blade tip

blade tip

The part of a blade that is the farthest from the hub.
An Illustrated Dictionary of Aviation Copyright © 2005 by The McGraw-Hill Companies, Inc. All rights reserved
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Our materials are in the main and tail rotor blades; blade spar; blade tip and skin; fuselage; tailcone/aft transition; tail rotor pylon; sponsons, doors and engine nacelle.
Each of the 84 turbines stands taller than the London Eye, at 188 metres from sea level to blade tip.
You will learn forging basics and then move on to forge the shape of your knife and make the blade tip. From there, you will cut the blade profile, grind in bevels to make the edge of the knife, heat treat and temper your blade, grind and polish it, and make a handle and sheath for it.
"Blade material, blade thickness and blade tip thickness can all be tailored for a specific job or to resolve a specific problem such as too much ink left on the anilox roll," adds Latosek.
The full blade tip reveal provides an unobstructed view of surgical site, and a 360 degree swivel allows for fluid hand movement.
He drops the knife into his trouser pocket, blade tip down, like a pencil.
The company said the scalable 3-megawatt test turbine has an assembled hub height of 130 meters and a blade tip height of 199.2 meters, making it the tallest wind turbine in the US.
In order to allow the relative motion of blades and to prevent the blade tip surface from rubbing, clearance gap between blades and casing is required in turbomachinery.
In effect, these employees were the company's sensory experts, tasked with judging the shaving experience and rating the double-edged blades for the shaving closeness (blade sharpness), comfort and overall quality of shave observations, such as: smoothness; any irritation of the skin (usually caused by a blunt blade or lack of PTFE coating); whether the blade started to cut on first stroke or not (breaking through the PTFE coating on the blade tip).
Blade tip clearance refers to the tiny gap between the duct wall and the tip of the propeller blade.
Meanwhile, taking the aerodynamic and structural coupling effect conditions into consideration, the mathematical model was established by taking the minimal mass of the blade as the optimization objective, the interaction mechanism between the blade tip deformation and load distribution was studied by using modal analysis.