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公开(公告)号：US20240293859A1
公开(公告)日：2024-09-05
申请号：US18594192
申请日：2024-03-04
Applicant: Textron Aviation Inc.
Inventor： Andrew Ricks , Joshua Workman , Bradley Randal Higgins , Royce Heick , Juan Manuel De La Rosa Valverde
Abstract: An exchangeable forming component is configured for removable mounting relative to an interface block of a modular forming tool, with the interface block of the modular forming tool configured for removable mounting relative to a support structure to form a sheet metal component. The exchangeable forming component includes a component structure which is constructed using additive manufacturing, wherein the exchangeable forming component presents a first surface which provides an exchangeable forming surface shaped to form the sheet metal component, and a second surface configured to removably engage the support structure.
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公开(公告)号：US20240253530A1
公开(公告)日：2024-08-01
申请号：US18633079
申请日：2024-04-11
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
Abstract: A swivel locking system for preventing swiveling of a seat frame includes a locking pin and a series of pulleys along with a housing attached to a swivel plate. The locking pin is located in the housing and is biased to be extended downwardly through an aperture in the swivel plate and retracted from the aperture via a cable. The seat frame is able to be swiveled when the locking pin is retracted from the aperture, thereby unlocking the seat frame from a bottom support.
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公开(公告)号：US12049992B2
公开(公告)日：2024-07-30
申请号：US18484625
申请日：2023-10-11
Applicant: Textron Aviation Inc.
Inventor： Edward Francis Funke , Rebecca Rae Groninga , Allan Dale Schrag
IPC: F21S43/14 , B64D9/00 , F21W111/027
CPC classification number: F21S43/14 , B64D9/00 , B64D2203/00 , F21W2111/027
Abstract: An entry step lighting system for a deployable aircraft stairway. The system includes steps that having integrated light sources that direct and provide illumination to the steps. Some light sources illuminate strip lenses which indicate proximity to the step edges. Light emitted by a second group of light sources is directed into an angled face established on a riser wall between each step. The light bounces off of each angled face to illuminate the step below.
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公开(公告)号：US20240239517A1
公开(公告)日：2024-07-18
申请号：US18413903
申请日：2024-01-16
Applicant: Textron Aviation Inc.
Inventor： Royce Heick , Aaron Paul Shirley , Clark Ray Miller , William Richardson , Jason Short
Abstract: An aircraft skin alignment system includes a support structure to support one or more aircraft skins, a puller tool, and a clamp tool; the puller tool having a base, the base supporting a holding mechanism to releasably engage with a first aircraft skin and a pulling mechanism to apply a pulling force to the first aircraft skin when the first aircraft skin is engaged with the holding mechanism; and the clamp tool having a body supporting an edge locator; the puller tool is to pull the first aircraft skin such that a first edge of the aircraft skin abuts the edge locator, the edge locator preventing the first edge from being pulled past the edge locator; and tool holes can be drilled into the first aircraft skin such that the tool holes are aligned based on an edge index due to a position of the edge locator.
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公开(公告)号：USD1031338S1
公开(公告)日：2024-06-18
申请号：US29811196
申请日：2021-10-12
Applicant: Textron Aviation Inc.
Designer： Nathan Earl Esau , Craig Louis Bothell , Jason Eric Francis , Matthew R. Harrell , Shelby Nicole Page
Abstract: FIG. 1 is a perspective view of the drip edge on galley work surface showing our new design;
FIG. 2 is a front view of the drip edge on galley work surface of FIG. 1;
FIG. 3 is a back view of the drip edge on galley work surface of FIG. 1;
FIG. 4 is a left view of the drip edge on galley work surface of FIG. 1;
FIG. 5 is a right view of the drip edge on galley work surface of FIG. 1;
FIG. 6 is a top view of the drip edge on galley work surface of FIG. 1;
FIG. 7 is a bottom view of the drip edge on galley work surface of FIG. 1;
FIG. 8 is a perspective view of the drip edge on galley work surface of FIG. 1 in a stowed configuration;
FIG. 9 is a front view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 10 is a left view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 11 is a right view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
FIG. 12 is a perspective view of the drip edge on galley work surface of FIG. 1 in a deployed configuration;
FIG. 13 is a front view of the drip edge on galley work surface of FIG. 1 in the deployed configuration;
FIG. 14 is a left view of the drip edge on galley work surface of FIG. 1 in the deployed configuration; and,
FIG. 15 is a right view of the drip edge on galley work surface of FIG. 1 in the deployed configuration.
In FIGS. 1-15, broken lines indicate environmental structure that forms no part of the claimed design.-
Patent Agency Ranking
公开(公告)号：US20240165441A1
公开(公告)日：2024-05-23
申请号：US18515904
申请日：2023-11-21
Applicant: Textron Aviation Inc.
Inventor： Tanner David Harpool
Abstract: A system for establishing an auxiliary electrical connection for an igniter configured to puncture a fire bottle. The system having an adapter configured to conceal an electrical connection of the igniter and electrically couple the concealed electrical connection to the auxiliary connection. The auxiliary connection preventing an improper connection being made to the igniter by having a different connection size than the electrical connections on the igniter.
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公开(公告)号：US20240154257A1
公开(公告)日：2024-05-09
申请号：US18502204
申请日：2023-11-06
Applicant: Textron Aviation Inc.
Inventor： Michael Louis Koonce
IPC: H01M50/516 , H01M10/0525 , H01M50/534 , H01M50/581
CPC classification number: H01M50/516 , H01M10/0525 , H01M50/534 , H01M50/581
Abstract: A battery system includes a first battery cell; a second battery cell positioned adjacent to the first battery cell; and a fusible link connecting the first battery cell to the second battery cell. The fusible link having a first tab connected to and extending from the first battery cell; a second tab connected to and extending from the second battery cell; and a connection connecting the first tab to the second tab; the connection is to release the first tab from the second tab upon being heated to a threshold temperature; and releasing the first tab from the second tab protects the first battery cell from thermal runaway conditions of the second cell.
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公开(公告)号：US20240132212A1
公开(公告)日：2024-04-25
申请号：US18483338
申请日：2023-10-08
Applicant: Textron Aviation Inc.
Abstract: An electric aircraft includes a forward wing and an aft wing both located on a top side of a fuselage and both having an upward dihedral angle. The forward wing has a straight or slightly forward-swept leading edge. The aft wing has a swept leading edge. A plurality of propeller engines are located on a leading-edge side of the forward wing. A single propeller engine may be located on a top side of an aft end of the fuselage; alternatively, a plurality of propeller engines are located on the aft wing on either its leading or trailing edge. The propeller engines are each powered by an electric motor. An unobstructed cargo door is located on a side of the fuselage, aft of the forward wing.
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公开(公告)号：US20240034470A1
公开(公告)日：2024-02-01
申请号：US18360900
申请日：2023-07-28
Applicant: Textron Aviation Inc.
Inventor： Brandon Lynn Parks , David Grant Pulen , Jason Roger Purdy , Edward Moradians
IPC: B64D9/00
CPC classification number: B64D9/003
Abstract: A doorway side guide system includes a base mechanically coupled with a bottom portion of a doorway. A mounting member is rotatably coupled to the base via a hinge for rotating between a deployed position and a stowed position. A contact member is mechanically coupled with the mounting member via a pivot such that the contact member is configured to rotate about the pivot. The contact member extends outside of the doorway in the deployed position for guiding cargo through the doorway and for protecting a doorframe of the doorway.
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公开(公告)号：US20240034454A1
公开(公告)日：2024-02-01
申请号：US18362774
申请日：2023-07-31
Applicant: Textron Aviation Inc.
Inventor： Joseph Allan Smarsh , Evan Michael Johnson , Timothy Bachman , Richard S. Conkling
IPC: B64C1/14
CPC classification number: B64C1/1407
Abstract: A system and method for unlatching an aircraft door is disclosed. The system includes a latch pin design which enables retraction of the pin in the event the ordinary unlatching mechanical systems fail. The system includes the use of a rod that is reversely threaded on each side. Rotation of the rod either extends or retracts the pin.
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