Parallel starter/generator and air turbine starter
View Patent ↗A system for starting a turbine engine is provided. The system may comprise a gearbox, an electric starter, and an air turbine starter. The gearbox may have a gearbox input shaft. The gearbox may be coupled to the turbine engine. The gearbox input shaft may be coupled to a spool of the turbine engine. The electric starter may have an electric-starter shaft. The electric-starter shaft may be coupled to the gearbox input shaft. The air turbine starter may have an air-turbine-starter shaft. The air-turbine-starter shaft may be coupled to the gearbox input shaft. The electric-starter shaft and the air-turbine-starter shaft may be radially displaced, circumferentially displaced, or both radially and circumferentially displaced, with respective to an axis of the turbine engine, from one another. The electric starter may be a starter-generator connected alternatively between an auxiliary power source and an auxiliary load.
1. A system for starting a turbine engine, comprising:
a first gearbox having a gearbox input shaft, wherein the first gearbox is coupled to the turbine engine and the gearbox input shaft is coupled to a spool of the turbine engine;
an electric starter having an electric-starter shaft;
an air turbine starter having an air-turbine-starter shaft coupled to the gearbox input shaft; and
a second gearbox, wherein the second gearbox is separated from the first gearbox by the electric starter and the air turbine starter, wherein the electric starter outputs to the second gearbox via the electric-starter shaft, and wherein the second gearbox outputs to the air turbine starter via a second gearbox shaft,
wherein the electric-starter shaft and the air-turbine-starter shaft are radially displaced, circumferentially displaced, or both radially and circumferentially displaced, with respect to an axis of the turbine engine, from one another; and wherein the electric starter is a starter-generator connected alternatively between an auxiliary power source and an auxiliary load.
2. The system of claim 1 , wherein the air-turbine-starter shaft is selectively coupleable to the gearbox input shaft.
3. The system of claim 1 , further comprising a mounting member coupling one of the electric starter and the air turbine starter to a casing of the turbine engine.
4. The system of claim 3 , wherein the mounting member comprises a damping member.
5. The system of claim 1 , wherein both of the electric starter and the air turbine starter are located on the same side of the first gearbox.
6. The system of claim 1 , wherein the electric-starter shaft is radially displaced, with respect to the axis of the turbine engine, from the gearbox input shaft.
7. A system for starting a turbine engine, comprising:
a gearbox having a gearbox input shaft, the gearbox coupled to the turbine engine;
an electric starter having an electric-starter shaft, wherein the electric starter is a starter-generator connected alternatively between an auxiliary power source and an auxiliary load;
an air turbine starter having an air-turbine-starter shaft, the air turbine starter coupled to the gearbox input shaft; and
a second gearbox, wherein the second gearbox is separated from the first gearbox by the electric starter and the air turbine starter, wherein the electric starter outputs to the second gearbox via the electric-starter shaft, and wherein the second gearbox outputs to the air turbine starter via a second gearbox shaft,
wherein only one of the electric-starter shaft or the air-turbine-starter shaft is coaxial with the gearbox input shaft.
8. The system of claim 7 , wherein the air-turbine-starter shaft is selectively coupleable to the gearbox input shaft.
9. The system of claim 7 , further comprising a mounting member coupling one of the electric starter and the air turbine starter to a casing of the turbine engine.
10. The system of claim 9 , wherein the mounting member comprises a damping member.
11. The system of claim 7 , wherein both of the electric starter and the air turbine starter are located on the same side of the first gearbox.
12. The system of claim 7 , wherein the electric-starter shaft is selectively coupleable to the gearbox input shaft.
13. The system of claim 7 , wherein the electric-starter shaft the air-turbine-starter shaft are radially displaced, circumferentially displaced, or both radially and circumferentially displaced, with respect to an axis of the turbine engine, from one another.
14. A method of operating a turbine starting system, the turbine starting system comprising a first gearbox having a gearbox input shaft, the first gearbox coupled to a turbine engine, an electric starter having an electric-starter shaft, and an air turbine starter having an air-turbine-starter shaft, said air-turbine-starter shaft coupled to the gearbox input shaft, and a second gearbox, wherein the second gearbox is separated from the first gearbox by the electric starter and the air turbine starter, wherein the electric starter outputs to the second gearbox via the electric-starter shaft, wherein the second gearbox outputs to the air turbine starter via a second gearbox shaft, wherein only one of the electric-starter shaft or air-turbine-starter shaft is coaxial with the gearbox input shaft, the method comprising: rotating the gearbox input shaft, wherein the rotation of the gearbox input shaft rotates the turbine engine; and rotating the electric starter.
15. The method of claim 14 , further comprising:
rotating the air turbine starter, wherein the rotation of the air turbine starter causes the rotation of the gearbox input shaft and the electric starter.