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1.发明公开公开(公告)号：US20230184194A1
公开(公告)日：2023-06-15
申请号：US17870255
申请日：2022-07-21
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Gaches , Laurent Cazeaux
Abstract: An assembly includes a structure with 6 o'clock and 12 o'clock beams and front and rear curved beams, in which the 12 o'clock beam is mounted to be able to rotate on a pylon of an aircraft between a closed position and a raised position, a fan cowl fixed to the structure, a thrust reverser with a rear cowl and that is able to move in translation along the 6 o'clock and 12 o'clock beams between a forward position and a backward position, cascades fixed to the thrust reverser, and a mover for moving the thrust reverser. With such an arrangement, the fan cowl and the thrust reverser are fixed to the same structure, and it is this structure that is hinged to the pylon.
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公开(公告)号：US20200182194A1
公开(公告)日：2020-06-11
申请号：US16695820
申请日：2019-11-26
Applicant: Airbus Operations (S.A.S.)
Inventor： Frédéric Journade , Pierre Charon , Laurent Cazeaux , Pascal Gougeon
Abstract: A propulsion system includes a bypass turbine engine and a pylon. The turbine engine includes an engine, two internal cowls, two outer cowls, a first lock for locking the internal cowls to the engine, cascades of vanes fixed to the outer cowl via hooping, wherein the outer cowls are movable in translation with respect to the engine, in which each outer cowl is able to slide parallel to a direction of translation on an internal cowl via a top guideway connection and a bottom guideway connection, and in which each outer cowl is mounted with the ability to slide parallel to the direction of translation on the pylon via an upper guideway connection. The propulsion system makes it possible during maintenance operations to move the outer cowl and the internal fixed structure towards the rear and therefore away from the front cowls to get at the engine.
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公开(公告)号：US11511875B2
公开(公告)日：2022-11-29
申请号：US16682252
申请日：2019-11-13
Applicant: Airbus Operations S.A.S.
Inventor： Wolfgang Brochard , Laurent Cazeaux , Claire Maffre
IPC: B64D33/02 , G10K11/168 , G10K11/172 , B32B3/30
Abstract: An acoustic absorption structure includes: at least one acoustic element which has at least one cavity delimited by at least one enclosure comprising at least one first drainage orifice passing through the enclosure, and a rotational indexing system making it possible to position the acoustic element so that at least one first drainage orifice is positioned in proximity to or at a lowest point of the cavity. An aircraft propulsion assembly including such an acoustic absorption structure is also described.
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公开(公告)号：US11746705B2
公开(公告)日：2023-09-05
申请号：US16682271
申请日：2019-11-13
Applicant: Airbus Operations S.A.S.
Inventor： Wolfgang Brochard , Laurent Cazeaux , Claire Maffre
IPC: F02C7/24 , B64D29/00 , G10K11/168
CPC classification number: F02C7/24 , B64D29/00 , G10K11/168 , F05D2260/96
Abstract: A method for manufacturing an acoustic element of a sound absorption structure including at least one cylindrical, conical or truncated conical chamber obtained from a flat preform shaped and then assembled in order to obtain the cylindrical, conical or truncated conical shape of the chamber. This manufacturing method makes it possible to obtain an acoustic element that has thin walls and is made from a material suited to its environment. An acoustic element obtained using the manufacturing method, a sound absorption structure comprising at least one such acoustic element and an aircraft powerplant comprising at least one such structure are also described.
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公开(公告)号：US11187189B2
公开(公告)日：2021-11-30
申请号：US16695820
申请日：2019-11-26
Applicant: Airbus Operations (S.A.S.)
Inventor： Frédéric Journade , Pierre Charon , Laurent Cazeaux , Pascal Gougeon
Abstract: A propulsion system includes a bypass turbine engine and a pylon. The turbine engine includes an engine, two internal cowls, two outer cowls, a first lock for locking the internal cowls to the engine, cascades of vanes fixed to the outer cowl via hooping, wherein the outer cowls are movable in translation with respect to the engine, in which each outer cowl is able to slide parallel to a direction of translation on an internal cowl via a top guideway connection and a bottom guideway connection, and in which each outer cowl is mounted with the ability to slide parallel to the direction of translation on the pylon via an upper guideway connection. The propulsion system makes it possible during maintenance operations to move the outer cowl and the internal fixed structure towards the rear and therefore away from the front cowls to get at the engine.
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Patent Agency Ranking
6.发明申请公开(公告)号：US20200165975A1
公开(公告)日：2020-05-28
申请号：US16682271
申请日：2019-11-13
Applicant: Airbus Operations S.A.S.
Inventor： Wolfgang Brochard , Laurent Cazeaux , Claire Maffre
IPC: F02C7/24 , B64D29/00 , G10K11/168
Abstract: A method for manufacturing an acoustic element of a sound absorption structure including at least one cylindrical, conical or truncated conical chamber obtained from a flat preform shaped and then assembled in order to obtain the cylindrical, conical or truncated conical shape of the chamber. This manufacturing method makes it possible to obtain an acoustic element that has thin walls and is made from a material suited to its environment. An acoustic element obtained using the manufacturing method, a sound absorption structure comprising at least one such acoustic element and an aircraft powerplant comprising at least one such structure are also described.
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公开(公告)号：US11773806B2
公开(公告)日：2023-10-03
申请号：US17870255
申请日：2022-07-21
Applicant: Airbus Operations (S.A.S.)
Inventor： Thierry Gaches , Laurent Cazeaux
Abstract: An assembly includes a structure with 6 o'clock and 12 o'clock beams and front and rear curved beams, in which the 12 o'clock beam is mounted to be able to rotate on a pylon of an aircraft between a closed position and a raised position, a fan cowl fixed to the structure, a thrust reverser with a rear cowl and that is able to move in translation along the 6 o'clock and 12 o'clock beams between a forward position and a backward position, cascades fixed to the thrust reverser, and a mover for moving the thrust reverser. With such an arrangement, the fan cowl and the thrust reverser are fixed to the same structure, and it is this structure that is hinged to the pylon.
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8.发明申请公开(公告)号：US20210049993A1
公开(公告)日：2021-02-18
申请号：US16987949
申请日：2020-08-07
Applicant: Airbus Operations (S.A.S.)
Inventor： Laurent Cazeaux , Florent Mercat , Claire Maffre
IPC: G10K11/162 , B64D33/00
Abstract: A double-enclosure acoustic element of small size, in particular for an aircraft acoustic panel. The acoustic element has a first enclosure with a mouth and a second enclosure with, at a front longitudinal end, a mouth and arranged inside the first enclosure, these first and second enclosures being joined together at the front. The acoustic element includes a slotting assembly system, the assembly system including at least one protruding element on the first edge of one of the first and second enclosures and at least one recess in the first edge of the other of the first and second enclosures, the protruding element and the recess having complementary shapes such that the protruding element can be slotted into the recess. Thus, the two enclosures can be assembled by quick and easy slotting.
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公开(公告)号：US10900517B2
公开(公告)日：2021-01-26
申请号：US16654151
申请日：2019-10-16
Applicant: Airbus Operations S.A.S.
Inventor： Cédric Poupon , Laurent Cazeaux
Abstract: A slide includes a carriage, a guide, and interposed pads allowing the carriage to be moved in translation in a longitudinal direction by relative sliding of the pads on contact surfaces distributed symmetrically on both sides of two planes: a horizontal plane parallel to the longitudinal direction and the transverse direction and a median plane parallel to the longitudinal direction and the vertical direction. The contact surfaces are oriented so as to form with the horizontal plane an angle between 30° and 70° inclusive.
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公开(公告)号：US11499504B2
公开(公告)日：2022-11-15
申请号：US17064402
申请日：2020-10-06
Applicant: Airbus Operations (S.A.S.)
Inventor： Laurent Cazeaux
Abstract: A propulsion assembly for an aircraft includes a pylon, a turbofan including a structure fixed to the pylon, and at least one thrust reverser, each having a top beam extending parallel to a longitudinal direction and mobile in rotation on the structure around a rotation axis parallel to the longitudinal direction. For each thrust reverser, an actuator is provided, a first end of which is articulated on the pylon and a second end of which is articulated on the top beam of the thrust reverser and the articulation axis of the actuator on the top beam is not coaxial with the rotation axis. Such assembly allows a positioning of the actuator in the upper part of the turbofan between the top beam of the thrust reverser and the pylon to free some space.
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