I looked it up & answered my own question...the only reason this thing was replaced was AGE. The first one flew in 1947 & they stayed in service until the 1970's! It must have been a very good concept!
I just read an article about this. It was rejected by the military just because "shafts seemed too complex". What the heck? The conventional tail rotor, NOTAR or counter rotating rotors are classified as more much more complex by many books on helicopters.
I bet there were just some serious money behind in-service helicopters.
LOL helicopter was first proven as a concept and made by russian immigrant.
Igor Iwanowitsch Sikorski, the inventor of first helicopters was well aware of Anton Flettner's variation, but didn't bother to investigate as that would require new R & D, and he was not doing all that great with his existing helicopter layout.
Its to bad that there has not been further development of this rotor configuration for usage in unmanned vehicles. This type of rotor configuration is possible of flying high, high recon.
I bet it has something to do with varying the drag one rotor creates using the servoflaps. The speed of both rotors must be synchronized and mechanically interdependent. This is not something you'd want to leave to chance! :p
@briansmobile1 The rotors are connected to each other, sort-of, through a relatively simple transmission so the individual rotor speeds always match each other.
unfortunately the time required each week to untangle the rotor blades was prohibitive.
shooter963 1 month ago
Does any one know what kind of engine they first used during initial testing?
bnjones28 3 months ago
omg, how the hell would you do blade tracking on that thing :|
glennlopez 1 year ago
I looked it up & answered my own question...the only reason this thing was replaced was AGE. The first one flew in 1947 & they stayed in service until the 1970's! It must have been a very good concept!
lst1195 1 year ago
@lst1195
It is stable and simple.
I don't know why it wasn't utilised on military attack helicopters.
SEThatered 1 week ago 2
@SEThatered Yeah the K-max looks like a born Gunslinger with a thin Silhouette & everything. Surprised nobody tries that out.
lst1195 1 week ago
@lst1195
I just read an article about this. It was rejected by the military just because "shafts seemed too complex". What the heck? The conventional tail rotor, NOTAR or counter rotating rotors are classified as more much more complex by many books on helicopters.
I bet there were just some serious money behind in-service helicopters.
SEThatered 1 week ago
@SEThatered Yeah in the 1960's bell had some congressman by the nads. Howard Hughes was lucky to sell the OH-6A from what I've read.
lst1195 1 week ago
@lst1195
It is just plain stupid.
u.s.a. (bell and sikorski giants in particular) are insisting on inherently unstable and power wasting "one main rotor + tail rotor" design.
The system implemented in Flettner Fl 282 (predecessor of K-MAX)
was much more stable and simple and easy to use than a single rotor already back then in 1922.
us army even ditched teaching pilots on a copy of Fl 282, as it was more easy to fly and didn't prepare pilots for single rotor...
SEThatered 1 week ago
I guess the KMAX is the desendant of this thing? I remember the Airr Force flew the Huskie...were they not popular? why were they dropped?
lst1195 1 year ago
Some day, the Russians will make an even crazier looking one...
igotbored44 1 year ago
@igotbored44
LOL helicopter was first proven as a concept and made by russian immigrant.
Igor Iwanowitsch Sikorski, the inventor of first helicopters was well aware of Anton Flettner's variation, but didn't bother to investigate as that would require new R & D, and he was not doing all that great with his existing helicopter layout.
SEThatered 1 week ago
It's strange that the tail-rotor configuration being THE most sloppy and inefficient of all is the one the prevailed.
Afrocanuk 1 year ago
@Afrocanuk
Sometimes people overlook better solutions just because they mastered the worst one better.
SEThatered 1 week ago
I was there.
superskullmaster 1 year ago
sowas von hässlich :-D
ClanOfSteel 2 years ago
Its to bad that there has not been further development of this rotor configuration for usage in unmanned vehicles. This type of rotor configuration is possible of flying high, high recon.
idrobinhood 2 years ago
I believe Lockheed Martin is pursuing an unmanned version of the KMAX which has this same configuration.
rs232killer 2 years ago
It's an old an very effective rotor configuration
watch?v=64fgG2CnHn0
Grommo 2 years ago
Internal Gyro?
briansmobile1 2 years ago
How is directional control achieved? Don't the rotors have to be equal in speed to prevent hitting each other?
briansmobile1 2 years ago
yes! and its main rotors are controled with the same principal of normal helicopters.
Helicopterpilot16 2 years ago
@briansmobile1
I bet it has something to do with varying the drag one rotor creates using the servoflaps. The speed of both rotors must be synchronized and mechanically interdependent. This is not something you'd want to leave to chance! :p
M4xPower 1 year ago
@M4xPower Good call ; )
briansmobile1 1 year ago
@briansmobile1 The rotors are connected to each other, sort-of, through a relatively simple transmission so the individual rotor speeds always match each other.
shooter963 1 month ago
KOLM
miketacoma5 3 years ago
very good looking pilot!
SAGpilot 3 years ago