HELICOPTER Flashcards
Because of lift differential due to differing rotational relative wind values along the blade, the blade should be designed with a TWIST to alleviate internal blade stress and distribute the lifting force more evenly along the blade.
BLADE TWIST
Because of lift differential due to differing rotational relative wind values along the blade, the blade should be designed with a
TWIST to alleviate internal blade stress and distribute the lifting force more evenly along the blade.
provides higher pitch angles at the root where velocity is low and lower pitch angles nearer the tip where velocity is higher.
BLADE TWIST
This increases the induced air velocity and blade loading near the inboard section of the blade.
BLADE TWIST
Blade twist sections
SECTION NEAR ROOT
SECTION IN CENTER
SECTION NEAR TIP
TRUE/FALSE
“More nose-down” tilt to blade section closer to tip
TRUE
TRUE/FALSE
“Less nose-down” tilt to blade section closer to tip
FALSE
TRUE/FALSE
“More nose-down” tilt to blade section further to tip
FALSE
on the mast, the attaching point for the root of the blade, and the axis about which the blades rotate.
HUB
the farthest outboard section of the rotor blade
TIP
the inner end of the blade and is the point that attaches to the hub
ROOT
the change in blade incidence from the root to the outer blade
TWIST
Helicopters are used for many different reasons and they may be the most ______vehicle in the world
versatile
A helicopter can do it all: 1._____,2._____3.______4._____________
From leg-like skids to electric tail rotors, it will be interesting to see how much further the helicopter develops.
- hover
- land on uneven ground
- travel vertically
- horizontally and every other direction in between
two main types of engine
reciprocating engine, turbine engine
use one or more pistons to convert pressure into a rotating motion creating power
reciprocating engine