-
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.
-
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.
-
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.
-
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.
-
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.
-
Patent Agency Ranking
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
-
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.
-
公开(公告)号：US20250108909A1
公开(公告)日：2025-04-03
申请号：US18477984
申请日：2023-09-29
Applicant: Textron Aviation Inc.
Inventor： Kelly Ray Laflin , Robert Glynn Wiegers
Abstract: A low drag nacelle and pylon fairing for an aircraft includes a fairing configured to provide a low drag connection between a pylon and a nacelle. The fairing includes an aft-facing face formed between the nacelle and a trailing edge of the pylon with the aft-facing face being configured with a vent for exhausting air in the same direction as engine jet exhaust flow. The fairing includes aerodynamically formed curves providing a larger aft-facing face compared with traditional fairing arrangements. A substantial improvement in drag reduction is achieved by venting air into the space immediately beyond the aft-facing face.
-
公开(公告)号：US20250095413A1
公开(公告)日：2025-03-20
申请号：US18783378
申请日：2024-07-24
Applicant: Textron Aviation Inc.
Inventor： Adam Blake Wolfe , Haines Todd , Mark Christopher Hansen
Abstract: Techniques are disclosed for data collection in connection with one or more aircraft. Avionics inputs are received, at an avionics data collection platform, regarding a plurality of avionics parameters. The avionics parameters may be associated with components of the aircraft and collected by way of avionics sensors. The avionics parameters are aggregated by way of the data collection platform. The aggregated avionics parameters are multiplexed at the data collection platform. The multiplexed and aggregated plurality of avionics parameters are transmitted over loosely-coupled networking connections to an aircraft recording system. The aircraft recording system includes a network collector and an embedded microcontroller system. A prioritized aggregation of the avionics parameters is provided by way of the network collector and the embedded microcontroller system to external systems.
-
公开(公告)号：US12234004B1
公开(公告)日：2025-02-25
申请号：US18488740
申请日：2023-10-17
Applicant: Textron Aviation Inc.
Inventor： Rebecca Rae Groninga , Clayton Auther Richards , Zonmong Alexander Lor , Merril Binford Williams , Sergio Ricardo Martinez
Abstract: An aircraft door handle and lighting system for an entryway on an aircraft. The system includes a face plate with recessed areas. One recessed area includes a handle positioned for a user to grasp when entering or exiting the aircraft, and another recessed area includes a light source configured to direct light towards one or more stairs. Another recessed area is configured on the opposite side of the entryway and includes a light source configured to direct light towards the stairs.
-
-
-
-
-
-
-
-
-
Search Results
303
records
(took 0.022 seconds)
