Non-pressurized accessory gearbox
A non-pressurized accessory gearbox for an aircraft includes: a housing, one or more gears disposed within the housing, an input rotating member to receive input from a main rotor gearbox via a shaft connected to the one or more gears, and one or more output rotating members in communication with the one or more gears. The gearbox is configured to utilize splash lubrication for moving a lubrication fluid within the housing.
1. A non-pressurized accessory gearbox for an aircraft comprising:
a non-pressurized accessory gearbox housing;
one or more gears disposed within the non-pressurized accessory gearbox housing;
an input rotating member connected to the one or more gears and configured to receive input from a main rotor gearbox via a shaft connected to the one or more gears; and
one or more output rotating members in communication with the one or more gears, wherein the one or more output rotating members are configured to be connected to two or more outputs for a blower, a hydraulic pump, or an electrical generator;
wherein the non-pressurized accessory gearbox is configured to utilize splash lubrication for moving a lubrication fluid within the non-pressurized accessory gearbox housing, and wherein the non-pressurized accessory gearbox is configured to be connected to the main rotor gearbox; and
wherein a pressurized oil line for the non-pressurized accessory gearbox is excluded.
2. The non-pressurized accessory gearbox of claim 1 , wherein at least one of the one or more gears, the input rotating member, or the one or more output members are lubricated within the non-pressurized accessory gearbox housing.
3. The non-pressurized accessory gearbox of claim 1 , wherein the one or more output rotating members are configured to drive the blower, the hydraulic pump, and the electrical generator.
4. The non-pressurized accessory gearbox of claim 1 , wherein the non-pressurized accessory gearbox housing further comprises an oil level gauge in fluid communication with the lubrication fluid in the non-pressurized accessory gearbox housing and positioned to provide an indicium of a level of the lubrication fluid in the non-pressurized accessory gearbox housing when the non-pressurized accessory gearbox is not in operation.
5. The non-pressurized accessory gearbox of claim 1 , further comprising an oil level sensor that measures a level of the lubrication fluid in the non-pressurized accessory gearbox housing.
6. The non-pressurized accessory gearbox of claim 1 , wherein an external oil cooler for the non-pressurized accessory gearbox is excluded.
7. The non-pressurized accessory gearbox of claim 1 , wherein external grease-packed bearings for the non-pressurized accessory gearbox are excluded.
8. The non-pressurized accessory gearbox of claim 1 , wherein at least one of the one or more gears is a drive gear that includes two of the output rotating members, wherein a first output rotating member of the two output rotating members is a first portion of the drive gear facing in a first direction, and a second output rotating member of the two output rotating members is a second portion facing in a second direction that is opposite to the first direction.
9. The non-pressurized accessory gearbox of claim 8 , wherein the drive gear is configured to drive the blower and the electrical generator.
10. An aircraft, comprising:
a main rotor gearbox;
two non-pressurized accessory gearboxes configured to be connected to the main rotor gearbox, each of the non-pressurized accessory gearboxes comprising:
a non-pressurized accessory gearbox housing;
one or more gears disposed within the non-pressurized accessory gearbox housing;
an input rotating member connected to the one or more gears and configured to receive input from the main rotor gearbox via a shaft connected to the one or more gears; and
one or more output rotating members in communication with the one or more gears, wherein the one or more output rotating members are configured to be connected to two or more outputs for a blower, a hydraulic pump, or an electrical generator;
wherein each of the two accessory gearboxes is configured to utilize splash lubrication for moving a lubrication fluid within the non-pressurized accessory gearbox housing; and
wherein a pressurized oil line for each of non-pressurized accessory gearboxes is excluded.
11. The aircraft of claim 10 , wherein each of the two non-pressurized accessory gearboxes is connected to the main rotor gearbox via a shaft.
12. The aircraft of claim 10 , wherein at least one of the one or more gears, the input rotating member, or the first output member is lubricated within each non-pressurized accessory gearbox housing.
13. The aircraft of claim 10 , wherein the one or more output rotating members are configured to drive the blower, the hydraulic pump, and the electrical generator.
14. The aircraft of claim 10 , wherein each non-pressurized accessory gearbox housing further comprises an oil level gauge in fluid communication with the lubrication fluid and positioned to provide an indicium of a level of the lubrication fluid in the non-pressurized accessory gearbox housing when the non-pressurized accessory gearbox is not in operation.
15. The aircraft of claim 10 , further comprising an oil level sensor that measures a level of a lubrication fluid in the non-pressurized accessory gearbox housing.
16. The aircraft of claim 10 , wherein at least one of the one or more gears is a drive gear that includes two of the output rotating members, wherein a first output rotating member of the two output rotating members is a first portion of the drive gear facing in a first direction, and a second output rotating member of the two output rotating members is a second portion facing in a second direction that is opposite to the first direction.
17. The aircraft of claim 16 , wherein the drive gear is configured to drive the blower and the electrical generator.
18. A method of providing redundant accessory functions to a rotorcraft comprising:
providing a main rotor gearbox;
connecting two non-pressurized accessory gearboxes to the main rotor gearbox, each of the non-pressurized accessory gearboxes comprising:
a non-pressurized accessory gearbox housing;
one or more gears disposed within the non-pressurized accessory gearbox housing;
a lubrication fluid within the non-pressurized accessory gearbox housing;
one or more output rotating members in communication with the one or more gears wherein the one or more output rotating members are configured to be connected to two or more outputs for a blower, a hydraulic pump, or an electrical generator;
an input rotating member configured to receive input from the main rotor gearbox via a shaft, wherein the input rotating member is connected to the one or more gears in the non-pressurized accessory gearbox housing;
wherein a pressurized oil line for each of the non-pressurized accessory gearboxes is excluded; and
moving the lubrication fluid within each non-pressurized accessory gearbox housing using splash lubrication.
19. The method of claim 18 , wherein at least one of the one or more gears is a drive gear that includes two of the output rotating members, wherein a first output rotating member of the two output rotating members is a first portion of the drive gear facing in a first direction, and a second output rotating member of the two output rotating members is a second portion facing in a second direction that is opposite to the first direction.
20. The method of claim 18 , wherein the drive gear is configured to drive the blower and the electrical generator.
21. The method of claim 18 , wherein each of the two non-pressurized accessory gearboxes is connected to the main rotor gearbox via a shaft.
22. The method of claim 18 , wherein at least one of the one or more gears, the input rotating member, or at least one of the one or more output rotating members is lubricated within the non-pressurized accessory gearbox housing.
23. The method of claim 18 , further comprising providing an indicium of a level of the lubrication fluid in each non-pressurized accessory gearbox housing when the each non-pressurized accessory gearbox is not in operation using an oil level gauge in fluid communication with a lubrication fluid.
24. The method of claim 18 , further comprising measuring a level of the lubrication fluid in the non-pressurized accessory gearbox housing using an oil level sensor.
25. The method of claim 18 , wherein an external oil cooler for each of the non-pressurized accessory gearboxes is excluded.
26. The method of claim 18 , wherein external grease-packed bearings for each of the non-pressurized accessory gearboxes are excluded.
27. A method of lubricating a non-pressurized accessory gearbox comprising:
providing a lubrication fluid in a non-pressurized accessory gearbox housing comprising one or more gears;
providing an input rotating member configured to receive input from a main rotor gearbox via a shaft connected to the one or more gears;
providing one or more output rotating members connected to the one or more gears wherein the one or more output rotating members are configured to be connected to two or more outputs for a blower, a hydraulic pump, or an electrical generator; and
moving the lubrication fluid within the non-pressurized accessory gearbox housing using splash lubrication, and wherein the non-pressurized accessory gearbox is connected to the main rotor gearbox;
wherein providing a pressurized oil line for the non-pressurized accessory gearbox is excluded.