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the Aviation Dictionary

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blade dampener blanket method of recovering

hub. The airfoil shape of the cuff pulls cooling air into

the engine nacelle.

blade dampener - A shock absorbing mechanism

installed between a helicopter rotor blade and the hub

to diminish or dampen blade movement on the lead-lag

axis.

blade droop - The angle of the spa nwise axis of the

helicopter rotor at rest with only the : forces of gravity

acting on it.

blade face - The flat portion of a propeller blade,

resembling the bottom portion of an airfoil.

blade featherlfeathering - In rotorcraft, the rotation of

the blade around the spanwist: (pitch change) axis.

blade fillet -The portion of the blade closest to the base

or platform. Usually an area where the least damage is

allowed.

blade flap - In rotorcraft, the ability of the rotor blade to

move in a vertical direction. Blades may flap

independently or in unison.

blade flapping - The movement of helicopter rotor

blades, about a horizontal hinge, in which the blades

tend to rise and descend as they rotate. Blade flapping

tends to minimize asymmetrical lift by increasing the

angle of attack of the retreating blade while decreasing

the angle of attack of the advancing blade.

blade stall - A condition of the rotor blade in flight

when it is operating at an angle of attack greater than

the maximum angle of lift. This occurs at high forward

speed to the retreating blade and to all blades during

"settling with power."

blade station - Reference voints on the blade measured

in inches from the center of the propeller hub. Blade

station measurements are used to identify locations

along the blade of a propeller.

blade sweeping - An adjustment of the dynamic

chordwise balance in which one or both blades are

moved aft of the alignment point.

blade tabs - Fined tabs mounted on the trailing edge

helicopter rotor blades for track adjustment.

blade tip - In rotorcraft, the of the blade the

furthest from the hub of the rotor.

blade track - In rotorcraft, the relationship of the blade

tips in the plane of rotation. Blades that are in track

will move through the same plane of rotation.

blade tracking - 1. The process of determining the

position of the tips of the propeller blades relative to

each other. 2. The mechanical procedure used to bring

the blades of the rotor in satisfactory relationship with

each other under dynamic conditions so that all blades

rotate in a common plane.

blade grips - The part of a helicopter rotor hub into blade twist -The variation in the angle of incidence of a

which the blades are attached by a lead-lag hinge pin. blade between the root and the tip. The amount of

Blade grips are sometimes referred to as blade forks.

thrust that is produced by a propeller blade is

determined by the pitch angle of the blade at each

blade inspection method (BIM)- A system using an

blade station, and by the speed at which the blade is

indicator and inert gas to detect rotor blade cracking.

moving through the air. In order to maintain a constant

Used by Sikorsky Helicopter.

amount of thrust along the blade, the blade angle must

blade inspection system (BIS)- A method used by Bell be twisted; however, some degree of twist can also be

Helicopter to determine if rotor blades have cracked.

caused by aerodynamic forces.

blade lead or lag - In rotorcraft, the fore and aft

movement of the blade in the plane of rotation. It is

sometimes called hunting or dragging.

blade loading - In rotorcraft, the load imposed on rotor

blades, determined by dividing the total weight of the

helicopter by the combined area of all the rotor blades.

blade root - The portion of a propeller blade that fits

into the propeller hub. The blade root is also called the

blade butt.

blade section - A cross section of a propeller blade

made at any point by a plane parallel to the axis of

rotation of the propeller and tangent at the center of the

section to an arc drawn with the axis of rotat~on as its

center.

blade shank - The thick, rounded portion of a propeller

blade near the hub.

blade wrench - A paddle-shaped lever having a slot

shaped to fit the cross section of a propeller blade.

Used for manually turning propeller blades. Blade

beams are also referred to as blade wrenches.

blade-disk - A forged, one-piece compressor or turbine

blade and disk as opposed to separate blades fitted into

a disk.

blank - To cut out the surplus material from a part, prior

to finishing.

blank blade - The identification of one blade of a

helicopter during electronic balancing. It is the blade

with the single interrupter. The target blade will have

the double interrupter.

blanket - 1. A sheet of insulation material in the cabin

and passenger compartments used to aid in suppressing

noise. 2. A shroud covering for airplane heat ducts.

blade span - In rotorcraft, the length of a blade from its blanket method of recovering - The method of

tip to its root.

applying fabric to an aircraft structure so that the fabric

Aircraft Technical Book Company

P.O. Box 270

Tabernash, CO 80478

http:llw.ACTechbooks.com

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