22nd Congress of International Council of the Aeronautical Sciences, Harrogate, UK, 28 August - 1st September, 2000
Paper ICAS 2000-5.3.R1
THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES
D. Ikaza, P.R. Zarda, C. G. Ruiz
Null
Keywords: thrust vectoring nozzle, military aircraft
Even though Thrust Vectoring is a relatively new
technology, it has been talked about for some time, and
several programmes worldwide have explored its
application and benefits. Thrust Vectoring can provide
modern military aircraft with a number of advantages
regarding performance and survivability, all of which has
an influence upon Life Cycle Cost.
There are several types of Thrust Vectoring Nozzles. For
example, there are 2-D and 3-D Thrust Vectoring
Nozzles. The ITP Nozzle is a 3-D Vectoring Nozzle.
Also, there are different ways to achieve the deflection of
the gas jet: the most efficient one is by mechanically
deflecting the divergent section only, hence minimizing
the effect on the engine upstream of the throat (sonic)
section.
The ITP concept consists of a patented design featuring
the so-called “Three-Ring-System”, which allows all
nozzle functions to be performed with a minimum
number of actuators, which, in turn, leads to an optimized
mass and overall engine efficiency.
ITP has dedicated a research programme on Thrust
Vectoring technology which started back in 1991, and
which met an important milestone as is the ground testing
of a prototype nozzle at ITP.
The next major goal will be the realisation of a flight
programme, in order to validate the system in flight, and
evaluate the capabilities and performance of the system
as a means of primary flight control.
A decisive contribution is being done by ITP’s partner
company MTU of Munich, Germany, by developing the
electronic Control System.
This programme is making the Thrust Vectoring
technology available in Europe for existing military
aircraft such as Eurofighter, in which the introduction of
Thrust Vectoring could be carried out with a relatively
small number of changes to the aircraft and to the engine,
and could provide it with significant enhancements.
view full paper