1598 results about "Cowling" patented technology

An air purifier for removing particles from air and providing an aesthetically pleasing appearance includes a housing having an air inlet, an air outlet and an airflow path therethrough. An air filter is mounted within the housing in the airflow path and a motor is mounted within the housing. The motor includes a motor shaft and a fan is mounted to the motor shaft for urging air into the air inlet, through the airflow path and out of the air outlet. An air cowl is removably mounted to the housing. The air cowl includes a peripheral edge. The air inlet or the air outlet is defined between the peripheral edge and the housing. A method of operating the air purifier with the inlet or outlet formed between the peripheral edge and the housing is also disclosed.

A combination of vehicle fairing structures forming a fairing system having a front end structure, a rear end structure, and first and second side structures, for optimizing the aerodynamic profile of vehicles, especially tractor-trailer combinations.

A gas turbine engine comprising a fan section, a compressor, a combustor and a turbine, includes a nacelle having an inner nacelle surface defining an inlet duct designed to reduce an inlet duct area of the inlet duct to increase acoustic attenuation. The gas turbine engine also includes a spinner, disposed forward of the fan section, that includes features to increase acoustic attenuation. In one embodiment of the present invention, the nacelle includes a nacelle contoured surface protruding radially inward from the inner nacelle surface to reduce the inlet duct area. In a further embodiment of the present invention, the spinner includes a spinner contoured surface for reducing the inlet duct area. In other embodiments, the nacelle and/or the spinner include an inflatable bladder, a SMA actuator, a fluidic actuator, or a combination thereof, selectively activated to increase acoustic attenuation during certain conditions of an aircraft.

A turbine exhaust casing having an outer casing, an inner casing, an annular exhaust gas path defined between outer and inner flow path walls, and a turbine exhaust casing cavity located radially outward and radially inward from the gas path. A plurality of structural struts support the inner casing to the outer casing, and a fairing surrounds each of the struts in an area extending between the outer and inner flow path walls. A first purge air path extends through at least one of the struts for conducting purge cooling air radially inward to the inner casing, and a second purge air path extends through the strut for further conducting the purge cooling air radially outward to provide a flow of purge air to a location of the exhaust casing cavity radially outward from the outer flow path wall.

A vehicle underbody fairing apparatus for reducing aerodynamic drag caused by a vehicle wheel assembly, by reducing the size of a recirculation zone formed under the vehicle body immediately downstream of the vehicle wheel assembly. The fairing body has a tapered aerodynamic surface that extends from a front end to a rear end of the fairing body with a substantially U-shaped cross-section that tapers in both height and width. Fasteners or other mounting devices secure the fairing body to an underside surface of the vehicle body, so that the front end is immediately downstream of the vehicle wheel assembly and a bottom section of the tapered aerodynamic surface rises towards the underside surface as it extends in a downstream direction.

A mounting assembly for a forward end of a liner in a combustor of a gas turbine engine including a dome and a cowl, wherein a longitudinal centerline axis extends through the gas turbine engine. The mounting assembly includes a pin member extending through each one of a plurality of circumferentially spaced openings formed in the forward end of the liner, an aft portion of the cowl, and a portion of the dome, with each pin member including a head portion at one end thereof. A nut is adjustably connected to an end of each pin member opposite the head portion. A bushing is located on each pin member at a position intermediate the head portion and the nut, wherein the openings in the liner forward end are sized to fit around the bushings. In this way, the cowl aft portion and the dome portion are fixedly connected together between the bushing and the nut so that the bushings are able to slide radially through the openings in the liner forward end as the cowl and the dome experience thermal growth greater than the liner.

A multi-section blade for a wind turbine comprising a hub extender connected to a hub of the wind turbine is provided. The blade includes at least one pitchable outboard section. The hub extender can have a pitch bearing located near the interface between the hub and hub extender, or the hub extender and outboard blade section. The hub extender can be configured to pitch or not pitch with the outboard blade sections. An aerodynamic fairing is configured to mount over the hub extender and is configured to not pitch with the outboard blade sections.

A three-wheeled vehicle for on-road use with a modular front headlight system that complies with both United States and European Community laws is disclosed. The modular system includes a headlight module, an air intake module, and a fairing module.

A device for fastening bumper fairings to the fenders of a motor vehicle. A window is formed in the rim of the bumper fairing and a resilient tongue is provided in the fender to penetrate into said window when the bumper is in place, thereby holding the rim in its housing.

A fairing structure for a vehicle having a front vehicular component and a rear vehicular component in tandem and separated by a gap, comprising a top fairing surface adapted to be attached to the rear vehicular component, a first side surface adapted to be attached to a first side of the rear vehicular component, joining a first end of the top surface and generally perpendicular to the top surface, and a second side surface adapted to be attached to a second side of the rear vehicular component, joining a second end of the top surface opposite the first end and generally perpendicular to the top surface. Each of the top and first and second side surfaces has a proximal edge adapted to be positioned adjacent a vehicle, as well as a distal edge adapted to be positioned away from the vehicle with respect to the respective proximal edge. The proximal edges of the top and side surfaces attach to the leading top and side edges, respectively, of the front surface of the trailer box, so that an approximately uninterrupted surface is formed from the fairing structure to top and sides of the rear vehicular component. The area bounded by the distal edges of the surfaces is smaller than an area bounded by the proximal edges. The top side surface, the first side surface and the second side surface are made of a resilient material in the regions distal from the regions where the first side surface joins the top side surface, and where the second side surface joins the top side surface, the top side surface including a heat and fire resistant material in the regions proximate to the first and second side surface, and the first and second side surfaces including a heat and fire resistant material in the regions proximate to the top side surface.

A gas turbine engine has a plurality of radial struts in a bypass duct. At least one strut has a scoop incorporated with the fairing of the strut and in communication with an air passage of an engine secondary air system. The scoop faces a bypass air flow to scoop a portion of the bypass air flow using available dynamic pressure in the bypass duct. Scooped air may be provided, for example, to an active tip clearance control apparatus in a long duct turbofan engine.