Turbojet nacelle having a removable air intake structure
View Patent ↗A turbojet engine nacelle, including an air intake structure for directing an airflow towards a fan of the turbojet engine, a middle structure attached to the air intake structure for surrounding the fan of the turbojet engine, the air intake structure including an inner panel attached to the middle structure and defining a fixed structure with the middle structure, and an outer panel including an air intake lip at the end thereof opposite the middle structure, the outer panel being longitudinally translatably movable relative to the inner panel. The nacelle further includes at least one rod having one end attached onto a flange of the air intake lip and a mechanism rigidly connected to the middle structure for securing and locking the other end of each rod by applying a traction force thereon.
1. A turbojet nacelle comprising:
an air intake structure for channeling a stream of air towards a fan of the turbojet;
a middle structure fastened to the air intake structure, the middle structure having an external housing with an internal casing serving to surround the fan of the turbojet;
the air intake structure comprising an internal panel fastened to the internal casing of the middle structure and co-operating therewith to form a stationary structure, and an external panel incorporating an air intake lip at an end of the external panel remote from the middle structure, the external panel being movable in longitudinal translation relative to the internal panel; and
further comprising at least one rod including a first end and a second end, the first end fastened on a flange of the air intake lip and the second end terminating in a loop; and
an attachment member hinged about a pin secured to a hatch in the external housing of the middle structure, the attachment member engaging the loop of the second end for attaching and locking the external panel to the middle structure by exerting a traction force on the at least one rod, the attachment member actuated manually by a handle housed in the hatch.
2. A nacelle according to claim 1 , wherein the at least one rod is covered in a vibration-damper material.
3. A nacelle according to claim 1 , wherein the at least one rod is held by clip-fastening in a notch formed in an inner wall of the air intake structure.
4. A nacelle according to claim 1 , wherein the flange of the air intake lip includes a plurality of centering pegs that are received in notches of complementary shapes provided in a corresponding flange of the internal panel.
5. A nacelle according to claim 1 , wherein the at least one rod is fastened to the flange of the air intake lip by a ball joint.
6. A nacelle according to claim 1 , wherein the at least one rod is made of steel.
7. A nacelle according to claim 1 , including a plurality of the at least one rod regularly distributed around a longitudinal axis of the nacelle.
8. A turbojet including a nacelle according to claim 1 .