Remote mounted accessory gearbox

Patent metadata

Field	Value
Publication number	US-12540579-B2
Application number	US-202418654628-A
Country	US
Kind code	B2
Filing date	May 3, 2024
Priority date	May 3, 2024
Publication date	Feb 3, 2026
Grant date	Feb 3, 2026

Abstract

An apparatus includes an engine and an accessory gearbox. The engine is positioned on a top side of an aircraft. The accessory gearbox is mounted with an airframe of the aircraft remote from the engine, wherein the accessory gearbox is drivingly connected to the engine.

First claim

What is claimed is:

1 . An apparatus comprising:
an engine positioned on a top side of an aircraft; an accessory gearbox mounted within an airframe of the aircraft and remote from the engine; and a tower shaft extending from the engine through the airframe to the accessory gearbox and configured to drivingly connect the engine to the accessory gearbox, wherein the tower shaft comprises:
a first flex joint adjacent the engine, the first flex joint configured to accommodate movement of the engine in relation to the accessory gearbox; and
a second flex joint adjacent the accessory gearbox, the second flex joint configured to accommodate movement of the accessory gearbox in relation to the engine.

2 . The apparatus of claim 1 , further comprising:
a reduction gearbox arranged between a main shaft of the engine and the tower shaft, the reduction gearbox configured to rotate the tower shaft at a different rotation speed than the main shaft.

3 . The apparatus of claim 1 , wherein the accessory gearbox includes:
a first shaft configured to drive a first accessory; and a first set of gears arranged between the tower shaft and the first shaft, the first set of gears configured to rotate the first shaft at a different rotational speed than the tower shaft.

4 . The apparatus of claim 3 , wherein the accessory gearbox includes:
a second shaft configured to drive a second accessory; and a second set of gears arranged between the tower shaft and the second shaft, the second set of gears configured to rotate the second shaft at a different rotational speed than the tower shaft.

5 . The apparatus of claim 4 , wherein a rotational speed of the second shaft is different than a rotational speed of the first shaft.

6 . The apparatus of claim 1 , further comprising an accessory driven by the accessory gearbox, wherein the accessory is one of a fuel pump, a hydraulic pump, an oil pump, an electric generator, a permanent magnet alternator, or a manual engine starter.

7 . The apparatus of claim 1 , further comprising:
an engine controller mounted to the accessory gearbox and configured to remotely control the engine; at least one sensor mounted on the engine; and a remote interface unit operably coupled to the at least one sensor and configured to transmit outputs of the at least one sensor to the engine controller and control the engine based on signals received from the engine controller.

8 . The apparatus of claim 1 , further comprising a fuel tank mounted at an elevation equal to or above the accessory gearbox.

9 . The apparatus of claim 1 , wherein the first flex joint is one of a universal joint or a constant velocity joint.

10 . An apparatus comprising:
an engine; an accessory gearbox mounted remotely from the engine at an elevation equal to or below a fuel tank; and a tower shaft extending from the engine to the accessory gearbox and configured to drivingly connect the engine to the accessory gearbox, wherein the tower shaft includes:
a first flex joint adjacent the accessory gearbox, the first flex joint configured to accommodate movement of the accessory gearbox in relation to the engine; and
a second flex joint adjacent to the engine, the second flex joint configured to accommodate movement of the engine in relation to the accessory gearbox.

11 . The apparatus of claim 10 , further comprising:
a reduction gearbox arranged between a main shaft of the engine and the tower shaft, the reduction gearbox configured to rotate the tower shaft at a different rotation speed than the main shaft.

12 . The apparatus of claim 10 , wherein the accessory gearbox includes:
a first shaft configured to drive a first accessory; and a first set of gears arranged between the tower shaft and the first shaft, the first set of gears configured to rotate the first shaft at a different rotational speed than the tower shaft.

13 . The apparatus of claim 12 , wherein the accessory gearbox includes:
a second shaft configured to drive a second accessory; and a second set of gears arranged between the tower shaft and the second shaft, the second set of gears configured to rotate the second shaft at a different rotational speed than the tower shaft.

14 . The apparatus of claim 13 , wherein a rotational speed of the second shaft is different than a rotational speed of the first shaft.

15 . The apparatus of claim 10 , further comprising a fuel pump driven by the accessory gearbox, wherein the fuel pump provides fuel from the fuel tank to the engine.

16 . The apparatus of claim 10 , further comprising:
an engine controller mounted to the accessory gearbox and configured to remotely control the engine; at least one sensor mounted on the engine; and a remote interface unit operably coupled to the at least one sensor and configured to transmit outputs the of at least one sensor to the engine controller and control the engine based on signals received from the engine controller.

17 . The apparatus of claim 10 , further comprising an aircraft airframe, wherein the engine is positioned on a top side of the airframe.

18 . The apparatus of claim 10 , wherein the first flex joint is one of a universal joint or a constant velocity joint.

19 . An apparatus comprising:
an engine positioned on a top side of an aircraft; an accessory gearbox mounted within an airframe of the aircraft and remote from the engine; a fuel tank mounted at an elevation equal to or above the accessory gearbox; and a tower shaft extending from the engine through the airframe to the accessory gearbox and configured to drivingly connect the engine to the accessory gearbox, wherein the tower shaft comprises a first flex joint adjacent the engine, the first flex joint configured to accommodate movement of the engine in relation to the accessory gearbox.

20 . An apparatus comprising:
an engine; an aircraft airframe, wherein the engine is positioned on a top side of the airframe; an accessory gearbox mounted remotely from the engine at an elevation equal to or below a fuel tank; and a tower shaft extending from the engine to the accessory gearbox and configured to drivingly connect the engine to the accessory gearbox, wherein the tower shaft includes a first flex joint adjacent the accessory gearbox, the first flex joint configured to accommodate movement of the accessory gearbox in relation to the engine.

Assignees

• Rtx Corp

Inventors

• Hanrahan Paul R
• Poth Jr Stefan M
• Schafer Bradley C

Classifications

• F05D2260/4031

  as in toothed gearing · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• B64D2033/0293

  for turboprop engines · CPC title

• B64D2033/0286

  for turbofan engines · CPC title

• B64D2033/0273

  for jet engines · CPC title