About 61 results
https://drivepatents.com/patents/1010336 · 10 Aug 2011
The housing has an outer ring (3), inner ring (1) and an intermediate ring (2), which are supported against each other via an inner strut (4. 1) and outer strut (5.1). An auxiliary device gear box (7) is connected with a radial shaft (6). Other outer strut...
https://drivepatents.com/patents/1011656 · 22 Jun 2011
The arrangement has a breather pipe (13) which leads into a setting chamber (12) formed inside an exhaust cone (9) of a gas turbine engine. A venture nozzle (14) is positioned in an exhaust gas flow of the gas turbine engine, and is arranged in the flow di...
https://drivepatents.com/patents/1011672 · 22 Jun 2011
The arrangement has a breather pipe (10) which leads into a diffuser (13) integrated in an exhaust cone (9). The exhaust cone proceeds from an exhaust flow (A) of a gas turbine engine for conversion of a kinetic energy of an oil venting air into a pressure...
https://drivepatents.com/patents/1016368 · 19 Jan 2011
The engine has a core-flow channel (5), and a bypass duct (3) surrounding the core-flow channel and comprising an inner sidewall (2). The sidewall is retained against an engine lining (1). The sidewall has a straight, conically widening form that is smooth...
https://drivepatents.com/patents/1069396 · 8 Mar 2006
The fan machine with at least one stator and a downstream rotor, for gas or liquid flows, has fixed vanes (1) with a rounded radius (12) at the stator and the rotor with a number of vanes is on a rotating shaft. A housing contains the flow through the asse...
https://drivepatents.com/patents/1071360 · 28 Dec 2005
Air (3) entering the blower or compressor passes a first row of stator blades (4) with air injection nozzles (11) at the blade roots on the stator housing (2). There is a first row of rotor blades (7) and a second row of stator blades (5) which may have ai...
https://drivepatents.com/patents/1077335 · 1 Jun 2005
The machine has a rotor with several rotor vanes (8) fixed on a rotating shaft whereby the means for removing the flow medium from at least one vane of one row are provided at non-axially symmetrical aerodynamically critical spots on the vane tips and ring...
https://drivepatents.com/patents/1078445 · 20 Apr 2005
The blade has a tip section (5) assembled to a base section (2) by a joining weld (4). The base section that is made of a metal e.g. titanium, includes long cavities (7, 9) that originate at an upper abutting edge (6) of the base section. The cavities are ...
https://drivepatents.com/patents/1081192 · 29 Dec 2004
The control for an aircraft engine produces optimum power of the basis of aircraft data for different engine output levels and multiple power defining thermodynamic and mechanical engine parameters. For each power defining engine parameter (L1-4) an indivi...
https://drivepatents.com/patents/1082833 · 27 Oct 2004
The high pressure gas turbine has a turbine disk (1) with running paddles (2) and guide paddles (3). A side zone (5) is formed between the turbine disk and a guide paddle rim (4). A seal (8) is formed in the axial direction between the guide paddle platfor...