Patent classifications
B64C1/1492
Plindow with opaque plug
A porthole, a porthole plug in a vehicle, and an aircraft with portholes are provided. The porthole includes an opaque plug with an aperture therethrough.
LIGHTWEIGHT AIRCRAFT WINDOW WITH LOW DRAG
An aircraft window composed of a monolithic interior pane made of polymer material and of a laminated exterior pane made of glass that are separated by an air-filled space, wherein the laminated exterior pane consists of two glass sheets bonded by an adhesive interlayer, and wherein the thickness of the exterior glass sheet is between 0.2 and 2.6 mm, and the thickness of the interior glass sheet is between 0.2 and 2.1 mm.
Unitary aircraft windshield with conical single curvature
A windshield for an aircraft cockpit is provided which includes a glazed windshield part which has a single curvature corresponding to a portion of the envelope of a cone extending between a lower plane and an upper plane which intersect an axis of the cone. The single curvature of the glazed part of the windshield enables the glazed part to be produced more easily, for example by rolling or by hydroforming. It also makes it possible to create configurations for a cockpit for two pilots, a single pilot or even no pilot, on the basis of a single aerodynamic shape of the fuselage of the aircraft by only adapting the structure of the windshield. Also provided are a windshield frame for such a windshield, a windshield assembly including such a windshield frame and such a windshield, and an aircraft equipped with such a windshield.
Window for an aircraft and display for aircraft window
A sidewall assembly for an aircraft and an aircraft are provided. In one example, the sidewall assembly includes a window. A sidewall portion has an inner-facing side and at least partially surrounds the window. A transparent display panel is coupled to the sidewall portion and covers the inner-facing side of the sidewall portion including the window. The transparent display panel includes a display screen configured to display information to a passenger. A display controller is in communication with the transparent display panel to communicate a video/audio signal providing the information to the display screen.
Window element with a non-concealing cover, aircraft region and aircraft with a window element
A window element for an aircraft comprises a window frame which has a frame reveal forming an opening, and a receptacle adjoining the frame reveal, an inner window pane which is configured to be inserted into the receptacle, a holding frame which is configured to be inserted into the receptacle and to fix the inner window pane in the receptacle, and a cover which has an opening and is configured to be attached to the window frame and to conceal the window frame around the frame reveal. An encircling inner edge of the cover that forms the opening of the cover lies radially substantially outside an encircling inner edge of the receptacle.
CANOPY SEPARATION SYSTEMS AND METHODS FOR AN AIRCRAFT
A canopy for an aircraft includes a pivot assembly including a first hinge and a second hinge opposite from the first hinge. The first hinge includes a first pivot slot having a first length. The first pivot slot is configured to retain a first aft pin of a fuselage of the aircraft. The second hinge includes a second pivot slot having a second length. The second pivot slot is configured to retain a second aft pin of the fuselage of the aircraft. The first length differs from the second length.
Window clamp system for a vehicle
A window clamp system and method are to secure a window pane to a window frame of a vehicle. The window clamp system includes a mounting bracket configured to be secured to the window frame, one or more ratchets coupled to the mounting bracket, and a spring clip configured to move in relation to the mounting bracket and the one or more ratchets. The spring clip is configured to engage a seal positioned around the window pane.
Quiet urban air delivery system
A public transportation system combines a unique combination of components that includes interoperable electric-powered vehicles, facilities, hardware and software having specifications, standards, processes, capabilities, nomenclature, and concepts of operations that together include a concerted, comprehensive, multi-modal, future system for moving people and goods that is herein named Quiet Urban Air Delivery (QUAD) and in which uniquely-capable, ultra-quiet, one to six-seat, electrically-powered, autonomous aircraft (SkyQarts) fly sub-193 kilometer trips on precise trajectories with negligible control latency and perform extremely short take-offs and landings (ESTOL) with curved traffic patterns at a highly-distributed network of very small, airports (“SkyNests”) that themselves have standardized compatible facilities that interoperate with SkyQarts as well as with versatile, autonomous electric-powered payload carts (EPCs) and robotic delivery carts (RDCs) to provide safe, fast, on-demand, community-acceptable, environmentally friendly, high-capacity, affordable door-to-door delivery of both passengers and cargo across urban, suburban and rural settings across the globe.
Window Frame For A Vehicle And Method Of Manufacturing A Window Frame
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.
Aircraft windowed structure
A windowed structure includes a body having a frame with an outer wall extending between a first end and a second end. An inner wall extends from the outer wall. The inner wall is connected to the outer wall at the first end to define a proximal joint of the body delimiting a window opening extending through the body. A window element covers the window opening and defines an outer window surface and an inner window surface. The window element has an overlap segment overlaying the outer wall and attached thereto. An unobstructed portion of the window element is defined between the overlap segment and is unobstructed by the frame between the proximal joint.