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公开(公告)号：WO2018027002A1
公开(公告)日：2018-02-08
申请号：PCT/US2017/045246
申请日：2017-08-03
Applicant: TEXTRON AVIATION INC.
Inventor： WILLFORD, Neal, Herbert , COTTRELL, Travis
Abstract: An aircraft where an engine creates mechanical energy. That energy is then converted into another transmittable form, e.g., electrical using a generator, or hydraulic using a pump, and is delivered to remotely-located motors and thrusters, e.g., propellers at one or more locations on the aircraft. The general concept makes the engine as well as the motors used scalable to accomplish overall efficiency objectives.
Abstract translation:
一台发动机产生机械能的飞机。 然后该能量被转换成另一种可传输的形式，例如使用发电机的电气或使用泵的液压，并且被传送到位于远处的电动机和推进器，例如在飞机上的一个或多个位置处的推进器。 一般的概念使得发动机和电机可以扩展使用，以实现整体效率目标。
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公开(公告)号：WO2018049384A1
公开(公告)日：2018-03-15
申请号：PCT/US2017/051132
申请日：2017-09-12
Applicant: TEXTRON AVIATION INC.
Inventor： KENDRICK, Phillip, Anthony , GINTERT, Lawrence, Arthur , SKIDMORE, Herbert, Lee , MCKOWN, Mike, Preston
Abstract: A system and process for bonding involves a pocket made into one article is used to secure that article to another using a flowable, curable material (e.g., resin) which during saturation enters through a passageway and at least partially fills the void. When the article is cured, the article is bonded to another article to which resin has also been applied since the void (now containing cured material) is larger than the passageway.
Abstract translation: 用于粘合的系统和方法包括制成一个物品的口袋用于使用可流动的可固化材料（例如树脂）将该制品固定到另一个制品上，所述可流动的可固化材料在饱和期间通过通道进入，并且至少 部分填补了空白。 当制品固化时，由于空隙（现在含有固化材料）比通道大，所以制品粘合到另一种树脂已经涂覆的制品上。
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公开(公告)号：WO2018027017A1
公开(公告)日：2018-02-08
申请号：PCT/US2017/045269
申请日：2017-08-03
Applicant: TEXTRON AVIATION INC.
Inventor： HUGHES, Mark, Alan , WILLFORD, Neal, Herbert
Abstract: A propulsion system for an aircraft includes an engine (e.g., piston engine, or turbine) having an axis made to be nonparallel with the longitudinal axis of the aircraft. This is enabled using an electrical, hydraulic, or other system to transfer energy generated by the engine (e.g., via electrical wiring, fluid conduits, etc.) to remotely power a motor used to drive a thrust-creating device (e.g., propeller or ducted fan). That the engine is able to be freely oriented allows for it being positioned without regard to any mechanical restraints existing in conventional arrangements.
Abstract translation: 用于飞机的推进系统包括具有与飞行器的纵向轴线不平行的轴线的发动机（例如活塞发动机或涡轮机）。 这通过使用电动，液压或其他系统来传递由发动机产生的能量（例如，通过电线，流体导管等）以远程驱动用于驱动推力产生装置的电动机（例如螺旋桨或 管风扇）。 发动机能够自由定向，因此可以在不考虑传统配置中存在的任何机械限制的情况下定位发动机。
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公开(公告)号：US20250151913A1
公开(公告)日：2025-05-15
申请号：US19021391
申请日：2025-01-15
Applicant: Textron Aviation, Inc.
Inventor： Blake David Raybern
IPC: A47C7/50
Abstract: Embodiments provides a cable tensioning system comprising a mounting plate assembly with a mounting plate and a retraction cam mounted to the mounting plate and configured to pivot about a primary axis, wherein the retraction cam comprises a cam body and a spur body having a cable sheave groove, wherein the mounting plate assembly is fixedly secured to a mounting fixture of a leg rest of a seat, and wherein the cable sheave groove is configured to receive a cable fixed to extension frame of the leg rest, the extension frame being movable relative to the mounting fixture.
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公开(公告)号：US20250151901A1
公开(公告)日：2025-05-15
申请号：US18508810
申请日：2023-11-14
Applicant: Textron Aviation, Inc.
Inventor： Gavin Thomas Smith , Jim Michael Dugan , William Dale George , James Arthur Knittel , Jonathan Swartz
IPC: A47B88/90 , A47B88/407
Abstract: In an embodiment a tray includes a base area having a top side, a bottom side, a rear end, peripheral sides and a front end, a plurality of flanges extending upward from the top side and arranged at the rear end and the peripheral sides, a pin, bolt or stud arranged at an outside of a flange arranged at the rear end or a hole arranged in the flange at the rear end configured to receive a pin, bolt or stud, a first plurality of restraining rings arranged at a first side flange at the first peripheral side and a second plurality of restraining rings arranged at a second side flange at the second peripheral side.
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Patent Agency Ranking
公开(公告)号：US20250145272A1
公开(公告)日：2025-05-08
申请号：US18932883
申请日：2024-10-31
Applicant: Textron Aviation Inc.
Inventor： Trenton Keil , Jeremy Greene , Robert Bair , Jeffrey Johannsmeyer
IPC: B64C1/18
Abstract: A configurable aircraft aisle flooring system which includes a flat floor configuration and a drop-down aisle configuration. The flat floor configuration provides floor panels positioned to span across a trough of an aircraft aisle to form a level surface between upper sections of an aircraft aisle. The drop-down aisle configuration provides floor panels positioned below the upper section of the aircraft aisle to have a drop-down step between the upper sections of the aircraft aisle.
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公开(公告)号：US20250145271A1
公开(公告)日：2025-05-08
申请号：US18934165
申请日：2024-10-31
Applicant: Textron Aviation Inc.
IPC: B64C1/14 , B64D27/33 , B64D27/355 , B64D27/357
Abstract: An aircraft having unobstructed cabin door access includes a hybrid power drive with a combustion engine connected to an electricity generating machine. Components of the hybrid power drive are positioned throughout the aircraft to provide a weight distribution having an aft bias. The aircraft further includes a forward swept wing and a cabin door positioned forward of the forward swept wing, such that access into a fuselage of the aircraft via the cabin door is unobstructed by the forward swept wing.
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公开(公告)号：US12280865B2
公开(公告)日：2025-04-22
申请号：US18452855
申请日：2023-08-21
Applicant: Textron Aviation Inc.
Inventor： Jonathan Lynn Headrick , Joshua Lawrence Bell
IPC: B64C1/14
Abstract: A window roller shade and dimming pane assembly includes a rigid frame having a first side member on a first side and a second side member on a second side opposite the first side. An outer pane and an inner pane are disposed within the rigid frame with a gap between the outer pane and the inner pane. A roller shade includes a motor for rolling and unrolling the roller shade. A first constant force spring and a second constant force spring are each configured to pull the roller shade downwardly through the gap while the motor is unrolling the roller shade. A dimming film is disposed on the inner pane for dimming light through the inner pane. A window interface is operatively coupled to the inner pane for receiving touch input for controlling the dimming film and the roller shade.
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公开(公告)号：USD1069434S1
公开(公告)日：2025-04-08
申请号：US29910693
申请日：2023-08-23
Applicant: Textron Aviation Inc.
Designer： Allan Dale Schrag , Torin Alexander De Joy , Lydia P. Pierce , Matthew William Reese , Adam Brickman , John Hladik
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公开(公告)号：US20250108923A1
公开(公告)日：2025-04-03
申请号：US18476467
申请日：2023-09-28
Applicant: Textron Aviation Inc.
Abstract: Additively manufactured aircraft vent structures are provided with a one-piece frame which includes a substantially planar face plate defining a longitudinally elongate vent opening and a series of fixed-position vanes unitarily joined to the planar face plate which extend latitudinally across the vent opening. Each of the vanes may be curvilinear and provided such that unidirectional venting is established or may be in a V-shaped configuration of vane pairs such that multidirectional venting is established. Alternatively or additionally, the vanes may have a widthwise dimension between leading and trailing edges thereof such that the trailing edges of each vane terminally extends at least to a latitudinal plane defined by a leading edge of an immediately adjacent one of the vanes.
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