Oil collector for a torque transmission device of an aircraft turbine engine
AssigneesSafran, Safran Transmission Systems
InventorsBoris Pierre Marcel Morelli, Xavier Roger Betbeder-Lauque, Mathieu Jean Charrier
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Abstract
An oil collector for a torque transmission device of an aircraft turbine engine, this oil collector being configured to collect sprayed oil, wherein it includes at least one wall formed at least in part by a mesh structure, and at least one recovery device located at one end of the wall and configured to recover the oil captured by the wall and intended to flow from this wall to the recovery device.
Claims19
An oil collector for a torque transmission device of an aircraft turbine engine, this oil collector being configured to collect sprayed oil, wherein it comprises:
- at least one outer wall formed at least in part by a porous lattice structure, said porous lattice structure being suitable to capture oil, and
- at least one oil recovery device located at one end of the at least one outer wall and configured to recover the oil captured by said porous lattice structure and intended to flow from said porous lattice structure to the at least one oil recovery device,
- wherein said porous lattice structure is composed of parallelepipedal patterns,
- wherein each of said patterns comprises bars connected to each other.
An oil collector for a torque transmission device of an aircraft turbine engine, this oil collector being configured to collect sprayed oil, wherein it comprises:
- at least one outer wall formed at least in part by a porous lattice structure, said porous lattice structure being suitable to capture oil, and
- at least one oil recovery device located at one end of the at least one outer wall and configured to recover the oil captured by said porous lattice structure and intended to flow from said porous lattice structure to the at least one oil recovery device,
- wherein said porous lattice structure is composed of parallelepipedal patterns,
- wherein each of said patterns comprises bars connected to each other, and
- wherein each of said patterns comprises eight bars.
An oil collector for a torque transmission device of an aircraft turbine engine, this oil collector being configured to collect sprayed oil, wherein it comprises:
- at least one outer wall formed at least in part by a porous lattice structure, said porous lattice structure being suitable to capture oil, and
- at least one oil recovery device located at one end of the at least one outer wall and configured to recover the oil captured by said porous lattice structure and intended to flow from said porous lattice structure to the at least one oil recovery device,
- wherein said porous lattice structure is composed of parallelepipedal patterns,
- wherein each of said patterns comprises bars connected to each other, and
- wherein each of said patterns comprises bars at least some of said bars terminating by a ball.
Dependencies are inferred from the claim text.