Locking system for air intake structure for turbojet engine nacelle
The invention relates to a nacelle for a turbojet engine that includes an air intake structure capable of directing an air flow towards a fan of the turbojet engine, and a middle structure for surrounding said fan and to which is attached the air intake structure in order to provide aerodynamic continuity, wherein the air intake structure includes at least one inner panel attached to the middle structure and defining, with the latter, a nacelle fixed structure and at least one outer longitudinal panel removably attached to the fixed structure and including an air intake lip in order to define a removable air intake structure, wherein the removable air intake structure is provided with a locking device including at least one electric lock capable of interaction with a complementary retention structure.
1. A nacelle for a turbojet engine, comprising:
an air intake structure configured to direct an air flow towards a fan of the turbojet engine; and
a middle structure configured to surround said fan and to which is attached the air intake structure in order to provide an aerodynamic continuity,
wherein the air intake structure includes at least one inner panel attached to the middle structure and defines, with the latter, a nacelle fixed structure, the air intake structure further including at least one outer longitudinal panel that includes an air intake lip in order to define a removable air intake structure that is axially movable along a rail-guideway sliding system, and
wherein the removable air intake structure is provided with peripheral locking means including at least one electric lock that interacts with a complementary retaining means,
wherein at least one of the peripheral locking means and the complementary retaining means is attached to the nacelle fixed structure, and the rail-guideway sliding system is also attached to the nacelle fixed structure, and
wherein a fitting situated on the at least one outer longitudinal panel forms an opening that is configured to provide for insertion of a tool from outside of the outer longitudinal panel such that while inserted in the opening, the tool engages with adjusting means for adjustment of a prestress of the complementary retaining means.
2. The nacelle according to claim 1 , wherein the at least one electric lock comprises a hook configured to cooperate with a corresponding yoke.
3. The nacelle according to claim 1 , wherein the at least one electric lock is situated at a level of a guide rail.
4. The nacelle according to claim 1 , wherein the at least one electric lock is associated with at least one means for detecting the locking and/or unlocking position.
5. The nacelle according to claim 1 , further comprising a member for controlling the locking means.
6. The nacelle according to claim 1 , wherein each electric locking means is configured to be locked or unlocked manually from outside of the nacelle via a hatch formed in the at least one outer longitudinal panel of the air intake structure.
7. The nacelle according to claim 1 , wherein the electric locking means are configured to receive a mechanical inhibiting rivet designed to allow blocking of the corresponding electric locking means.
8. The nacelle according to claim 1 , wherein the adjusting means comprise an adjustment screw configured to move a lug having an inclined surface so as to allow the adjustment of the prestress of the complementary retaining means along a retaining direction.
9. The nacelle according to claim 1 , wherein the adjusting means comprise a worm screw configured to cooperate with a threaded zone of said complementary retaining means so as to allow a translation of the complementary retaining means along a retaining direction.
10. The nacelle according to claim 1 , wherein the complementary retaining means are attached to the fixed structure while the at least one electric lock is attached to the removable air intake structure.