About 61 results
https://drivepatents.com/patents/996056 · 14 Nov 2012
The engine has a core thruster (10) surrounded by a by-pass channel (29). A radially expressed engine cowl (30) encloses the by-pass channel and is placed at a rear portion of a thrust-reverser (31). The thrust-reverser is moveable relative to the engine c...
https://drivepatents.com/patents/996050 · 14 Nov 2012
The gas turbine engine has a compressor (13) and an air bleed device that is comprised of an annular channel (30) in a radially outer wall (31) of a flow channel (29). An annular sealing element (32) is arranged in the region of the annular channel, and is...
https://drivepatents.com/patents/997581 · 3 Oct 2012
The device (9) has an air-carrying duct (11), a fuel-carrying duct (10), and guide elements (14,15) provided in air-carrying duct, extending over a height of air-carrying duct and distributed over a circumference of air-carrying duct. Each guide element ha...
https://drivepatents.com/patents/998577 · 5 Sep 2012
The device (1) has a set of strut-like support elements (17) connected at one end to an inner wall (3) and at another end to an outer wall (4). Each support element has a thickness distribution defined along a central longitudinal plane (21). Each plane fo...
https://drivepatents.com/patents/1005897 · 25 Jan 2012
The bleed air discharge opening has a covering that is designed as aerodynamic casing element (3) and is elongated, particularly oval or saucer-type and extends in longitudinal direction of a bypass duct (2).A base (10) with convex bending is provided in l...
https://drivepatents.com/patents/1008466 · 19 Oct 2011
The bypass flow channel comprises guide wheel (1) and a guide wheel scoop (2) to untwist fan generated air flow, where a cladding element is provided for installing secondary flow channel such as cables, brackets, supports or drive transmission medium. The...
https://drivepatents.com/patents/1008518 · 19 Oct 2011
The engine has core engine unit (1) comprising high pressure turbine (6) and downstream low pressure turbine (7). The core engine unit is surrounded by a bypass duct (18) and mixer (19) is arranged in an inlet portion of low pressure turbine. The bypass fl...
https://drivepatents.com/patents/1009520 · 14 Sep 2011
The element has a supporting structure radially extended between inner and outer walls of a bypass duct and including a front edge part (7) and a rear edge part (8). A connecting rod (9) connects the front and rear edge parts to form a recess that extends ...
https://drivepatents.com/patents/1009757 · 31 Aug 2011
The gas turbine (1) has a bleed air system (4) for the compressor (2), a tap (5) on the housing (3) of the compressor and a bleed air outlet (6). A bleed-air chamber (7) is formed between the tap and the bleed air outlet. The bleed air system has a device,...
https://drivepatents.com/patents/1009711 · 31 Aug 2011
The bypass duct has support struts, which are formed as guide vanes-support struts (3) with bigger thickness and chord length than the guide vanes (2) in an aligned aerodynamic form. A flow channel (4) existing between a suction side (7) of the guide vane-...