Avro Arrow-An Aviation Chapter In Canadian History pg2 |
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Drawing: DND
AVIONICS ARMAMENT EQUIPMENT ENGINE FUEL
The
Fuselage
The
aircraft was extensively "area ruled." This concept
involves aerodynamic shaping of the cross-sectional
area of the fuselage along its length, to reduce
drag to a minimum. Also called the "Coke bottle" design,
the fuselage is characteristically pinched at
the waist at the wing joint, although this was
not immediately noticeable on the Arrow.
Similarly, the cockpit was designed as an extension of the
fuselage rather than as a separate bubble, again for good aerodynamic performance.
The cockpit canopy itself was of unusual design, opening and closing in clam-shell
fashion due to its size and weight, as well as for case of entry and exit. The
canopy was made of a magnesium alloy with partly glazed glass. In back, drag
was reduced by trailing the canopy off into a spine running the length of the
aircraft to the tail, This also doubled as a conduit for controls and wire cabling.
In short, everything possible was done to reduce aerodynamic drag, including
the internal carriage of weapons.
The
Weapons Carriage
The
concept of internal weapons carriage has spawned
several misguided criticisms about an aircraft
that would destroy itself if the weapons package
were lowered during supersonic flight. In fact,
the weapons package was designed to be lowered
and removed only while on the ground. In this
way, a fully loaded package could be "snapped" into
place, considerably reducing the turnaround time
per aircraft. This concept also allowed easy
reconfiguration for other roles, including reconnaissance
and bomber. The pack was never designed to be
lowered in flight; since it was 16 feet long
and nine feet across, lowering in flight would
have been ludicrous. At no time were any of the
completed aircraft fitted with weapons.
Initially, the Arrow was to have carried the Hughes Falcon
guided missile. The Falcons were to be re- placed by Sparrow 2D missiles, with
a sophisticated weapons control system known as ASTRA. However, Avro engineers
judged the Sparrow missiles to be inferior for use in a high performance aircraft
without further development.
Each missile was to be mounted on its own hydraulically activated
retractable launching mechanism. Be- cause of their large fins, Sparrows would
sit partially within and partially outside the belly of the aircraft. (This is
similar to the manner in which missiles are carried on the Tornado aircraft:
they are recessed into the underbelly; however, no retractable launcher is required.)
The smaller Falcon missiles would have been fully internal to the aircraft. Missiles
would extend from their own individual bay doors. Aft missiles would be fired
first, followed by forward missiles.(2) A sliding
bay' door arrangement was being considered for the Sparrows. Door opening or
closing was to have been completed in 0.35 seconds; extension was to have taken
another 1.25 seconds or less.
It has been argued that no other fighter has duplicated this
internal weapons carriage. This is simply not the case. The CF-101 Voodoo aircraft,
for example, employed a rotating platform, which carried some of the weapons
internally and the remainder externally. The F-106 Delta Dart used an almost
identical internal missile system to that of the Arrow. Internal weapons carriage
may also become the future norm.
As calculated by Avro engineers, externally mounting four missiles
could have increased drag by some 20% at Mach 1.5. Bill Gunston (3)
states that the move towards faster, more agile fighters is slowly forcing the
removal of externally mounted weapons in order to take every advantage of the
resulting reduced drag. He states it will simply no longer be good enough to
hang missiles on pylons. One solution is to use the recessed method of missile
carriage and the other is to place weapons in an internal bay.
A recent article (4) describes
stealth design techniques to reduce radar cross-sectional (RCS) area. These include
using aerodynamic shapes such as delta wings, blending cockpit and wings into
the fuselage and, of course, carrying weapons internally. Aerodynamic and stealth
efficiency appear to be complementary design requirements. The Arrow was not
a stealth aircraft, but obviously the concept of a "clean" aircraft could have
several inherent advantages.
Setting
the Record Straight: The Designer's View
Margaret
McCaffery
|
" I
feel for the youngsters. In our day you could
get on with the job and not worry about going
over the precipice." Those hardly sound like
the words of a man who has known overwhelming
disappointment in "getting on with the job," yet
they capture the spirit of the man who designed
the C-102 jetliner-which the New York press
claimed "licks anything of ours" -was vice-president
of engineering for Avro Aircraft when it
was building the CF-105 (Avro Arrow), and
ended up consulting on production of the
Anglo- French Concorde.
James C. Floyd, P.Eng., epitomizes the cheery "mustn't grumble" attitude
of his native Manchester, yet he's a proud Canadian, who retired to this country
after spending 20 years working in Britain following cancellation of the Arrow
and the crumbling of A.V. Roe Canada. His concern for "the youngsters" has led
him on a concerted campaign to set the history books straight if possible, and
if not, well, he's written one of his own.(1) He is currently helping to set
up the Canadian Aerospace Heritage Foundation which aims to build a full-scale
replica of the Arrow and other Canadian aircraft for permanent
exhibit.
What does someone who was responsible for the design
of the Avro Arrow think about the criticisms of its abilities? Jim Floyd and
other Avro engineers have expressed themselves eloquently to the publishers of
Professor Morton's books, but he sees this kind of misinformation as part of
a larger picture:
"High technology is, by its very nature, difficult for the
layman or voter to adequately assess, and its worth and impact can only be fully
appreciated, even by those who have to ensure its survival, if it is properly
and compre- hensively presented. In the past, Canadian engineers have tended
to adopt a low profile in the political arena and have rarely been consulted
about the long-term effects of the decisions made by the 'captains of industry'
or their political counterparts. As an example, I firmly believe that had Mr.
Howe been exposed to a proper and full-scale engineering briefing on the Jetliner
project, he would not have made the utterly erroneous statements about the alleged
technical shortcomings of the aircraft, which must have influenced his decision
to abandon the project and which later caused him considerable embarrassment,
even within his own party."'
Although he refers to himself (with a twinkle in his eye) as "just
a poor engineer" who doesn't know anything about politics, he was embroiled in
the Cold War politics of the late 1950s by his involvement with the Arrow. In
this interview with Engineering Dimensions' editor Margaret McCaffery,
he relives those days at Malton.
ED.. Why do you think Diefenbaker
cancelled the Arrow?
Floyd: Diefenbaker had
the worst advice possible. His main
advice came from General Pearkes,
who was a brave old soldier, but
he didn't know anything about airplanes
at all. He'd been hoodwinked by a
visit to the States where he was
told that airplanes are out and missiles
are in and there'll never be another
manned airplane bought by any air
force.
ED: Was it on the strength
of that advice alone that Diefenbaker
acted?
Floyd: Oh no. It was such
a complex picture, it was like a
tree: even the leaves had something
to do with it dying. There were four
major reasons: 1 Diefenbaker could
see the costs of the Arrow rising.
It isn't unusual for the costs on
high technology to be going up all
the time; one of the prime examples
would be the Concorde, which by the
time it flew cost more than double
what it had been estimated at. The
Arrow was going the same sort of
way.
2 General Pearkes had said we can only justify this sort of a
cost if we could sell it to the Yanks or the Brits. So he went
out, completely prematurely, because you never sell an aircraft
to a foreign government before you've de- veloped it yourself,
and of course he came back with a no.
3 Then there's this memorandum Paul Campagna brought back from
Washington (see p. 51). It's obvious that the Americans had virtually
insisted on the cancellation of the Arrow |
as part
of this deal, long before Diefenbaker came
out and said that the Arrow was can- celled.
That's a new one to me.
4
Then the Americans were cutting down on their development
of manned airplanes. Although they'd put out a
specification for the F-108, which was a very highly
supersonic airplane, probably as near to the Arrow
as you can get, they'd cancelled it, because they
weren't too sure that manned aircraft would be
needed. The British government had put out a White
Paper saying that they didn't foresee that there'd
be any fighter aircraft designed from that point
on. So I really don't blame Diefenbaker for
his uneasiness looking at the program. I would
blame him, though, for the way he accomplished
the cancellation.
ED: Did you suspect that
the program was going to be cancelled?
Floyd: We suspected that there'd be some hiccup. In September
1958, we were told that the whole thing would be reviewed in March, so of course
we were on tenterhooks. But the appraisal was done on February 20 and the can-
cellation came the same day. That was the biggest shock of the century. We were
in a board meeting with John Plant (president of Avro Aircraft) trying to settle
some very mundane union situation about seniority Joe Morley (sales and service
manager) came running down the corridor with a man from the DDP (Department of
Defence Production) saying they'd heard on the radio that Diefenbaker had cancelled
the Arrow.
ED. So you heard about
it at the same time as the general
public?
Floyd: Later than the
general public--- they heard
it on the radio.
ED: It sounds like the
government had a gun to its head.
Floyd: We were told to
close everything down and that nothing
would be paid as from that day. My
first thought was to see if any of
our other projects could be got into
shape so I could keep my 1,500 engineers.
I'd been pleading for years to get
another project going at the same
time as the Arrow, but Fred Smye
(general manager), who was a most
sincere man, felt we had a duty to
do the best we could on that airplane.
ED: I still find it very
difficult to understand why it was
ordered scrapped, especially when
today we're all talking about technology
transfer, joint ventures, etc.
Floyd: You're in very
good company, The first thing that
I did was to get on to the RAE (Royal
Aircraft Establishment) in
the UK to see if they'd be interested
in taking some of these airplanes
and they said of course, provided
we could back them up with parts.
Well, we had 31 aircraft back through
the plant in different stages of
production, so we had plenty of parts.
We'd even worked out a method of
transportation over the northern
route and then the order to scrap
came down. (This was mid-April 1959.
Floyd had been ordered to scrap the
Jetliner, his admitted favourite
project, on November 23, 1956. Three
years later, after setting up another
first class design tearn at Hawker-Siddely,
UK, where he led the feasibility
study on the Concorde, Jim Floyd
experienced the disappointment of
seeing the design study for Concorde
go to Bristol Aviation Corporation.
Saying he didn't want to see another
aircraft, he quit and took his family
on vacation. On his return, his first
call was from the minister in charge
of the Concorde asking him to consult
on the project. That one flew!)
ED: What message would
you have for today's engineers?
Floyd: The best things
I've learned have been about dealing
with people to bring out the best
in them. The old things I learned
in England I rebelled against. I
try to coax people rather than beat
them over the head. Canadians are
very flexible: treat them the right
way and you can get anything out
of them.
One of the things I'm trying to do with the Canadian Aerospace
Heritage Foundation is to help young people get the incentive to do some of the
things we tried to do. Today there seems to be an apathy, a sense of too many
things in the way. I'd like to give the kids some hope.
Reference
1. Floyd, J. The Avro Canada C-102 Jetliner, Erin:
Boston Mills Press, 1986. |
Photo: J.C. FLOYD, P.Eng.
Avro
Arrow design team, left to right. Bob
Lindley, chief engineer; Jim Floyd, vice president, engineering;
Guest Hake,
Arrow project engineer, and Jim Chamberlin, chief,
technical design.
The
Landing Gear
The
requirement for such a large weapons bay necessitated
stowage of the main landing gear in the thin
delta wings. This caused a number of engineering
difficulties, overcome by Dowty Engineering Limited.
On retraction, the main gear would be shortened,
angled forward and then twisted in order to be
accommodated Given the 30-ton weight of the aircraft
and resulting 200,000-ib compressive load on
the main gear on landing, ultra-high-tensile
steel with an ultimate tensile strength of 260,000-280,000
psi was required. Use of aluminum was obviously
precluded, as was the use of butt and gas welding
techniques. Instead, large forgings were made,
using a die process. For example, the main outer
leg was the largest forging, weighing 1,000 lb.
After machining this would be reduced to 167
lb. Solutions to the problem put Dowty and Avro
engineers at the forefront of metallurgical research.
Likewise, the engineers at Jarry Hydraulics were obtaining
patents for their steering mechanism in the nose gear arrangement, among others.
In fact, Avro engineers and their subcontractors made enormous strides
in developing high temperature alloys, high pressure and high temperature systems,
fuel technol- ogy for supersonic flight and human engineering, in terms of cockpit
layout and design. These techniques pushed the world aircraft industry further
ahead. In support of these advances, Avro maintained a huge metal-to-metal autoclave,
a special heat treat furnace, a giant skin mill and a 15,000-ton rubber pad forming
press (then the largest in the world).
Fly-by-wire
Early
in the design, it was decided that some form of
power assist would be required to help control
and fly the aircraft during supersonic flight.
The chosen result was fly-by-wire. In conventional
systems, the pilot's stick and rudder controls
are mechanically linked via steel cables or rods
to valves which control high pressure
fluid flow to the actuators. These powerful hydraulic
actuators, in turn, operate the aircraft's control
surfaces, such as elevators and ailerons. In military
aircraft, automatic flight control systems, gyroscopes
and position sensors are also mechanically linked
to the actuators through the control rods.
In the Arrow automatic flight control system (AFCS), in automatic
mode, the pilot's stick and position- ing sensors were linked electrically to
electro-hydraulic actuators. Hence, stability, command and control were effected
almost instantaneously in all three axes. Analogue computers with a mix of vacuum
tube and transistor technology were used, together with autostabilization of
the tail fin and artificial feel, to give the pilot some sense of force on his
control stick.
Not until the 1970s did fighter planes use a similar AFCS,
although variations had been employed in experimental aircraft and the SR 71
Blackbird. The F-16 and Panavia Tornado both used analogue fly-by-wire.The first
fighter to replace the analogue system with digital electronics was the F/A-18
Hornet.
How effective was the Arrow fly-by-wire automatic flight control
system? According to test pilot Spud Potocki, in a 60-degree climb, with full
afterburner, he would shut down one engine and experience no expected sideslip
or roll. The AFCS would compensate instantaneously. Automatic approaches and
takeoffs were also successfully completed. The Arrow was the most modern interceptor
in the world, clearly over 20 years ahead of its time.
Continued
on Page 3>>
CONVERTED TO HTML, AND
HYPERLINKS ADDED, JANUARY 22, 2001.
Scott McArthur.
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