In the world researches are realized and the development directed on
improvement of existing flying vehicles to decrease aerodynamic drag, to
increase efficiency and maneuverability. Numerous attempts to create flying
vehicles of new type are made. A plenty of research laboratories and design
office participates in this work, huge financial resources are spent. Despite of
it, productivity of works is reduced more and more. Main reasons are: all
researches and develops, including attempts of create of flying vehicles of
new type, based on stationary aerodynamics and usual mechanics.
The classical aeromechanics is a principal cause constraining the further
improvements of efficiency of aircraft
Absolutely new opportunities can be opened
by using nonlinear
oscillatory aerodynamics [3,
6,
12 ]. Flying and swimming animals which
developed by this way have
reached efficiently and a maneuverability inaccessible modern aircraft. Many
attempts to use oscillatory movement to reach lifting force and draft are made.
Now in the USA works in several programs are conducted to create micro flying
vehicles (MAV). Among developments vehicles with oscillating wings start to be popular.
Even for Mars flight the decision was accepted, that the flying robot will have
oscillating wings. Despite of the big attention to creation of vehicles with
such wings, despite of greate financings of these projects, there is no confidence
in their future. The reasons are old. Because developers try to create vehicle
of new type basing on the old theory: on quasy-steady aerodynamics and usual
mechanics. There is an impression, that the enthusiasm and desire to create
flying vehicle of new type replace real knowledge of physical phenomena and ways
of their realization. Trying to develop on such low scientific level will lead
to many exotical devitalized or uneconomical vehicles. And business will end
with the crash as it occured with ornithopter.
It is necessary urgently to change a situation and to proceed supporting of
operations in this area on high level on the basis of nonlinear oscillatory
aerodynamics and reviewing of apparatus as uniform oscillating system. It is
difficult to make because nonlinear oscillatory aerodynamics is only in a stage
of origin and represented in hundreds bad-known papers. The situation is
complicated by that among designers and the managers there is no conception
of phenomena, which can be described only by nonlinear oscillatory aerodynamics.
Its fantastic possibilities are unknown, for example, the annihilation of an
aerodynamic drag, force by gradient energy, obtaining of thrust many times
greater, than is possible to receive it using the concepts of classical (stationary)
aerodynamics.
To create very effective flying vehicles of new type based on nonlinear
oscillatory aerodynamics
we have:
1. Knowledge of nonlinear oscillatory aerodynamics.
Kinematics of vortexes about a oscillating body
2. Programs of calculation thruster-engine complex of oscillatory type,
gear-agreeing elements.
3. Programs for kinematic, dynamic and power characteristics calculations for
oscillating wings.
4. Programs of calculation of a flow-around wave mode. The wing profile atlas (quasy-steady
and nonlinear aerodynamic mode).
5. The program of measurement and identification of dynamic and power
characteristics for oscillating wings.
6. The stands for aerodynamic characteristics of oscillating wings researches
in on place mode.
The aerodynamic test-bench for research of flapping big wings
The aerodynamic test-bench for research of flapping small wings
7. A complex of the equipment for measurements of
characteristics of oflapping wings.
Complex of the measuring equipment
8. Equipment for operating on characteristics of
flapping wings.
The block of management of kinematic characteristics of a of flapping wing
9. System of adaptive management of characteristics thruster.
We are looking for investors to create super effective flying vehicle of new
type.
We can develop and make the first working samples of flying vehicles for
various assignment. We have no ready-made samples. We have the big theoretical,
experimental and practical experience of development and production of working
samples of technical equipment using oscillations. We need investors well
knowing problems of flying vehicles, and professionally able to organize
business.
Our production and services:
1. To develop and make the first samples
Micro Air Vehicles ( MAV, UAV ) creating lift with the help
of
flapping.
2. To develop and make the first samples of flying vehicles with vertical
take-off and landing (VTOL) on creating lift with the help
of
flapping.
3. To develop and make the first sample of a
dirigible balloon creating
thrust and reducing aerodynamic drag of the case with the help of flapping.
4. To develop and make the first samples of the
air coshion vehicles
creating aerostatic and additional aerodynamic lift and force of thrust with the
help of oscillating.
5. Participation in your projects on decrease in aerodynamic drag of your vehicles with the help of creation of a wave flow.
6. Research and development of
alternative flying vehicles creating force
due to a gradient of energy.
7. Performance research, calculations and design works under your orders:
-Drawing up of the atlas of aerodynamic
characteristics of a flapping wing for a mode kwazi stationary oscillations;
- Drawing up of the
atlas of aerodynamic characteristics of a flapping wing for a mode nonlinear
oscillatory;
- Drawing up of the
atlas of aerodynamic characteristics of a wave flow (a fuselage, a
wing or other bodies) at kwazi a
stationary mode of a flow;
- Drawing up of the
atlas of aerodynamic characteristics of a wave flow (a fuselage, a
wing or other bodies) at a nonlinear mode of a flow;
- Calculation of aerodynamic characteristics for flying vehicles
(MAV, VTOL)
with flapping wings ;
- Development of a design of a oscillating
wing for flying vehicles (MAV, VTOL);
- Development of a design of tansmitting.-agreeing elements for the coordination of kinematic, dynamic and
power characteristics between the engine and aerodynamic loading of a wing;
- To develop and make system of
a drive for flapping wings;
- To develop and make of a control
system for flying vehicles (MAV,
VTOL) with flapping wings;
- To develop and make of system of
adaptive optimum control for flying
vehicles
(MAV, VTOL)
with flapping wings;
- Techniques and programs for experimental
researches;
- Reviews of scientific publications on
aerodynamics flapping wings;
- Reviews of designs of flying vehicles (MAV, VTOL)
with flapping wings;
- Reviews of patents of flying vehicles (MAV, VTOL)
with flapping wings.
