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公开(公告)号：US20190233081A1
公开(公告)日：2019-08-01
申请号：US16312336
申请日：2017-06-27
申请人： BOMBARDIER INC.
摘要： Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap (28) along an elongated track member (36C) as the trailing edge flap (28) moves toward the deployed position; guiding a forward portion of the trailing edge flap (28) along the elongated track member (36C) as the trailing edge flap (28) moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap (28) relative to the elongated track member (36C).
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公开(公告)号：US20190233085A1
公开(公告)日：2019-08-01
申请号：US16311356
申请日：2017-06-27
申请人： BOMBARDIER INC.
发明人： Iyad AKEL , Dmitry BUDNITSKY , Howard Ian SMITH , Thomas HANSON
摘要： Systems and methods for deploying adjacent trailing edge flaps that are part of different flap assemblies of different stiffnesses are disclosed. An exemplary method comprises: deploying a first flap of a first flap assembly having a first stiffness by a first deployment amount and deploying a second flap adjacent the first flap by a second deployment amount where the deployment amount of the first flap part of the flap assembly of lower stiffness is greater than the second deployment amount of the second flap part of the flap assembly of higher stiffness. The difference in deployment amounts may be adapted to improve continuity between the first flap and the second flap when the first and second flaps are deployed and subjected to an aerodynamic load.
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公开(公告)号：US20240228016A1
公开(公告)日：2024-07-11
申请号：US18615260
申请日：2024-03-25
申请人： BOMBARDIER INC.
摘要： Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.
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公开(公告)号：US20220242553A1
公开(公告)日：2022-08-04
申请号：US17681061
申请日：2022-02-25
申请人： BOMBARDIER INC.
摘要： Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.
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公开(公告)号：US20230128350A1
公开(公告)日：2023-04-27
申请号：US18085980
申请日：2022-12-21
申请人： BOMBARDIER INC.
发明人： Iyad AKEL , Dmitry BUDNITSKY , Howard Ian SMITH , Thomas HANSON
摘要： Systems and methods for deploying adjacent trailing edge flaps that are part of different flap assemblies of different stiffnesses are disclosed. An exemplary method comprises: deploying a first flap of a first flap assembly having a first stiffness by a first deployment amount and deploying a second flap adjacent the first flap by a second deployment amount where the deployment amount of the first flap part of the flap assembly of lower stiffness is greater than the second deployment amount of the second flap part of the flap assembly of higher stiffness. The difference in deployment amounts may be adapted to improve continuity between the first flap and the second flap when the first and second flaps are deployed and subjected to an aerodynamic load.
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公开(公告)号：US20210237855A1
公开(公告)日：2021-08-05
申请号：US17236097
申请日：2021-04-21
申请人： BOMBARDIER INC.
发明人： Iyad AKEL , Dmitry BUDNITSKY , Howard Ian SMITH , Thomas HANSON
摘要： Systems and methods for deploying adjacent trailing edge flaps that are part of different flap assemblies of different stiffnesses are disclosed. An exemplary method comprises: deploying a first flap of a first flap assembly having a first stiffness by a first deployment amount and deploying a second flap adjacent the first flap by a second deployment amount where the deployment amount of the first flap part of the flap assembly of lower stiffness is greater than the second deployment amount of the second flap part of the flap assembly of higher stiffness. The difference in deployment amounts may be adapted to improve continuity between the first flap and the second flap when the first and second flaps are deployed and subjected to an aerodynamic load.
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