 . The process of claim 8 , further comprising: configuring the transmission for a low spool drive power extraction wherein the low spool drive power extraction is arranged for A/C loads and battery recharge. 13 . The process of claim 8 , further comprising: configuring the transmission for a low spool drive power injection on ground.
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