Abstract: An oblique wing aircraft designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment and an aft swept wing segment. A center oblique airfoil section connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. Preferably, the aircraft is an all-wing aircraft.

Abstract: Disclosed is a system for thermally distributing hot air generated in a vehicle headlamp. A channel is defined between different chambers in the headlamp to allow for air circulation, thus reducing hot spots inside the housing around light sources which might compromise internal structures or devices.

Abstract: A vehicle door hinge that includes a door bracket mountable to a vehicle door, a body bracket mountable to a vehicle body, a pivot bushing having a cylindrical bearing that is disposed within a pivot axis hole of the body bracket, and a pivot pin that rotatably couples the door bracket and the body bracket together. The pivot pin includes a first shoulder disposed within the cylindrical bearing; and the pivot pin includes a second shoulder extending from the first shoulder. The second shoulder has a knurled cylindrical surface that is disposed within a pivot axis hole of the door bracket.

Abstract: The present application discloses various embodiments of a heat sink for semiconductor devices and methods for using and constructing the same. According to at least one aspect of the present disclosure, a heat sink for cooling a semiconductor device includes a base plate including a first side and a second side; a leg extending from the second side of the base plate, the leg including a distal end opposite the base plate and opposing walls extending between the base plate and the distal end; a leg plate disposed adjacent the distal end of the leg; a plurality of fins disposed between the distal end of the leg and the leg plate; and a plurality of micro-channels defined by the distal end of the leg, the plurality of fins, and the leg plate.

Abstract: Lit image projection lamp and method. In an exemplary embodiment of a projection device of the present disclosure, the projection device comprises a light source; a first lens positioned at a first distance from the light source; and a second lens at a second distance from the first lens; wherein the first lens and the second lens are lenticular lenses, each having an optical axis; and wherein the projection device is configured to generate a three-dimensional image from light emitted from the light source that passes through the first lens and the second lens.

Abstract: A method of manufacturing a tubular member for an automotive application that includes providing a flat workpiece of a material; forming at least one lance in the flat workpiece; roll-forming the flat workpiece into a tubular configuration; induction welding a seam of the tubular workpiece after the roll-forming; and trimming the tubular workpiece through the lance after welding the seam.

Abstract: Lamp assembly with thermal transporter. The present disclosure includes disclosure of a lamp assembly, comprising a housing; a cover attached to the housing defining a volume; a light source disposed within the volume; and a thermal transporter in thermal communication with the light source; wherein the thermal transporter comprises a plurality of graphite sheets structured to transfer heat generated by the light source away from the light source.

Abstract: Active grille shutter. In an embodiment of a shutter system of the present disclosure, the shutter system comprises a plurality of moveable louvers, at least one lifter, the lifter including a lifter arm having a plurality of platforms and a plurality of spurs extending therefrom, a plurality of tensioners, and a drive mechanism connected to the lifter arm and structured to reversibly move the lifter arm and the plurality of platforms extending therefrom, wherein the movement of the lifter arm and platforms causes each louver to rotate about a pin extending therefrom, the pin adjacent and offset from the post.

Abstract: A vehicle bumper assembly is provided having an energy absorber, a bracket, a step pad and a bumper fascia. The energy absorber includes an upper horizontal surface wherein the upper horizontal surface may define a deformable structure. The deformable structure may be in the form of flexible fins. The bracket may be mounted to the vehicle frame on a first end of the bracket and the energy absorber affixed to a second end of the bracket. The step pad may be affixed to the energy absorber. The bumper fascia may be affixed to either or both the step pad and the energy absorber.

Abstract: The present application discloses a light pipe assembly having a light pipe with a proximal end, an opposing distal end, a length between the proximal end and the distal end, and a surface, the surface having an emitting portion and an overlay portion, where the light pipe is a material capable of transmitting light with a first refractive index; and a reflective secondary surface having a second refractive index and a width, the reflective secondary surface positioned adjacent the overlay portion of the light pipe, where the first refractive index is greater than the refractive index of air, and the second refractive index is greater than the first refractive index. In at least one embodiment, the reflective secondary surface is a non-metallic material capable of reflecting light. In at least one embodiment, the width of the reflective secondary surface varies along the length of the light pipe.

Abstract: Lit image projection lamp and assemblies and methods to use the same to generate three-dimensional images. In an exemplary embodiment of a projection device of the present disclosure, the projection device comprises a light source and a curved lens positioned at a first distance from the light source, wherein the curved lens is a lenticular lens, having a concave portion and a convex portion, and wherein the projection device is configured to generate a homogenous light bar image from light emitted from the light source that passes through the curved lens.

Abstract: A vehicle bumper assembly is provided having an energy absorber, a bracket, a step pad and a bumper fascia. The energy absorber includes an upper horizontal surface wherein the upper horizontal surface may define a deformable structure. The deformable structure may be in the form of flexible fins. The bracket may be mounted to the vehicle frame on a first end of the bracket and the energy absorber affixed to a second end of the bracket. The step pad may be affixed to the energy absorber. The bumper fascia may be affixed to either or both the step pad and the energy absorber.

Abstract: The disclosure of the present application includes a light pipe assembly having a light pipe with a proximal end, an opposing distal end, a length between the proximal end and the distal end, and a surface, the surface having an emitting portion and an overlay portion, where the light pipe is a material capable of transmitting light with a first refractive index; and a reflective secondary surface having a second refractive index and a width, the reflective secondary surface positioned adjacent the overlay portion of the light pipe, where the first refractive index is greater than the refractive index of air, and the second refractive index is greater than the first refractive index. In at least one embodiment, the reflective secondary surface is a non-metallic material capable of reflecting light. In at least one embodiment, the width of the reflective secondary surface varies along the length of the light pipe.

Abstract: Active grille shutter. In an embodiment of a shutter system of the present disclosure, the shutter system comprises a plurality of moveable louvers, at least one lifter, the lifter including a lifter arm having a plurality of platforms and a plurality of spurs extending therefrom, a plurality of tensioners, and a drive mechanism connected to the lifter arm and structured to reversibly move the lifter arm and the plurality of platforms extending therefrom, wherein the movement of the lifter arm and platforms causes each louver to rotate about a pin extending therefrom, the pin adjacent and offset from the post.

Abstract: An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).

Abstract: An oblique wing aircraft designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment and an aft swept wing segment. A center oblique airfoil section connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. Preferably, the aircraft is an all-wing aircraft.

Abstract: The disclosure of the present application includes a light pipe assembly having a light pipe with a proximal end, an opposing distal end, a length between the proximal end and the distal end, and a surface, the surface having an emitting portion and an overlay portion, where the light pipe is a material capable of transmitting light with a first refractive index; and a reflective secondary surface having a second refractive index and a width, the reflective secondary surface positioned adjacent the overlay portion of the light pipe, where the first refractive index is greater than the refractive index of air, and the second refractive index is greater than the first refractive index. In at least one embodiment, the reflective secondary surface is a non-metallic material capable of reflecting light. In at least one embodiment, the width of the reflective secondary surface varies along the length of the light pipe.

Abstract: An oblique wing aircraft designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment and an aft swept wing segment. A center oblique airfoil section connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. Preferably, the aircraft is an all-wing aircraft.

Abstract: An oblique wing aircraft (1) designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment (27) on one side of the wing and an aft swept wing segment (29) on the opposite side of the wing. A center oblique airfoil section (25) connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. The center oblique airfoil section is not shaped solely to function as a circular fairing to fill the gap between an oblique wing and a fuselage at different oblique wing angles, nor is it a second wing in an X wing configuration. Preferably, the aircraft is an all-wing aircraft.

Abstract: A vehicle bumper assembly includes a polymeric support structure and a metal cover. The polymeric support structure may be one piece or a multi-piece component. The polymeric support structure includes a plurality of ribs formed on a substantially vertical wall. The chrome-plated metal cover is disposed on the one-piece polymeric support structure.