An aircraft can include a turbine engine including a rotor and a stator, and also including a compressor, a combustor, and a turbine in axial flow arrangement. The aircraft can further include an anti-icing system with a magnetic field generator having a rotating portion and a non-rotating ...
One described example apparatus includes a skin (206) on an inlet side of a nacelle (201) of an aircraft defining an annular chamber (211), a gas delivery system (212) disposed within the annular chamber to provide a first gas to mix with and entrain a second gas in the annular ...
Anti-icing system for aircraftAnti-icing system for aircraftdoi:EP0436243 A2EP0436243A2 Dec 4, 1990 Jul 10, 1991 The Boeing Company Anti-icing system for aircraftEP0436243A2 * Dec 4, 1990 Jul 10, 1991 The Boeing Company Anti-icing system for aircraftEP...
RegisterLog in Sign up with one click: Facebook Twitter Google Share on Facebook anti-icing Acronyms anti-icing [‚an·tē′īs·iŋ] (aerospace engineering) The prevention of the formation of ice upon any object, especially aircraft, by means of windshield sprayer, addition of antifreeze ...
An actuating linkage is provided for use in an aircraft engine having a double door-type particle separator, anti-icing system installed within its air intake ducts. The actuating linkage interconnects the deflecting vane and the bypass door through a coupler link. The deflecting vane is pivotally...
Aircraft engine inlet cowl anti-icing system 专利名称：Aircraft engine inlet cowl anti-icing system 发明人：Wallace M. Schulze 申请号：US07/251727 申请日：19881003 公开号：US05088277A 公开日：19920218 专利内容由知识产权出版社提供 摘要：A system is provided for preventing and removing ice ...
Another icing condition detection system that is part of the FIPS is the Super-Cooled Large Droplet marker (SLD). This system consists of a black/yellow/red colored sphere visually indicating whether the aircraft is flying in normal ice accretion conditions (black), or if they are becoming too...
For more than 30 years, Safran Aerosystems anti-icing detection and protection systems and equipment have offered a range of innovative and reliable solutions to make flights safer, to reduce energy consumption and to lower pilot workload.
The article discusses the automatic control system of the Diamond DA42 aircraft anti-icing system. The project was created in MATLAB environment equipped with the Fuzzy Logic Toolbox package. The discussion revolves around the problem of preventing icing. In the analysis four parameters were taken ...
The present invention relates generally to antiicing systems for airplanes. More particularly the invention relates to that type of airplane anti-icing system which serves either to prevent the format