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THE GREEN EAGLE

09/24/08 3:52 PM

#37749 RE: stockdiety #37748

nice:)

stockdiety

09/24/08 4:38 PM

#37750 RE: stockdiety #37748

another project anthony brown was a part of....
NRC in vortex chase

By Rob Coppinger in London

A modified Canadair CT-133 research aircraft will next month collect wake-vortex-flow field data to help develop wake-detection systems. It follows a flight earlier this year behind airliners cruising in Canadian airspace.

In May the Canadian National Research Council Institute for Aerospace Research’s (NRC Research) CT-133 (a Canadian version of the two-seat Lockheed T-33 trainer) flew six trial-instrumentation development and calibration flights, and one wake-vortex flight over the St Lawrence Seaway. That flight between Quebec City and Toronto was behind three aircraft that were cruising en route – an Airbus A310, A319 and a Boeing 767-300.


© National Research Council

Wakes up to 11nm long were recorded


During the flights the CT-133 collected air and inertial data 600 times every second, high sampling rates that NRC Research claims are research firsts. “Our goal is to obtain data on the flow phenomena to clarify the risk and highlight the desirability, or the need, to develop wake-vortex turbulence warning instrumentation that can be installed on aircraft,” says NRC Aerospace research officer and test pilot Anthony Brown.

The work follows a 2004 study with a modified research Dassault Falcon 20 that flew behind aircraft cruising at 24,000-39,000ft (7,500-12,000m) with separation distances of 1-30nm (2-56km), and experienced wakes that were 7-11nm long.


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stockdiety

09/24/08 4:41 PM

#37751 RE: stockdiety #37748

another anthony brown project...the list is numerous..i just want tthe board to see he is the real deal...


Diamond DJet Flight Test Envelope Expansion
Following the initial flight test series in late April, Diamond's D-Jet resumed flight testing after installation of its data acquisition system and minor planned modifications to the inlet engine fairings.

In a series of flight tests conducted from June 26th through June 30th, the speed and altitude envelope was progressively expanded from the previously flown 170 kts and 12,000'. The latest flight, flown by pilots Christian Dries and Anthony Brown, on June 30th, expanded the cruise speed to 280+ ktas and altitude to the design certification limit of 25,000'.


"We are very pleased to have expanded the envelope in such a short time. The aircraft is a joy to fly, smooth, very stable and with all systems functioning perfectly," said CEO Christian Dries. "The aircraft is doing everything we are expecting of it. The more time I spend in it, the more I am convinced that the aircraft will be an absolute sensation. The blend of exceptional comfort with real world performance is sure to appeal to many current piston pilots, as well as established turboprop and light jet owners."

Diamond is preparing the flight test aircraft and full fuselage and interior mock-up for display at DiamondFest on July 15th/16th and EAA Airventure 2006 one week later.

The D-JET is a 5 place luxury personal jet, powered by the FADEC controlled Williams FJ33 turbine and equipped with Garmin all glass flight deck and autopilot.

Diamond offers the most comprehensive range of modern GA aircraft, including the 2 place DA20, the 4 place single DA40 DiamondStar, the twin engine DA42 TwinStar and now the ultimate personal aircraft, the D-JET.

For further information on Original Release

stockdiety

09/24/08 10:14 PM

#37753 RE: stockdiety #37748

anthony brown has been called upon by many companies to bring his expetise and knowledge to their aid...he beleives the integrity will not only fly,handle well,but most importantly...be certifiable...attached is another example of what he has done..
The dangers of turbulence
behind en route commercial
aircraft could be better
understood and thereby
limited, following new
research by Canada’s
National Research Council
Institute for Aerospace
Research (NRC Aerospace).
NRC Aerospace (Hall 4,
C17a) has installed and
tested new instrumentation
on its Canadair CT-133
aircraft that will enable it to
gather extremely detailed
information on the effects
of turbulence generated by
commercial aircraft.
Aircraft travelling
through wake vortices can
experience substantial aerodynamic
loading and flight
path upsets, possibly
causing injuries to passengers
and structural overload.
Armed with its new air
data acquisition system,
which can collect 600
samples of inertial and air
data a second, the CT-133
performed six calibration
Light relief from
Rockwell Collins
Rockwell Collins (Hall 4,
Stand F10) is showcasing
its CISS-2100
Configurable Integrated
Surveillance System,
which combines weather
detection, traffic alert
and collision avoidance,
Mode S surveillance and
terrain awareness and
warning functions into
a single system.
It also features
Rockwell Collins’
MultiScan Hazard
Detection System, which
provides fully automatic
weather hazard detection
up to 320nm,
ground clutter suppression,
and enhanced
turbulence detection
capabilities.
The CISS-2100 uses
40% fewer parts than
traditional aircraft
surveillance systems,
reducing the weight,
volume and power
consumption.
Eaton’s low-cost
fluid sensor
A new oil indicator
sensor that determines
oil fluid levels in intermediate,
tail rotor and
main gearboxes has been
developed by Eaton
Aerospace (Hall 4, F12).
The retrofit item
works with existing
aircraft wiring interfaced
with a remote
indicator at the
cockpit caution panel
to detect the presence
of oil.
This also eliminates
additional wiring and
space requirements and
minimises upgrade
costs.
Thales upgrades
Merlin sonar
Thales UK (Hall 3, C5)
has been awarded a £27
million contract by
Lockheed Martin to
upgrade the acoustics
(sonar) system of the
Merlin multi-mission
helicopter.
The award covers the
upgrade of 30 helicopter
systems with options for
eight further systems in
the future.
The upgrade, together
with a Sonobuoy
command and receiver
system, will give the
aircraft enhanced
performance, especially in
shallow water environments.
The upgrades will be
undertaken by Thales
UK’s underwater systems
Anti Submarine Warfare
(ASW) Airborne group in
Stockport, England, and
supported by airborne
group elements in Brest,
France.
Canadian research logs wake vortex data
flights in May, followed by
a wake vortex flight behind
three commercial aircraft –
an Airbus A310, A319 and
Boeing 767-300.
Later this summer, NRC
Aerospace will refine the
instrumentation and undertake
further data gathering
flights.
The study follows one
conducted by NRC
Aerospace in 2004, using a
Dassault Falcon 20 and less
sophisticated instrumentation.
Anthony Brown, NRC
Aerospace research officer
and test pilot, says: “We
gathered data at 600Hz,
which is 600 samples per
second. To our knowledge,
this is the first atmospheric
research aircraft to do so at
that high a rate. It gave us
an immediate impression of
the wake vortex flow field
that we just didn’t observe
when we gathered data at
32Hz using the Falcon. As a
result, we feel that this is a
good platform to obtain
detailed information on
wake vortex flow fields.
“Our goal is to obtain data
on the flow phenomena to
clarify the risk and highlight
the desirability or the need
to develop wake vortex
turbulence warning instrumentation
that can be
installed on aircraft.”

stockdiety

09/27/08 10:24 PM

#37782 RE: stockdiety #37748

hope all read this post to see the truth behind the viaility of the integrity ...

Son of Jr

09/28/08 1:16 AM

#37789 RE: stockdiety #37748

Thanks for informing us about the unemployed test pilot and for proving that the Integrity can not be certified.
See below:
------------------------------------------------------------

ED Decision 2003/14/RM
Final
14/11/2003
European Aviation Safety Agency
DECISION NO. 2003/14 /RM
OF THE EXECUTIVE DIRECTOR OF THE AGENCY
of 14 November 2003
on certification specifications, including airworthiness codes and acceptable means of
compliance for normal, utility, aerobatic and commuter category aeroplanes (« CS-23 »)

CS 23.1 Applicability
(a) This airworthiness code is applicable to –
(1) Aeroplanes in the normal, utility and
aerobatic categories that have a seating
configuration, excluding the pilot seat(s), of nine
or fewer and a maximum certificated take-off
weight of 5670 kg (12 500 lb) or less; and

(2) Propeller-driven twin-engined
aeroplanes in the commuter category that have a
seating configuration, excluding the pilot seat(s),
of nineteen or fewer and a maximum certificated
take-off weight of 8618 kg (19 000 lb) or less.
---------------------------------------------------------

Intergrity does not meet either category for applicablility!!
Sorry, your case and test pilot just went down in flames. Thanks for giving us the proof we need to write this one off.