CHAPTER I - Meeting the Kolibri
The  Flettner Fl-282 Kolibri, a single seat open cockpit intermeshing rotor  synchropter, was the World's first mass produced helicopter and the  first helicopter to land on a ship. Today one can say without  exaggeration that it was the best helicopter of its day. It was actually  an improved version of the previously built Flettner Fl-265, a  pioneering example of a synchropter with two intermeshing rotors. The  exact date on which the RLM issued the development contract for the  Fl-282 is not really known. It can be assumed with certainty, however,  that design work was begun in 1939 while testing of the Fl-265 was under  way. All the test results and experience from the previously built  Fl-265 were applied to the design of the Fl-282. By mid-August 1941 work  on the Fl 282 V1 had progressed to the point where it could be used on  the ground as a transmission unit test bed. The test bed was anchored  but could climb the length of the restraint to a certain height and  hover. 125 hours and 39 minutes were spent in these tests, which lasted  until November 21st 1941. In the event of the destruction of the V1 or a  lengthy interruption of testing due to some other problem, it was  planned to use the V4 as a replacement test bed. First free flight was  made by the V2 on October 30th 1941. At the controls was test pilot  Ludwig Hoffmann, who had joined Flettner as the successor to company  pilot Perlia. Flight tests resumed in March 1942 following design  changes to the cardan shaft; the tests revealed a significant  improvement in the helicopter's handling. The Fl-282 V2 was taken out of  service on May 25th 1942; the aircraft's transmission & engine were  removed for use in other prototypes. Test pilot Ludwig Hoffmann carried  out two altitude flights in the Fl-282 V3 on April 27th 1942. On the  first he reached a height of 3500 meters over the takeoff point and on  the second attempt 3800 meters in 36 minutes (from 15:17 to 16:10  hours).
In following pictures, the Fl-282 prototype helicopters.  The V2 (registered as GF-YB) with fully glazed cockpit, completed its  first flight on October 30th 1941 and the V3 (registered as GF-YC) had  "H" shaped horizontal stabilizers with end plates. The first three  prototypes ("A" series) had fully enclosed cabins made up of a series of  optically flat plexiglass panels, faired-in rotor pylons and  well-contoured fuselages. The V3 version was fitted with endplate  auxiliary fins and a long underfin beneath the rear fuselage. Later  machines had more utilitarian bodies. Some ("B-0" series) had a  completely open pilot's seat, some ("B-1" series) had semi-enclosed  cockpits by flat plexiglass panels and finally some others ("B-2"  series) had cockpits enclosed by combination of plexiglass & wooden  sidewalls.
The  idea of the helicopter was new at that time and Anton Flettner and his  team made a lot of efforts to convince the German Air Ministry that it's  a good product. One of these efforts was to take an average German  housewife and teach her to fly the new helicopter. As seen into  following photograph, they finally proved that the vehicle was extremely  stable and very easy to fly. So easy, that an average German housewife  with no previous flying experience, managed to control the Fl-282 V22  (registered as CI-TV) helicopter, after only 3 hours of flight training.
The  fuselage was constructed from truss-type welded steel tube, covered  with doped fabric. It was fitted with a fixed non-retractable tricycle  type undercarriage, with the braced fixed nose wheel with VDM oil shock  absorber leg coupled with the rudder foot pedals for steering. Nose  wheel was equipped with a 350x150 mm tire and main gear with 465x165 mm  tires. The rectangular outline with rounded tips rotor blades were made  by tubular steel spar with riveted-on wooden ribs and plywood skin with  fabric covering and axes of both rotors were angled outboard at 12° from  the vertical. Seen from above, the right rotor rotates clockwise and  the left rotor counter clockwise. At the rear end of the fuselage, a  two-part horizontal stabilizer with single spar was provided for  trimming purposes and a rudder fin of very generous area. This large  area was necessary because much of it was ineffective due to the poor  aerodynamic shape of the fuselage causing rearwards flow separation and  turbulence. It was constructed by tubular steel spar with riveted-on  wooden ribs, plywood leading edge & fabric-covered. Steering of the  Fl-282 was by a combination of the rudder and differential collective  pitch change on the two rotors, but only the rudder could give steering  during autorotation since collective pitch was then ineffective (another  reason for the large rudder area). Rudder fin was made of wood and  covered by fabric, with 40° deflection. The vertical stabilizer and the  elevators were also made of wood, with plywood leading edge and fabric  covering, bolted to fuselage frame.
It was equipped with flight and navigation instruments such as an ASI -  AirSpeed Indicator, an altimeter, a VSI - Vertical Speed Indicator, a  turn & bank indicator, RPM indicator for rotors, rotor blade angle  indicator, a master compass and a dashboard clock. Radio &  signalling equipment consisted of a FuG 19 ultra short wave radio  installation. Back type parachute, first aid kit, signal flare pistol  and one-man inflatable raft were also present. In following pictures,  the instrument panel of the first three prototype helicopters with fully  enclosed cabins made up of a series of optically flat plexiglass  panels.
The  Flettner Fl-282 Kolibri was equipped with a Bramo Siemens Halske  SH-14A, 7-cylinders radial engine of 119 kW (160 hp) mounted in the  center of the fuselage, with a transmission unit on the front of the  engine from which a drive shaft ran to an upper gearbox, which then  split the power to a pair of opposite drive shafts to turn the rotors.  The SH-14A was an already tried engine design that only required  servicing every 400 operating hours.
A  drive shaft with universal joints took the drive from the engine  transmission unit to the upper transmission unit, which consisted of  gears and shafts connecting the two rotor shafts. The final cross-shaft  between the two rotor shafts was fitted with a free wheeling unit to  disconnect the engine drive, and also with a rotor brake. On the  drive-shaft from the engine, a friction disc clutch was fitted which was  used for running up the rotors until there was no slippage, when a  positive dog-type clutch, on the same shaft, was then engaged. Total  reduction through all the transmission units was 12.2 to 1. Cooling air  for the enclosed engine was drawn in through openings beneath the  fuselage by an eight blade wooden cooling fan with direct drive from the  engine and a high pressure air tank was connected to the engine  cylinders through a distributor for starting.
The two 2-blade rotors, which were synchronized to be parallel in the  45° position, were mounted on shafts having an included angle of 24°  between them and an inclination forward of 6°. The rotor blades  consisted of wooden ribs mounted on tubular steel spars with a covering  of plywood followed by fabric. Flapping and dragging hinges were fitted,  the latter having friction dampers. A centrifugally operated blade  pitch governor held the rotor rpm within prescribed limits, the governor  being driven through clutches from the rotor transmission. In order to  ensure that power-off autorotation was not lost, the governor was set  for a minimum rotor speed of 160 rpm. With the use of his collective  pitch lever, the pilot could over ride the governor but only to increase  rpm. Under certain conditions, self-excited oscillations could occur in  the rotor; this happened in flight on one occasion when an Fl-282 was  being flown with a high collective pitch and the low rotor speed of 140  rpm (compared with the recommended 175 rpm). Vibration became so severe  that the pilot prepared to bail out, but, before he could do so, the  machine went into autorotation and the vibration ceased.
The  Fl-282 was more highly developed and flew more hours than any other  German helicopter, and very extensive tests and measurements were made  of all flight aspects. Most of this test work was done by Anton  Flettner's chief pilot Oberleutnant (Luftwaffe 1st Lieutenant) Hans E.  Fuisting, who also undertook blind flying and trained many of the 50  pilots who learned to fly the Fl-282 Kolibri. Other test pilots  participated test pilot FliegerStabsingenieur (Luftwaffe Major) Gerhard  Geike, Dipl. Ins. Hans Fischer and Dipl. Ins. C. Bode. Some new pilots  ran into trouble when flying near the ground, because, as they turned  with the wind, they lost lift and struck the ground. One new pilot had a  fatal accident when flying his Fl-282 blind in cloud, and the assumed  cause of the accident was that the machine had been dived and the  controls then pulled back so violently that the blades were forced into  each other or into the tail. The diving speed thereafter was restricted  to 175 km/h. On occasions, the Kolibri was landed autogyro way and  without the use of collective pitch. This was done by vertically  descending, diving nose-down and then pulling back on the controls to  land. Unfortunately, by using this landing technique without the use of  collective pitch, on (at least) one occasion, the tail boom hit the  ground and was damaged.
As seen into following two photographs,  the CJ-SK registered Fl-282 V17 helicopter, following a crash-landing at  Travemünde, on April 13rd 1944, with test pilot FliegerStabsingenieur  (Luftwaffe Major) Gerhard Geike behind controls who replaced the main  test pilot Fliegerstabsingenieur Dipl. Ins. Hans Fischer after he was  badly hurt in a Dornier Do-217 crash.
Extremely  manoeuvrable and very stable, even in gusty conditions, the machine  could be flown hands-off in forward flight above 60 km/h for indefinite  periods by making an adjustment to neutralize the loads on the controls.  However, in forward flight at speeds below 60 km/h there was some  longitudinal instability, which reached a maximum at about 40km/h.  Another slight criticism of the Fl-282 was that it vibrated rather badly  while the rotor was running up on the ground, but this vibration  decreased upon lifting off, although there was still a certain amount of  vibration transmitted to the control column, which was sluggish and  tended to overshoot the requisite amount of movement. Although many of  the mechanical components were unnecessarily complicated and heavy, the  general design and workmanship were of excellent quality.
Since  taxiing under its own power was strictly forbidden, the Fl-282 V12  registered as CJ-SF seen in following picture, pushed back by ground  personnel. This rule imposed because the non vertical angled rotor hubs  resulted in the blade tips at the sides of the craft being around human  body height and made the craft dangerous to approach from the ground  whilst the blades were spinning. In addition, the blades could be damage  by contact with the ground. At heliports these two problems could be  overcome, but at unprotected sites this would be a concern. So, they had  a simple rule that ground crew could not approach at that time or only  directly from the front.
In  following picture, Emil Arnolt (left) chief designer at Anton Flettner  Flugzeugbau GmbH, test pilot Oberleutnant (Luftwaffe 1st Lieutenant)  Hans E. Fuisting and a mechanic (name unknown), in front of company’s  factory plant. Next photograph, Emil Arnolt’s family (wife & kids)  having their first contact with the new helicopter. Pictures provided by  Carsten Arnolt, grandson of Emil Arnolt.
						
						
						
								Aceasta postare a fost editata de Nick_Karatzides: 11 August 2014 - 12:46 AM