VEHICULE VOLANT DE TRANSPORT INDIVIDUEL "AVIOCAR"

AVIO-CAR-PTFV

Abrégé anglais

Aviocar or PTFV is a Personal Transport Flying Vehicle that is
capable of driving on the road like any other sport utility vehicle
and fly for a sit distance between two major points like any other
small executive jet without using any airport facilities. Aviocar is
designed to be driven in a city powered by light weight electrical
hybrid (mix) engine and in the air powered by two small size jet
engines. The aviocar is a "transformer" vehicle in SUV shaped
body with added features such as retractable wings, fin, stabilizers
and retractable jet engines in such designed aerodynamically to be
capable of flying for medium range distance between cities. It
must be no more than 8" feet wide and 30" feet long over all to be
practical. The frame is made of very light weight material, but
strong enough to withstand side and frontal impact, hard landing
and the weight of the load.
The Aviocar meets all of the above criteria by using an enhanced
normal car shaped body designed aerodynamically to maximize the
lift ability of said vehicle. The Aviocar utilizes a novel
aerodynamic design that can function at a high angle of attack to
optimize low speed lift while still presenting minimal resistance to
airflow at high speeds. Moreover, the design features allow it to
function in the roadway as a car and in the air as a craft.

Revendications

Claims: The embodiments of the invention the "Avio-car-PTFV" in which an
exclusive
of property or privilege is claimed are defined as follows:


1. Avio-car-PTFV is An automobile that is capable of driving on the road in
SUV
shape body powered by electric hybrid(mix) engine designed aerodynamically to
ease and
withstand the wind on the ground when drive switch is been selected.
2. A method according to claim 1: Avio-car-PTFV wherein a trajectory system
that puts
pressure on the front-end using airflow which in-turn the faster the car goes
the more it
will have airflow pushing it to hold all wheels on the ground supported by
double
wishbone independent suspension, rack-pinion steering thus configured for
legal road
travel.
3. A method according to claim 1: Avio-car-PTFV on the ground powered by
combination lithium-ion batteries system, hybrid(mix) electrical engine which
limits top
speed to just over 95mph, maximum power output is 195bhp and the car can be
recharged
in just one hour from any "but not limited to" main electricity outlet using
the onboard
charger device.
4. A method according to claim3: Recharging the combination lithium-ion
batteries
system via connecting section module to the two jet-engine during flight thus
minimizing
recharging on the ground.
5. Avio-car-PTFV is An automobile that is drivable on the road-way and
designed
aerodynamically to fly with added feature such as retractable wings, vertical
stabilizer,
horizontal stabilizer and powered by two small size retractable jet engines in
which
enables Avio-car-PTFV to transform to a flying car that enable it to function
aerodynamically in the air for a sit distance between two pre-defined points.
6. A method according to claim5: Avio-car-PTFV wherein a mechanical design to
retract the end portion of the wing (B'C=3) inside the main body of the
wing(AB=5)~
process according to claim5 ~ the retractable wing becomes shorter than it
designed for
flight ~ by measurement (AB=AB'=AC=8)-(BC=B'C=3)=(AB=AB'= 5) in
measurement equal to (AQ).
7. A method according to claim6: Avio-car-PTFV wherein the mechanism in which
the
top end portion of the wing (B'C) (right wing) or (B1'C1)(left wing) ~
retracts with semi-
circle mechanism in the centre of the wing(A ~ F) attached to the tip of the
wing by a
chain from inside guided by hydraulic stick made of light weight material
8. A method according to claim5: Avio-car-PTFV wherein the mechanism in which
~
(AB - B'C) of the wing retracts underneath the frame of Avio-car (AF-Q)(right
wing) ~
(A1F1-Q1)(left wing) by semi-circular motorized hydraulic arm mechanism ~ in
uniform synchronization process in respect with claim7 thus synchronizing the
movement
of the whole wing.
9. A method according to claim5: Avio-car-PTFV wherein the mechanism in which
to
retract the horizontal stabilizer down in vertical position parallel to the
vertical stabilizer
by L shaped mechanism as illustrated in the drawing p5 that moves like an arm
thus
locking the horizontal stabilizer vertically thus enabling the tail-end to be
retracted in-
ward to the back of the automobile
10. A method according to claim9: Avio-car-PTFV wherein the mechanism in which
the
horizontal stabilizer and vertical stabilizer ~ process according to one of
the preceding



claims had indicted ~ a cylinder shape device with curved section in a loop
path
connecting to the base of the tail-end section works like a joint.
11. A method according to claim 10: Avio-car-PTFV wherein the mechanism in
which an
egg shaped device attached to the cylinder shaped device by a chain and
antenna like
stick.
12. A method according to claim 11: Avio-car-PTFV wherein the mechanism in
which
the egg shaped device work in only clock or counter-clock way in a uniform
synchronization with the horizontal stabilizer in a vertical position parallel
with the
vertical stabilizer.
13. A method according to claim 11: Avio-car-PTFV wherein the mechanism in
which
the antenna like stick works like a sensor in synchronization with the
preceding claims
moving forward or back-ward.
14. A method according to claim5: Avio-car-PTFV wherein the mechanism in which
a
sensor synchronizes the movement of the two jet engines in an in-ward or out-
ward
position using the L shaped mechanism process according to the preceding
claim9.
15. A method according to claim5: Avio-car-PTFV wherein the pre-defined
destination is
by computed human machine inter-face devise that is programmed to execute all
the
process according to all the preceding claims in a trajectory synchronization
method thus
triggering all the sensors to activate in the command that requested (driving
or flying)~
in-turn detecting all abnormalities and if the command requested is viable to
initiate ~
weather condition ~ fuel on board in relation to the destination chosen for
flight.

Description

CA 02572448 2006-12-28

Subject-matter of the invention: It's a personal transport vehicle that is
capable of flying
between to major point like; Ottawa - Toronto and can stop in between if the
facilities are
available.

Specification:
Aviocar or PTFV is a Personal Transport Flying Vehicle that is capable of
driving on the road
like any other sport utility vehicle and fly for a sit distance between two
major points like any
other small executive jet without using any airport facilities.

Aviocar-PTFV is designed as road able car or SUV that has normal air
resistance which keeps it
on the ground up to the speed limit in which it has been designed to go and
the maximum wind to
withstand. Over all aerodynamic shape it's beneficiary for Aviocar on the road
and in the air.
Aviocar is designed to be driven in a city powered by light weight electrical
hybrid (mix) engine
and on the air powered by two small size jet engines.

The frame is made of very light weight material, but strong enough to
withstand side and frontal
impact, hard landing and the weight of the load.

Which is made of Carbon fiber with ultra-lightweight, high-tech design and by
placing the
engine behind the cockpit to achieve a weight distribution that makes the car
extremely
aerodynamic in the air and stable on the road?

RANG AND USE OF AVIOCAR:

The maximum rang for Aviocar in the air is about 500 miles at cruising speed
between (180 to
315 miles/hr) at an altitude of (1500 to 5000 feet). During flight this
vehicle is designed to be
flown by pr-programmed computer that will decide the altitude base on
destination choosing...
exp: (Ottawa to Toronto it will go up to 5000 feet in a speed of 180 to 315
miles/hr).
The computer program will give options on a touch-on screen to chose your
destination from pr-
set destination that has been calculated from the runway you are standing on,
by using GPS built
in the car and two homing devices that is built in both end of the runway or
manually by trained
pilot, to be flown between two major points with option to stop in between ...
Exp: (from Ottawa
to Toronto you will have an option to stop in two major point if chosen it
before take-off).
The flight will be in controlled airspace in straight line with minimal
maneuver, parallel to major
highway, like taking a trip from one major city to another major city but
instead of driving on the
highway you will be flying over the highway.
Landing will be in a small runway between (900 to 1500 feet) built parallel to
the highway at the
edge of the city.
After landing it will take the vehicle few minutes to go back to a normal car
configuration
allowing it to be driven on the highway and on a city street with the traffic.
Aviocar will not require to use any airport facilities or to contact any air
traffic controller, unless
the highway passes by an airport and the vehicle is in an emergency stress.
The vehicle will be


CA 02572448 2006-12-28

equipped with transponders making it visible to the radar and air Data
Computers, flight
Directors, and autopilot which will be controlling each leg of the trip.

Aviocar-PTFV usefulness comes in so many ways. A trip between two major cities
that will
normally take fife hours will be cut to a quarter of the time, without the
need to go through
airports and lost of bags and time.
Aviocar will be useful to executives who would like to be in two places in
short times, and since
Aviocar uses triangle system like for example if you are leaving Ottawa on the
touch-on screen
you will have the option to go to Toronto or Montreal within Canada. Another
example; the east
cost of the U.S from Main to Virginia, you will have the option of choosing in
any set of three
Exp: (Boston, Newark and Baltimore)

WINGS
RETRACTABLE WINGS:

The wings will be retractable in two positions:

1) 1/4 inch of the end portion of the wing wil I retract inside the main body
of the wing. This makes
the wing shorter than during flight.
2) The length of the wing will be the same length between the front and back
wheel. That design
features allow the wing to be retracted inside the body of the Aviocar. This
keeps the wings
stored in safe area away from the outside aliment during driving.

RETRACTABLE STABILIZER AND FIN:

The back of the Aviocar is egg shaped for aerodynamic design presenting
minimal resistance
during flight and storage facilities for the fin and the stabilizer during
driving. Retracting the
stabilizer and the fin will be in two steps:

1) the stabilizer will come downward in down right position to the fin and
lineup with the rudder.
2) Than the fin attached with the stabilizer elevator and rudder will retract
inward to the back of
the Aviocar, this mechanism puts the whole tail of the aviocar underneath the
back of the two
passenger seats.

Boundaries of patent: Retractable wings, retractable stabilizer and fin,
retractable engines and
the martial the body is composed of and over all aerodynamic shape.