1. A gas turbine engine, comprising:
a nacelle having an inner wall providing a bypass duct of a gas turbine engine, and an outer wall;
an accessory gearbox being received between the inner wall and the outer wall of the nacelle; and
an accessory drive of the accessory gearbox, the accessory drive configured to rotate about an accessory drive axis that is transverse to a central axis of the gas turbine engine.
2. The gas turbine engine of claim 1, including an oil pump rotatably coupled to the accessory drive.
3. The gas turbine engine of claim 1, including a hydraulic pump rotatably coupled to the accessory drive.
4. The gas turbine engine of claim 1, including a driveshaft extending through the inner wall, the driveshaft to be connected to the gas turbine engine, wherein the driveshaft and the accessory gearbox circumferentially overlap relative to the central axis.
5. The gas turbine engine of claim 4, wherein the driveshaft is positioned circumferentially between a four o’clock and a five o’clock position.
6. The gas turbine engine of claim 4, including a bevel gear rotatably coupling rotation of the driveshaft with the accessory drive.
7. The gas turbine engine of claim 1, wherein the gearbox is received axially between an upstream end and a downstream end of the nacelle.
8. The gas turbine engine of claim 1, wherein the accessory drive axis extends tangentially relative to the nacelle.
9. The gas turbine engine of claim 1, wherein the accessory drive axis is perpendicular to the central axis.
10. The gas turbine engine of claim 1, wherein the accessory drive is a first accessory drive, and including at least one second accessory drive of the gearbox, the at least one second accessory drive configured to rotate about a respective accessory drive axis that is aligned with the central axis.
11. The gas turbine engine of claim 10, wherein the first accessory drive is downstream from the at least one second accessory drive relative to a direction of flow through the gas turbine engine.
12. The gas turbine engine of claim 11, including a third accessory drive configured to rotate about an axis that is upstream from the at least one accessory drive relative to a direction of flow through the gas turbine engine.
13. The gas turbine engine of claim 1, wherein the accessory gearbox has a \u201cT\u201d shaped configuration and the accessory drive is a first accessory drive, and including at least one second accessory drive of the gearbox, the at least one second accessory drive configured to rotate about a respective accessory drive axis that is aligned with the central axis, the first accessory drive upstream from at least one second accessory drive.
14. The gas turbine engine of claim 1, wherein the accessory gearbox has a \u201cI\u201d shaped configuration and the accessory drive is a first accessory drive, and including at least one second accessory drive of the gearbox configured to rotate about a respective accessory drive axis that is transverse with the central axis, the first and second accessory drives engaging opposing sides of the accessory gearbox.
15. A gas turbine engine comprising:
a fan, a compressor section, a combustor section, and a turbine section, the turbine section configured to drive a shaft to rotatably drive the fan and the compressor, at least one driveshaft to be connected for rotation with the turbine section;
an accessory gearbox configured to rotatably drive an accessory at a drive location on a circumferentially facing side of the accessory gearbox; and
a nacelle having an inner wall defining a bypass duct receiving bypass air from the fan, and an outer wall, the at least one driveshaft extending through the inner wall, and being connected to drive the accessory gearbox received between the inner and outer walls of the nacelle.
16. The gas turbine engine of claim 15, wherein the accessory drive axis is perpendicular to the central axis.
17. The gas turbine engine of claim 16, wherein the driveshaft is configured to rotate about a radially extending driveshaft axis, and the accessory drive axis is perpendicular to the driveshaft axis.
18. The gas turbine engine of claim 16, wherein the drive location is a first drive location, and the gearbox includes a second drive location on the circumferentially facing side of the accessory gearbox, and at least one third drive location on an axially facing side of the accessory gearbox, the first drive location downstream from the third drive location and the second drive location upstream from the third drive location relative to a direction of flow through the gas turbine engine.
19. A method of providing a gearbox drive location within a gas turbine engine, comprising:
providing a nacelle having an inner wall defining a bypass duct of a gas turbine engine, and an outer wall;
providing an accessory gearbox between the inner wall and the outer wall of the nacelle; and
providing an accessory drive location from the accessory gearbox, the accessory drive location configured to rotate about an accessory drive axis that is transverse to a central axis of the gas turbine engine.
20. The method of claim 19, including providing another accessory drive location from the accessory gearbox that is configured to rotate about an accessory drive axis aligned with the central axis of the gas turbine engine.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. An electronic device comprising:
circuitry configured to
set one or more non-Guaranteed Bit Rate bearers in association with one or more packet data network connections for uplink packet communication;
receive a parameter corresponding to an Aggregate Maximum Bit Rate, AMBR, for uplink packet transmission via the non-Guaranteed Bit Rate bearers and a priority value for each of the plurality of non-Guaranteed Bit Rate bearers; and
control the uplink packet transmission of one or more non-Guaranteed Bit Rate bearers based on the Aggregate Maximum Bit Rate and the priority values.
2. The electronic device of claim 1, wherein the circuitry is further configured to:
receive control information including a Packet Data Network (PDN) gateway identifier, wherein the gateway is a node to a packet data network.
3. The electronic device of claim 1, wherein
the parameter corresponding to the Aggregate Maximum Bit Rate is received from infrastructure equipment.
4. The electronic device of claim 1, wherein
at least one radio resource of the non-Guaranteed Bit Rate bearers is allocated based on the parameter corresponding to the Aggregate Maximum Bit Rate.
5. The electronic device of claim 1, wherein
an aggregated bit rate of uplink packet via the non-Guaranteed Bit Rate bearers is limited based on the parameter corresponding to AMBR.
6. A mobile station comprising:
an antenna unit; and
circuitry configured to
set one or more non-Guaranteed Bit Rate bearers in association with one or more packet data network connections for uplink packet communication;
receive a parameter corresponding to an Aggregate Maximum Bit Rate for uplink packet transmission via the non-Guaranteed Bit Rate bearers and a priority value for each of the plurality of non-Guaranteed Bit Rate bearers; and
control the uplink packet transmission of one or more non-Guaranteed Bit Rate bearers based on the Aggregate Maximum Bit Rate and the priority values.
7. The mobile station of claim 6, wherein the circuitry is further configured to:
receive control information including a Packet Data Network (PDN) gateway identifier, wherein the gateway is a node to a packet data network (PDN).
8. The mobile station of claim 6, wherein
the parameter corresponding to the Aggregate Maximum Bit Rate is received from infrastructure equipment.
9. The mobile station of claim 6, wherein
at least one radio resource of the non-Guaranteed Bit Rate bearers is allocated based on the parameter corresponding to the Aggregate Maximum Bit Rate.
10. The mobile station of claim 6, wherein
An aggregated bit rate of uplink packet via the non-Guaranteed Bit Rate bearers is limited based on the parameter corresponding to AMBR.
11. A communication method comprising:
setting one or more non-Guaranteed Bit Rate bearers in association with one or more packet data network connections for uplink packet communication;
receiving a parameter corresponding to an Aggregate Maximum Bit Rate for uplink packet transmission via the non-Guaranteed Bit Rate bearers and a priority value for each of the plurality of non-Guaranteed Bit Rate bearers; and
controlling, by circuitry, the uplink packet transmission of one or more non-Guaranteed Bit Rate bearers based on the Aggregate Maximum Bit Rate and the priority values.
12. The method of claim 11, further comprising:
receiving control information including a Packet Data Network (PDN) gateway identifier, wherein the gateway is a node to a packet data network (PDN).
13. The method of claim 11, wherein
the parameter corresponding to the Aggregate Maximum Bit Rate is received from infrastructure equipment.
14. The method of claim 11, wherein
at least one radio resource of the non-Guaranteed Bit Rate bearers is allocated based on the parameter corresponding to the Aggregate Maximum Bit Rate.
15. The method of claim 11, wherein
an aggregated bit rate of uplink packet via the non-Guaranteed Bit Rate bearers is limited based on the parameter corresponding to AMBR.
16. An electronic device comprising:
means for setting one or more non-Guaranteed Bit Rate bearers in association with one or more packet data network connections for uplink packet communication;
means for receiving a parameter corresponding to an Aggregate Maximum Bit Rate for uplink packet transmission via the non-Guaranteed Bit Rate bearers and a priority value for each of the plurality of non-Guaranteed Bit Rate bearers; and
means for controlling the uplink packet transmission of one or more non-Guaranteed Bit Rate bearers based on the Aggregate Maximum Bit Rate and the priority values.