Lubrication device for a turbine engine
View Patent ↗The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe ( 23 ) provided with a pump ( 24 ) for supplying oil and control means ( 30 ) located downstream from the supply pump ( 24 ), a supply pipe ( 26 ) intended for supplying oil to a member to be lubricated and a recirculation pipe ( 27 ) connected upstream from the supply pump ( 24 ), the control means ( 30 ) making it possible to direct all or part of the flow of oil from the intake pipe ( 23 ) towards the supply pipe ( 26 ) and/or towards the recirculation pipe ( 27 ).
1. A lubrication device for a turbine engine, comprising an oil intake pipe provided with a supply pump for supplying oil and control means located downstream from the supply pump, a supply pipe configured to supply oil to a speed reduction gear to be lubricated and a recirculation pipe connected upstream from the supply pump, the control means making it possible to direct all or part of the flow of oil from the intake pipe towards the supply pipe and/or towards the recirculation pipe, with the supply pump being driven by at least one rotating member of an accessory gear box of the turbine engine, wherein the control means comprise a translationally mobile member, the position of which makes it possible to adapt the oil rates sent to the supply pipe and to the recirculation pipe respectively, with said mobile member being coupled to a centrifugal governor able to modify the position of said mobile member according to the speed of rotation of an input shaft of the governor.
2. The lubrication device according to claim 1 , wherein the centrifugal governor comprises:
the input shaft which comprises a rotating input shaft,
a translationally mobile output member connected to the control means mobile member,
a first and a second link each comprising a first and a second end, with the first ends of the first and second links being mutually articulated at a first pivot member which can be translationally moved in parallel with the rotating input shaft,
a third and a fourth link each comprising a first and a second end, with the first ends of the third and fourth links being respectively articulated on the second ends of the first and second links respectively at a second and a third pivot member, with the second ends of the third and fourth links being mutually articulated at a fourth pivot member which is stationary relative to the rotating input shaft,
a fifth and a six link each comprising a first and a second end, with the first ends of the fifth and six links being mutually articulated at the fourth pivot member,
a seventh and an eighth link each comprising a first and a second end, with the first ends of the seventh and eighth links being respectively articulated on the second ends of the fifth and six links respectively at a fifth and a sixth pivot member, with the second ends of the seventh and eighth links being mutually articulated at a seventh pivot member which can be translationally moved in parallel with the rotating input shaft,
at least one of the second, third, fifth and sixth pivot members comprising at least one weight, with the translationally mobile output member being connected with the first and/or the seventh pivot members.
3. The lubrication device according to claim 2 , wherein at least one return elastic member is so arranged as to move the first pivot member away from the fourth pivot member and/or to move the fourth pivot member away from the seventh pivot member.
4. The lubrication device according to claim 1 , wherein the control means comprise at least a mobile slide valve, with the slide position making it possible to adapt the oil rates sent to the supply pipe and to the recirculation pipe, respectively.
5. A turbine engine comprising the lubrication device according to claim 1 , a first and a second contra-rotating impeller driven into rotation by a low pressure turbine, through the speed reduction gear, with the governor input shaft being driven into rotation by one element of the speed reduction gear or the low pressure turbine.
6. The turbine engine according to claim 5 , further comprising a high pressure body comprising a high pressure compressor and a high pressure turbine rotationally coupled by a first shaft, and an additional body comprising a low pressure compressor and an intermediate pressure turbine, rotationally coupled by a second shaft, with the speed of rotation of the accessory gear box rotating member depending on the speed of rotation of the shaft of the high pressure body.
7. The lubrication device according to claim 1 , wherein the speed reduction gear comprises an epicyclic speed reduction gear.