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2. Fan disk - Wikipedia

   en.wikipedia.org/wiki/Fan_disk

   The one shown in the photo is over 31 inches (1.2 m) in diameter, and rotates up to 3800 rotations per minute (RPM). [3] Fan disks must withstand the centrifugal force of the attached fan blades. Because of their size and weight, a failed fan disk can severely damage an aircraft, as happened with United Airlines Flight 232 in 1989. [4]

3. Centrifugal fan - Wikipedia

   en.wikipedia.org/wiki/Centrifugal_fan

   Figure 1: Components of a centrifugal fan An external motor belt driven inline centrifugal fan discharging inline to the exterior of a building through a duct. Unlike non-inline/non-concentric impeller casing design with a cutoff blade above, the concentrically symetric cylinder casing and impeller geometry of inline type redirects the outflow around so that it is parallel to the inflow of gases.

4. Toyota Corolla (E110) - Wikipedia

   en.wikipedia.org/wiki/Toyota_Corolla_(E110)

   The G6 was a special version of the European E110 Corolla hatchback, powered by a 1.3 L 4E-FE or a 1.6 L 4A-FE engine in the pre-facelift and by a 1.4-liter 4ZZ-FE or a 1.6-liter 3ZZ-FE engine in the facelift, the G6 features color-matched bumpers, front Lip (pre-facelift and facelift optional) and unique to this model: short-ratio 6-speed C161 ...

5. Axial fan design - Wikipedia

   en.wikipedia.org/wiki/Axial_fan_design

   An axial fan is a type of fan that causes gas to flow through it in an axial direction, parallel to the shaft about which the blades rotate. The flow is axial at entry and exit. The fan is designed to produce a pressure difference, and hence force, to cause a flow through the fan. Factors which determine the performance of the fan include the ...

6. Turbofan - Wikipedia

   en.wikipedia.org/wiki/Turbofan

   Blade tip clearances are more difficult to maintain at the exit of the high-pressure compressor where blades are 0.5 in (13 mm) high or less; backbone bending further affects clearance control as the core is proportionately longer and thinner and the fan to low-pressure turbine driveshaft space is constrained within the core.

7. Embraer EMB 110 Bandeirante - Wikipedia

   en.wikipedia.org/wiki/Embraer_EMB_110_Bandeirante

   The Embraer EMB 110 Bandeirante (English: pioneer [2]) is a Brazilian twin-turboprop light transport aircraft designed by Embraer for military and civil use.. The EMB 110 was designed by the French engineer Max Holste; it had been designed in line with specifications issued by the Brazilian Ministry of Aeronautics in 1965. [3]