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公开(公告)号：USD1044652S1
公开(公告)日：2024-10-01
申请号：US29871646
申请日：2023-02-24
Applicant: Textron Aviation Inc.
Abstract: FIG. 1 is a perspective view of an aircraft vanity display screen showing our new design in an aircraft lavatory;
FIG. 2 is another perspective view showing the aircraft vanity display screen of FIG. 1;
FIG. 3 is a side view showing the aircraft vanity display screen of FIG. 1;
FIG. 4 is another side view showing the aircraft vanity display screen of FIG. 1; and,
FIG. 5 is front view showing the aircraft vanity display screen of FIG. 1.
In FIGS. 1-5, broken lines indicate environmental structure that forms no part of the claimed design.-
公开(公告)号：USD1034403S1
公开(公告)日：2024-07-09
申请号：US29811218
申请日：2021-10-12
Applicant: Textron Aviation Inc.
Designer： Torin Alexander De Joy , Jonathan Lynn Headrick , Joshua Phillip DeDonder , Matthew R. Harrell
Abstract: FIG. 1 is a perspective view of the set of window reveals showing our new design;
FIG. 2 is a front view of the set of window reveals of FIG. 1;
FIG. 3 is a left view of the set of window reveals of FIG. 1;
FIG. 4 is a right view of the set of window reveals of FIG. 1;
FIG. 5 is a top view of the set of window reveals of FIG. 1; and,
FIG. 6 is a close-up perspective view of one window reveal of the set of window reveals of FIG. 1.
The evenly spaced broken lines in FIGS. 1-6 depict environmental structure that form no part of the claimed design. The dash-dot-dash lines surrounding the detail views in FIGS. 1 and 6 are for the purpose of annotating the detail views only and form no part thereof. The dash-dot-dot-dash lines in FIGS. 1, 2, 5, and 6 illustrate boundaries of the claimed portions of the design and form no part thereof.
The set of window reveals is shown with a symbolic break in its length. The appearance of any portion of the article after the break lines, as well as the break lines themselves, form no part of the claimed design.-
公开(公告)号：US11912414B2
公开(公告)日：2024-02-27
申请号：US17736712
申请日：2022-05-04
Applicant: Textron Aviation Inc.
Inventor： Frank Joseph Rowe , Merril Binford Williams , Jonathan Lynn Headrick , Michael John Seibel
IPC: B64D11/06
CPC classification number: B64D11/0644
Abstract: A cockpit center console armrest includes a base member configured for mounting to a floor, an extending member mechanically coupled to the base member, and an armrest mechanically coupled to the extending member. The extending member includes an inner telescoping member configured for sliding within an outer telescoping member for adjusting a height of the armrest. A lever exposed on an underside of the armrest is configured for actuating a release mechanism. The release mechanism is configured for releasably securing the inner telescoping member to the outer telescoping member. A pivot axis pivotably couples the extending member to the base member such that the extending member is rotatable for rotating the armrest between a deployed orientation and a retracted orientation.
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Patent Agency Ranking
公开(公告)号：US20240059392A1
公开(公告)日：2024-02-22
申请号：US18452855
申请日：2023-08-21
Applicant: Textron Aviation Inc.
Inventor： Jonathan Lynn Headrick , Joshua Lawrence Bell
IPC: B64C1/14
CPC classification number: B64C1/1492
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：US20230159170A1
公开(公告)日：2023-05-25
申请号：US18056892
申请日：2022-11-18
Applicant: Textron Aviation Inc.
Inventor： Nathan Earl Esau , Jonathan Lynn Headrick
CPC classification number: B64D11/003 , B64F5/10
Abstract: An overhead bin in an aircraft includes a liner disposed on an underside of a cabin ceiling and a receptacle that protrudes through an opening in the liner. A bin has a top side with at least one attachment point that includes: a stud mechanically coupled to the top side and a screw disposed within the stud. The stud includes a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner. An installation method for an overhead bin in an aircraft includes raising the overhead bin to engage the stud with the receptacle, sliding the overhead bin outboard for inserting the stud into the receptacle, and turning a screw within the stud for tightening the stud within the receptacle for securing the overhead bin beneath the ceiling.
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公开(公告)号：US20250066009A1
公开(公告)日：2025-02-27
申请号：US18811442
申请日：2024-08-21
Applicant: Textron Aviation Inc.
Inventor： Michael Scott Robinson , Jonathan Lynn Headrick
Abstract: An aircraft windscreen comprises a plurality of liquid crystal display (LCD) films positioned on or within various portions of the windscreen to define a corresponding plurality of zones. The opacity of the LCD films are individually and separately controllable by control circuitry in communication with user controls to allow a user to darken or lighten portions of the various LCD films to achieve a desired level of gradient tint in the defined zones to block external light, such as sunlight, from the aircraft.
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公开(公告)号：USD1034402S1
公开(公告)日：2024-07-09
申请号：US29811204
申请日：2021-10-12
Applicant: Textron Aviation Inc.
Designer： Torin Alexander De Joy , Matthew R. Harrell , Jonathan Lynn Headrick , Joshua Phillip DeDonder
Abstract: FIG. 1 is a perspective view of the passenger service unit showing our new design;
FIG. 2 is a front view of the passenger service unit of FIG. 1;
FIG. 3 is a right view of the passenger service unit of FIG. 1;
FIG. 4 is a left view of the passenger service unit of FIG. 1;
FIG. 5 is a bottom view of the passenger service unit of FIG. 1;
FIG. 6 is a close-up perspective view of the passenger service unit of FIG. 1;
FIG. 7 is a close-up front view of the passenger service unit of FIG. 1; and,
FIG. 8 is a close-up bottom view of the passenger service unit of FIG. 1.
The evenly-spaced broken lines in FIGS. 1-6 depict environmental structure that forms no part of the claimed design. The additional evenly-spaced broken lines in FIGS. 5 and 8 showing internal elements depict portions of the passenger service unit that form no part of the claimed design. The dash-dot-dash broken lines in FIGS. 1-2 and 5-8 are for the purpose of annotating the close-up views and form no part of the claimed design. The passenger service unit is shown with a symbolic break in its length. The appearance of any portion of the article after the break lines, as well as the break lines themselves, form no part of the claimed design.-
公开(公告)号：US20220363396A1
公开(公告)日：2022-11-17
申请号：US17736712
申请日：2022-05-04
Applicant: Textron Aviation Inc.
Inventor： Frank Joseph Rowe , Merril Binford Williams , Jonathan Lynn Headrick , Michael John Seibel
IPC: B64D11/06
Abstract: A cockpit center console armrest includes a base member configured for mounting to a floor, an extending member mechanically coupled to the base member, and an armrest mechanically coupled to the extending member. The extending member includes an inner telescoping member configured for sliding within an outer telescoping member for adjusting a height of the armrest. A lever exposed on an underside of the armrest is configured for actuating a release mechanism. The release mechanism is configured for releasably securing the inner telescoping member to the outer telescoping member. A pivot axis pivotably couples the extending member to the base member such that the extending member is rotatable for rotating the armrest between a deployed orientation and a retracted orientation.
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