Aircraft engine unit comprising an improved front engine attachment
AssigneeAirbus Operations GmbH
InventorsFrederic Journade, Eric Renaud, Laurent Agostini
Life of this patent
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Abstract
An aircraft engine unit comprising an engine, a mast and an engine connection connecting the engine and the mast. The aircraft engine unit includes a front engine attachment of the engine connection which comprises at least one front rod connecting the primary structure of the mast and the core of the engine and which assures the take-up of vertical forces, and at least one connection connecting the primary structure of the mast and the fan casing of the engine and which assures the take-up of forces that are horizontal and perpendicular to the axis of rotation of the engine and/or a torque about the axis of rotation of the engine.
Claims5
An aircraft engine unit comprising an engine, a mast and a nacelle in which there is positioned the engine,
- the engine comprising:
- a core which comprises a stator, a rotor, and a front bearing between the stator and the rotor, the rotor pivoting about an axis of rotation relative to the stator and the front bearing assuring the guidance in rotation of the rotor relative to the stator and positioned further to a front of the engine,
- a fan connected to the rotor and positioned in a fan casing,
- the mast comprising a primary structure connected to the engine by an engine connection which comprises:
- a rear engine attachment which connects an intermediate part of the primary structure and the core of the engine,
- a front engine attachment which connects a front end of the primary structure and the engine, and
- at least two thrust rods,
- the front engine attachment comprising
- at least one connection which connects the primary structure of the mast and the fan casing of the engine, and
- at least one front rod which connects the primary structure of the mast and the core of the engine, and
- wherein each front rod is connected at a first end to a front end of the primary structure of the mast by a connection pivoting about a horizontal axis perpendicular to the axis of rotation, and is connected at a second end to the stator of the engine by a connection pivoting about a horizontal axis perpendicular to the axis of rotation, wherein an orientation of the front rod is convergent with the axis of rotation in a plane perpendicular to the axis of rotation, the plane perpendicular containing the front bearing assuring the guidance in rotation of the rotor relative to the stator and positioned further to the front of the engine.
An aircraft comprising at least one engine unit comprising an engine, a mast and a nacelle in which there is positioned the engine,
- the engine comprising:
- a core which comprises a stator, a rotor, and a front bearing between the stator and the rotor, the rotor pivoting about an axis of rotation relative to the stator and the front bearing assuring the guidance in rotation of the rotor relative to the stator and positioned further to a front of the engine,
- a fan connected to the rotor and positioned in a fan casing,
- the mast comprising a primary structure connected to the engine by an engine connection which comprises:
- a rear engine attachment which connects an intermediate part of the primary structure and the core of the engine,
- a front engine attachment which connects a front end of the primary structure and the engine, and
- at least two thrust rods,
- the front engine attachment comprising
- at least one connection which connects the primary structure of the mast and the fan casing of the engine, and
- at least one front rod which connects the primary structure of the mast and the core of the engine, and
- wherein each front rod is connected at a first end to a front end of the primary structure of the mast by a connection pivoting about a horizontal axis perpendicular to the axis of rotation, and is connected at a second end to the stator of the engine by a connection pivoting about a horizontal axis perpendicular to the axis of rotation, wherein an orientation of the front rod is convergent with the axis of rotation in a plane perpendicular to the axis of rotation, the plane perpendicular containing the front bearing assuring the guidance in rotation of the rotor relative to the stator and positioned further to the front of the engine.
Dependencies are inferred from the claim text.