| Class / Patent application number | Description | Number of patent applications / Date published |
|---|
| 415227000 | Runner having flow confining continuous passage | 7 |
| 20090053058 | GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE - A turbofan engine includes a fan variable area nozzle includes having a first fan nacelle section and a second fan nacelle section movably mounted relative the first fan nacelle section. The second fan nacelle section axially slides aftward relative to the fixed first fan nacelle section to change the effective area of the fan nozzle exit area. | 02-26-2009 |
| 20090136344 | COOLING MODULE, AND COOLING FAN DEVICE HAVING THE SAME - A cooling fan device includes a main housing having first and second accommodating spaces as well as first and second vent holes, a tubular heat-insulating case body receiving a core unit and a conducting unit of a cooling module and disposed in the first accommodating space, and a fan unit disposed in the second accommodating space and driven by a driving motor to rotate such that air entering into the first accommodating space via the first vent hole flows into the case body through a first opening, is cooled by the cooling module, and then flows out of the case body via a second opening and into the second accommodating space, thereby blowing cooled air in the second accommodating space out of the main housing via the second vent hole. | 05-28-2009 |
| 20110014045 | FAN EXHAUST NOZZLE FOR TURBOFAN ENGINE - The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas turbine engine power plant is greater than the corresponding flow area of the fan discharge nozzle on an opposite side of the central plane to compensate for the blockage of fan airflow by a pylon. | 01-20-2011 |
| 20120163973 | FAN DEVICE - A fan device includes an impeller, a motor, a fan frame, a circuit board and a covering member. The motor is used for driving rotation of the impeller. The fan frame includes an axial-flow channel for accommodating the impeller and the motor and includes a receptacle. The receptacle is defined by two airflow inlet/outlet plates, one channel wall and two lateral plates. The circuit board is accommodated within the receptacle. The covering member is used for sheltering the receptacle. | 06-28-2012 |
| 20130058783 | IMPELLER AND CENTRIFUGAL FAN USING THE SAME - An impeller includes: a main plate; a shroud; and a plurality of blades provided between the main plate and the shroud and arranged circumferentially; wherein the impeller is configured to rotated about a rotation axis; wherein the plurality of blades include a pressure surface and a negative pressure surface; and the pressure surface has a shape, in which at least three types of circular arcs are connected, as viewed from a rotation axial direction. A centrifugal fan includes the above-described impeller; and three or more pillars, wherein an interval between one adjacent pillars of the three or more pillars is different from an interval between the other adjacent pillars of the three or more pillars. | 03-07-2013 |
| 20140363286 | FAN MODULE - A fan module includes an aerofoil fan and an air duct. The aerofoil fan includes a shell defining a vent extending through two opposite ends of the shell and a fan rotatably received in the vent. The air duct is mounted on an end of the shell aligning with the vent. The air duct includes a tapered pipe and a number of latching plates mounted on the pipe. A smaller end of the pipe is located adjacent to the vent of the shell. One end of each latching plate is mounted to a bigger end of the pipe, and the other end of each latching plate is mounted to the shell. | 12-11-2014 |
| 20160003146 | ROTATING INLET COWL FOR A TURBINE ENGINE, COMPRISING AN ECCENTRIC FORWARD END - A rotating inlet cowl for a turbine engine includes a rotation axis. The rotating inlet cowl includes a forward cone defining a forward end of the inlet cowl. The forward end is configured to be eccentric relative to the rotation axis of the inlet cowl. Furthermore, the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl. | 01-07-2016 |
