Blade Droop Stops
    
    When a helicopter is at rest, the blades will droop because of a lack of centrifugal
        stiffening. To prevent them from hitting the fuselage when starting
    up or shutting down (at this time, rotor RPM is low, and so centrifugal stiffening
    is also low), we need droop stops. These are used to limit blade travel both up and down. The upwards stops are utilised to restrict excessive blade sailing when starting the
        helicopter up in a wind.
    
         
      
    
        Because a blade at rest is very flexible, it can droop quite significantly. This suggests that the droop stops have to limit downwards travel to a great extent.
        The
        blade now only has a very limited ability to travel. However, in flight, and
        because the blades are stiffened by centrifugal forces, more downwards travel may be needed in order to flap down without being in danger of hitting
        the fuselage
        (in a non zero offset head, the fuselage also tends to follow disc attitude). To provide
        this greater degree of freedom, there are solutions which allow more blade
        travel when rotor RPM gets above certain limits. These constructions function by using
        centrifugal forces to put the droop stops out of engagement. At a lower RPM,
        a string
        returns the droop stops.
    
    
        All articulated and teetering types of rotorheads use some form of droop stops. 
   Next topic > Underslung Rotor Design
    
        
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