Gas turbine engine comprising a starter in the auxiliary gear box
View Patent ↗A gas turbine engine incorporating a starter mounted on the gear box is disclosed. The gas turbine engine includes an AGB gear housing mechanically connected with an engine shaft for driving auxiliary machines and an air starter mounted on the housing, the starter and housing enclosures being in communication such that the lubricating oil of the starter should be distributed from the AGB housing. The oil enclosure of the starter is pressurized by a source of air, being independent from the AGB housing. Advantageously, the pressurization air is taken from a pressurization enclosure of an engine bearing.
1. A gas turbine engine, comprising:
an AGB gear housing mechanically connected with an engine shaft for driving auxiliary machines and an air starter mounted on the housing, the starter and housing enclosures being in communication such that lubricating oil of the starter be distributed from the AGB housing,
wherein the oil enclosure of the starter is pressurized by a source of air, being independent from the AGB housing.
2. An engine according to claim 1 , wherein pressurization air flows into an interface area between a casing of the starter and that of the housing.
3. An engine according to claim 2 , wherein an air return is arranged between the starter and the housing at a lower pressure than pressurization air supply pressure.
4. An engine according to claim 3 , wherein the air return is fed towards a de-oiler.
5. An engine according to claim 4 , comprising an air return towards an internal enclosure of a turbojet engine bearing.
6. An engine according to claim 1 , wherein, with a double seal of a rotary assembly of the starter being arranged on a side of an air turbine, pressurization air flows between both seals forming the double seal.
7. An engine according to claim 6 , wherein an air return is arranged between the starter and the housing at a lower pressure than pressurization air supply pressure.
8. An engine according to claim 7 , wherein the air return is fed towards a de-oiler.
9. An engine according to claim 1 , wherein pressurization air is taken from an external pressurization enclosure of a turbojet engine bearing.
10. An engine according to claim 8 , comprising an air return towards an internal enclosure of a turbojet engine bearing.