| The
SO.1221 Djinn in Switzerland
by
Mario Bazzani
The Djinn1 is a French two
seat turbine powered helicopter which made its first free flight on December
14th, 1953 with pilot Jean Dabos at the controls. In this helicopter the
main rotor is driven by compressed air supplied by a turbine located behind
the cabin. The compressed air is transmitted directly to the rotor blades
and is expelled from a nozzle placed on each blade tip. The elimination
of the usual mechanical transmission also eliminates the need of an antitorque
tail rotor. The Djinn in fact dispose of a simple rudder placed in the
continuos flow of the engine exhaust gas which is controlled by foot pedals
like in the others helicopters of conventional design and offer an “efficient”
control on the vertical axis. The great inertia of the Djinn’s rotor is
one of its most appreciated characteristics.
Up today this French model
is the only one with this configuration produced in series for military
and civil uses, and is even the first turbine powered helicopter mass produced.
The prototype, registered
as F-WGVH, was the result of the experiences made before with the predecessors
built by the French company Sud Ouest, like the Ariel series or the SO.1220,
the single place version of the SO.1221. The Djinn was an excellent climber,
and set many altitude records. On March 22, 1957 it set a new unofficial
world record when it climbed to 8482 meters, a record that later was broken
by an Alouette II.
On February 1955 the pilot
Dabos and a small technical staff arrived here in Switzerland with the
F-WGVY (the first pre-serie model of the Djinn) to demonstrate its flight
characteristics. Between February 7th and March 3th 1955 the helicopter
made several flights in the Jungfrau region and proved to be a good mountaineer.
It took-off and landed without problems from the Jungfraujoch at 3520 m
with a passenger. In this occasion the small helicopter captured the interest
of Air Import SA (the Swiss first civil helicopter’s company) and the Swiss
Army.
Air Import SA was so impressed
by the performances of the Djinn that decided to acquire one of them in
November of the same year. Unfortunately the helicopter, registered as
HB-XAN (an SO.1221 PS), was lost on May 4th 1956 in an accident in the
Innerthal/Trepsenalp during a slung load transport. A second one registered
as HB-XAS (an SO.1221 S) joined the fleet by the end of the year and remained
in service until October 16th, 1958. In January 1957, after Air Import
was absorbed by Heliswiss AG, it was used for school and much later it
was sold in France. Heliswiss had decided to use only Bell 47 models, because
these offered more space in cabin (two passengers instead of one), a greater
payload and superior performances.
The Swiss Army put in service
a total of four SO.1221 S. The first 3 were registered as V-21, V-22 and
V-23 and entered in service in February 1958. On September 2nd, 1958 the
V-21 was destroyed in an accident occurred in Andermatt (cable collision).
On July of the following year a fourth Djinn was acquired and registered
as V-24. These 3 helicopter remained in service with the Army until 1966.
The V-23 is now exposed in the “Fliegermuseum” in Dübendorf.
The Djinn was a versatile
helicopter, designed especially for light transports, school, aerial observation
and photography, air ambulance and liaison duties, aerial sprayer, etc.
It could be equipped with 2 external litters, an agricultural kit, an hook
for slung loads, and was experimentally used for trials with guided missiles.
In the Unites States the Djinn was tested by the U.S. Army as YHO-1DJ.
On August 6th, 1958 it received the CAA type certification.
The appearance of the new
turbine powered SE. 3130 Alouette II signed the end of the Djinn’s military
career. The limited forward speed and short range, as the limited payload
and high fuel consumption were its main limitations. However this helicopter
continued to be used for many years in civil roles as a school helicopter
or in agriculture as aerial sprayer. Today, after 50 years from its first
flight, many Djinn still survives, but the major part of them is exposed
in museums. Very few are still in flying condition - among them the F-AZAC
|
SO.1221 S
Djinn - Technical Specifications
|
| Main
dimensions |
Performances |
| Rotor diameter |
11.00 m |
Max. speed (Vne) |
125 km/h |
| Fuselage length |
5.30 m |
Cruising speed |
90-100 km/h |
| Max height |
2.60 m |
Hoovering IGE |
1500 m* |
| Max wide |
1.93 m |
Hovering OGE |
900 m* |
| Rotor disk area |
95.00 m2 |
Max. ceiling |
3100 m* |
| (rotor rpm min/max) |
300/400 |
Std rate of climb |
2-3 m/sec* |
| (rotor std rpm) |
380 |
Max. range |
190 km* |
| (disk loading) |
8 kg/m2 |
Max. endurance |
2h 15min* |
| |
| Weights |
Tank/fuel |
| Empty weight |
380 kg |
Std tank capacity |
250 litres |
| MTOW |
760 kg |
Std fuel consumption |
120 l/h |
| |
Power
unit
The Djinn’s power-plant
is a Turboméca Palouste IV of 179/240 Kw/hp compressed air generator
which supplies air under pressure to the blades. The rotor is driven exclusively
by the ejection of compressed air trough the blade-tip nozzles. |
| |
Optional
equipments
Two external stretchers,
agricultural spray kit for aerial applications, hook for external slung
load transport. |
| |
Features
- safe autorotation from
any altitude and/or speed
- no transmission
- hight rotor inertia
- no tail rotor
- low disc loading
Note: Djinn, pronounced “gin”
means “little devil”
* Std day conditions / 700
kg TOW |
|
HB-XAN
- Registered in November 1955
HB-XAN
- The first of two civil Swiss Djinn's
HB-XAS
- Owned by Air Import and later Heliswiss
A
Djinn engine during rebuild
F-AZAC
- After rebuild by Jet Systems in 2002
F-AZAC
- in June 1995 at Monaco
|