公开(公告)号：US20240343379A1

公开(公告)日：2024-10-17

申请号：US18634336

申请日：2024-04-12

Applicant: Jet Shades, LLC

Inventor： Kevin Duggan

IPC: B64C1/14

CPC classification number: B64C1/1492

Abstract: A removable tinted window panel system for an aircraft cockpit may include unique tinted panels and panel brackets which are easily installed and removed allowing full compliance with FAA regulations. The tinted panels, when installed, block 99.9% of UV radiation, reduce glare by up to 70%, reduce heat from solar energy up to 47% and thereby improve overall cockpit environment and pilot comfort. The panels allow the pilot to selectively block the sun when needed to remove glare and to remove the discomfort of being exposed to direct sunlight coming from the side windows. The panels reduce pilot fatigue, reduce eye strain and increase pilot performance and comfort and most of all improve flying safety.

公开(公告)号：US20240228010A9

公开(公告)日：2024-07-11

申请号：US17768715

申请日：2020-10-12

Applicant: SAINT-GOBAIN GLASS FRANCE

Inventor： Jean-Benoît MAYEUX ,  Flavien FREMY

IPC: B64C1/14

CPC classification number: B64C1/1492

Abstract: A monolithic or laminated glazing is bolted or pinched by a frame which is itself bolted onto or through a structure, wherein, in at least part of the periphery of the glazing of maximum flexibility or of minimum stiffness with respect to the buckling phenomenon, the bolting is performed by at least one bolt inserted into a bush concentric to the bolt, or replaced by the insertion of a bush or of a pin, each bush or each pin being mounted without play on the glazing or on the frame, and on or through the structure.

公开(公告)号：US20240217647A1

公开(公告)日：2024-07-04

申请号：US18557689

申请日：2022-04-29

Applicant: SAINT-GOBAIN GLASS FRANCE

Inventor： Gary JACQUS ,  Volodymyr IURASOV ,  Sylvain BERGER

IPC: B64C1/14 ,  G10K11/162

CPC classification number: B64C1/1492 ,  G10K11/162

Abstract: A glazed unit extending along a main surface and formed by a first material, includes a soundproofing zone that extends along a first length l along the main surface, the soundproofing zone having a first thickness h1 of the material, the first thickness h1 varying, as a function of a coordinate x, along the first length l in proportion to a value of xn, where n is a real number strictly greater than 1, from a minimum thickness h1min to a maximum thickness h1max, the first length l being predetermined such that the minimum thickness h1min is less than or equal to one third of the maximum thickness h1max.

公开(公告)号：US20240166327A1

公开(公告)日：2024-05-23

申请号：US18550858

申请日：2022-02-11

Applicant: SAINT-GOBAIN GLASS FRANCE

Inventor： Jean-Charles SAUVESTY ,  Ludovic CHAUVETTE

IPC: B64C1/14

CPC classification number: B64C1/1492 ,  B64C1/1484

Abstract: A multiple glazed unit includes a first pane and a second pane separated by an air gap, a mounting gasket covering a peripheral strip of the main surface of the first pane facing the second pane, the mounting gasket covering the edges of the first pane and of the second pane and occupying a peripheral portion of the air gap, a reinforcing and sealing element being incorporated in the mounting gasket by covering a peripheral portion of the main surface of the first pane facing the second pane and by engaging the edge of the second pane so as to limit the bending effect of the first pane.

公开(公告)号：US11827334B2

公开(公告)日：2023-11-28

申请号：US17489954

申请日：2021-09-30

Applicant: Premium Aerotec GmbH

Inventor： Pasquale Mauro

IPC: B64C1/14

CPC classification number: B64C1/1492

Abstract: A vehicle window frame includes a stiffening frame component and an inner retaining frame component adapted to be coupled to the stiffening frame component for receiving at least a portion of a window. The stiffening frame component includes a profile having a support portion and an inner flange extending perpendicularly thereto and forming an inner edge of the stiffening frame component. The support portion forms a support surface extending radially outwardly from the inner edge for support against an edge surface of a window opening. The inner retaining frame component includes a profile having a coupling portion adapted to be fitted onto the inner flange and a connecting portion. forming an edge surface of the retaining frame component for overlapping the edge surface and having at a radially inner boundary thereof a projection facing away from the coupling portion and the support portion for wrapping around the window opening.

公开(公告)号：US10077101B2

公开(公告)日：2018-09-18

申请号：US14076239

申请日：2013-11-10

Applicant: Airbus Operations GmbH

Inventor： Kenneth Boenning

IPC: B64C1/14 ,  B64C1/06

CPC classification number: B64C1/1484 ,  B64C1/066 ,  B64C1/1492 ,  Y02T50/46 ,  Y10T29/49826

Abstract: An aircraft window arrangement comprising a sidewall lining panel which is provided with a window opening, an inner window attached to the sidewall lining panel and extending across the window opening formed in the sidewall lining panel and an outer window arranged at a distance from the inner window and extending across a window opening formed in an aircraft outer skin. The aircraft window arrangement further comprises a window funnel including an inner rim facing the inner window and extending along a circumference of the window opening formed in the sidewall lining panel, and an outer rim facing the outer window and extending along a circumference of the window opening formed in the aircraft outer skin. The window funnel is formed separate from the sidewall lining panel. The window funnel may be attached to a retainer for retaining the outer window.

公开(公告)号：US20180200929A1

公开(公告)日：2018-07-19

申请号：US15918476

申请日：2018-03-12

Applicant: 4M Company

Inventor： Stephen B. Smolinske ,  Rodger Clement ,  Jim Sears ,  Vern Meyers

IPC: B29C45/00 ,  B29C45/72 ,  F16J15/02 ,  B64C1/14 ,  B29B11/16 ,  B29K83/00 ,  B29K105/16 ,  B29K509/08 ,  B29L31/26

CPC classification number: B29C45/0001 ,  B29B11/16 ,  B29C45/72 ,  B29K2083/00 ,  B29K2105/16 ,  B29K2509/08 ,  B29K2995/0046 ,  B29L2031/26 ,  B64C1/14 ,  B64C1/1492 ,  F16J15/025

Abstract: Disclosed herein is a novel approach to producing a lightweight component. The lightweight component is produced of a much lighter material than has been used before, produced by a process of mixing a compound containing uncured silicone and a volume of microspheres, and then dispensing this material into a mold. Such a mold may be a female mold having the negative three dimensional shape of the lightweight component to be produced. The lightweight component may then be pressurized and/or heated during the curing process either prior to removing the lightweight component from the mold or after removing the lightweight component from the mold.

公开(公告)号：US20180178895A1

公开(公告)日：2018-06-28

申请号：US15896551

申请日：2018-02-14

Applicant: BOMBARDIER INC.

Inventor： Alexandre Desroches ,  David Lencz ,  Franck Dervault

IPC: B64C1/14 ,  E06B7/16 ,  E06B3/66 ,  B60J1/00

CPC classification number: B64C1/1484 ,  B32B17/10055 ,  B32B17/10165 ,  B60J1/007 ,  B64C1/1492 ,  E06B3/66 ,  E06B7/16 ,  Y10T29/49764 ,  Y10T428/24628

Abstract: An aircraft includes a fuselage defining a mold line, at least one frame disposed in the fuselage, at least one transparent pane suspended within the frame. The transparent pane is a deformable material that defines a first surface position h1 when not subjected to a differential pressure ΔP thereacross and a second surface position h2 when subject to the differential pressure ΔP thereacross. The first and second surface positions are defined with reference to the outside mold line. The first surface position h1 defines a reverse curvature. In response to the differential pressure ΔP, the second surface position h2 includes bulging of the transparent pane by a predetermined distance Δh. The frame is constructed to be positioned within the aircraft such that the transparent pane presents a surface, when subjected to the pressure differential ΔP, that is substantially consistent with the outside mold line of the vehicle.

公开(公告)号：US09994300B2

公开(公告)日：2018-06-12

申请号：US15410993

申请日：2017-01-20

Applicant: Bell Helicopter Textron Inc.

Inventor： William Sumner ,  Tim Reed ,  Christopher Marvin Rowe ,  Lawrence Duane Lee ,  Glen Rivers ,  Robert Harmon ,  Jeremy Robert Schadler ,  William Lewis Neal, II

IPC: B64D45/00 ,  B64C1/14

CPC classification number: B64C1/1492 ,  B64D45/00

Abstract: This description relates to a strapped windshield assembly for a rotorcraft. In some implementations, the rotorcraft includes an airframe, a windshield, and a plurality of independent straps connected to the airframe and the windshield, the straps operative to move independently with respect to one another. The independent movement of the straps allow relative movement of portions of the windshield in response to a strike. In some implementations, the straps are spaced every 4-6 inches along an edge of the windshield. In some implementations, the straps are over an edge of the windshield. The straps can have a modulus of elasticity of 8-12 millions of pounds per square inch (MSI). The windshield can include polycarbonate material.

公开(公告)号：US09976726B2

公开(公告)日：2018-05-22

申请号：US14729555

申请日：2015-06-03

Applicant: Gentex Corporation

Inventor： Kevin L. Ash ,  Steven J. Veenman

IPC: F21V14/08 ,  B64D47/02 ,  F21V11/00 ,  B64C1/14

CPC classification number: F21V14/08 ,  B64C1/1492 ,  B64D47/02 ,  F21V11/00

Abstract: A window assembly includes a pressure pane and a bezel proximate a periphery of the pressure pane and defining an inner opening. The bezel includes an inner wall with a channel. An electro-optic element is disposed in the inner opening and is received in the channel of the inner wall. The electro-optic element operates between a transmissive condition and a dimmed condition. A surface of the electro-optic element exhibits a first level of spectral reflectivity at least when in the dimmed condition. The assembly further includes a dust cover assembly proximate the bezel. The dust cover assembly including a light transmitting sheet and a plurality of light sources disposed at edges of the light transmitting sheet and to emit light into the light transmitting sheet to illuminate the light transmitting sheet with a diffuse light.