Concept of Co-Axial Rotors

Coaxial rotors are a pair of rotors mounted one above the other on the same shaft and turning in opposite directions. The advantage of the coaxial rotor is that, in forward flight, the lift provided by the advancing halves of each rotor compensates for the retreating half of the other, eliminating one of the key effects of dissymmetry of lift: retreating blade stall. However, other design considerations plague coaxial rotors. There is an increased mechanical complexity of the rotor system because it requires linkages and swashplates for two rotor systems. Add that each rotor system needs to be turned in opposite directions means that the mast itself is more complex, and provisions for making pitch changes to the upper rotor system must pass through the lower rotor system.

SOURCE:http://www.facebook.com/photo.php?fbid=511945572191300&set=a.499381743447683.126153.116696045049590&type=1&permPage=1

Posted on February 28, 2013, in Aviation. Bookmark the permalink. Leave a comment.

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