An assembly for an aircraft with an engine includes an attachment device intended to support the engine, a pod intended to surround the engine and including a cover, joints intended to allow articulation of the cover and allow movement of the cover relative to the attachment device between a closed
An assembly for an aircraft with an engine includes an attachment device intended to support the engine, a pod intended to surround the engine and including a cover, joints intended to allow articulation of the cover and allow movement of the cover relative to the attachment device between a closed position and an open position, and at least one access panel mounted moveably on the cover between a closed position, in which the access panel extends continuously between the cover and the attachment device when the cover is in the closed position, and an open position in which the access panel is remote from its closed position. The assembly includes a handle which can be operated from the outside of the cover between a first position and a second position, and a transmission system provided to move said or each access panel from its closed position to its open position.
대표청구항▼
1. An aircraft engine assembly, said assembly comprising: an attachment device configured to support the engine and comprising a gasket: a pod configured to surround the engine and comprising a cover;a plurality of joints mounted on the attachment device and configured to allow articulation of the c
1. An aircraft engine assembly, said assembly comprising: an attachment device configured to support the engine and comprising a gasket: a pod configured to surround the engine and comprising a cover;a plurality of joints mounted on the attachment device and configured to allow articulation of the cover and allow movement of the cover relative to the attachment device between a closed position and an open position; and at least one access panel having a free edge,wherein said at least one access panel is mounted moveably on the cover between a closed position, in which the access panel extends continuously between the cover and the attachment device when the cover is in the closed position with the free edge of the at least one access panel resting against the gasket, and an open position in which the access panel is remote from the closed position of the at least one access panel, the at least one access panel configured to rotate in a first rotational direction when moving from the closed position to the open position and the cover is configured to rotate in a second rotational direction, opposite to the first rotational direction, when moving from the closed position to the open position, and wherein the assembly comprises:a handle operated from the outside of the cover between a first position and a second position; anda transmission system configured to move said at least one access panel from the closed position of the at least one access panel to the open position of the at least one access panel when the handle passes from the second position of the handle to the first position of the position of the handle, and to move said at least one access panel from the open position of the at least one access panel to the closed position of the at least one access panel when the handle passes from the first position of the handle to the second position of the handle. 2. The assembly according to claim 1, wherein the cover is articulated at an upper part of the cover and the handle is arranged in a lower part of the cover. 3. The aircraft engine assembly according to claim 2, wherein the handle selectively locks and unlocks the cove. 4. The aircraft engine assembly according to claim 1, wherein the handle and the transmission system are mounted on the cover. 5. The aircraft engine assembly according to claim 1, wherein the cover has an outer wall turned towards the outside and a thermal protection arranged inside the cover, and the transmission system is arranged between the outer wall and the thermal protection. 6. The aircraft engine assembly according to claim 1, wherein said least one access panel is mounted moveably in rotation on the cover via a hinge mounted on the inside relative to the cover. 7. The aircraft engine assembly according to claim 6, wherein the hinge is a piano hinge. 8. The aircraft engine assembly according to claim 1, wherein the transmission system comprises: a return means configured to force the at least one access panel into the closed position;a lever mounted moveably between an extended position in which the lever presses against the at least one access panel and forces the at least one access panel into the open position, and a retracted position in which the lever does not force the at least one access panel;a cable, one end of which is fixed to the handle and the other end of which is fixed to the lever; anda set of pulleys along which the cable is routed. 9. The aircraft engine assembly according to claim 1, wherein the transmission system comprises: a return means configured to force the at least one access panel into the open position,a cable, one end of which is fixed to the handle and the other end of which is fixed to the at least one access panel, anda set of pulleys along which the cable is routed. 10. An aircraft comprising an engine and an assembly, the assembly comprising: an attachment device configured to support the engine and comprising a gasket: a pod configured to surround the engine and comprising a cover; a plurality of joints configured to allow articulation of the cover and allow movement of the cover relative to the attachment device between a closed position and an open position; and at least one access panel having a free edge,wherein said at least one access panel is mounted moveably on the cover between a closed position, in which the access panel extends continuously between the cover and the attachment device when the cover is in the closed position with the free edge resting against the gasket, and an open position in which the access panel is remote from the closed position of the at least one access panel, the at least one access panel configured to rotate in a first rotational direction when moving from the closed position to the open position and the cover is configured to rotate in a second rotational direction, opposite to the first rotational direction, when moving from the closed position to the open position,wherein the assembly comprises:a handle operated from the outside of the cover between a first position and a second position; and a transmission system configured to move said at least one access panel from the closed position of the at least one access panel to the open position of the at least one access panel when the handle passes from the second position of the handle to the first position of the handle, and to move said at least one access panel from the open position of the at least one access panel to the closed position of the at least one access panel when the handle passes from the first position of the handle to the second position of the handle, wherein the attachment device is configured to support the engine, and wherein the pod is configured to surround the engine.
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이 특허에 인용된 특허 (7)
Banks Eddie D. (Renton WA) Hamatani Tomio (Seattle WA) Kishi Hajime (Kagamihara WA JPX) Odell Richard B. (Kirkland WA) Urasawa Takayoshi (Bellvue WA), Aircraft door hinge mechanism.
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