« The perils of combat airlift | Main | Clean, quick and composite - Europe's R&D targets »

Discopter - what goes around comes around

Steve Trimble over on The DEW Line reveals Boeing has a DARPA contract to study a disk rotor high-speed rotorcraft. Like most things in aerospace these days, this is not a new idea.

Swiss architect and designer George Vranek, on his diskrotor website, traces the concept of a circular rotor with retractable blades back to Germany in 1962 and also mentions a 1992 NASA Ames study.

US engineering firm owner Frank Black has tried for years to find backers for his Modus Verticraft concept, and now Nowegian firm SiMiCon is working on a retractable-blade disk rotor UAV.


They all see the same attraction - the ability to hover like a rotary-wing aircraft then retract the blades to fly fast like a fixed-wing aircraft. They all take slightly different approaches. While Vranek's concept has conventional rotor blades, the Modus design has a larger number of shorter fan blades. Modussm.jpg

Some concepts drive the disk rotor conventionally, and need an anti-torque mechanism. Others would duct engine exhaust to the disk's periphery to drive the rotor, avoiding the need for a tailrotor. SiMiCon's UAV is steered by moving the centre of rotation of the circular wing. All need a powerplant that converts from driving to rotor to propelling the vehicle.

It will be interesting to see which approach Boeing takes. DARPA appears to be funding a number of different advanced concept studies and its endorsement is far from a guarantee of success. After all, Boeing and DARPA had to abandon the Canard Rotor Wing after both demonstrators crashed. Maybe the disk rotor will have better luck.

TrackBack

TrackBack URL for this entry:
http://www.flightglobal.com/cgi-bin/mt/mt-tb.cgi/13090

About

This page contains a single entry from the blog posted on October 12, 2007 3:56 PM.

The previous post in this blog was The perils of combat airlift.

The next post in this blog is Clean, quick and composite - Europe's R&D targets .

Many more can be found on the main index page or by looking through the archives.