Tuesday, 18 June 2013

Vickers Vanguard Turboprop Airliner

 

The Vickers Vanguard was a British short/medium-range turboprop
airliner introduced in 1959 by Vickers-Armstrongs, a development of
their successful Viscount design with considerably more internal room.
The Vanguard was introduced just before the first of the large
jet-powered airliners, and was largely ignored by the market. Only 44
were built, ordered by Trans-Canada Air Lines (TCA) and British
European Airways (BEA).

      After only about 10 years service TCA experimentally converted
one of theirs to a freighter configuration, calling it the Cargoliner.
This was considered successful, and in the early 1970s most were
converted to freighters, those from BEA becoming the Merchantman.
These freighters remained in service for many years, with the last one
(G-APEP) only retiring in 1996.
The very considerable success of the Vickers Viscount in airline
service was due to the smoothness, economy and reliability of its
turbine engines. In one enormous leap it had raised cruising speed
almost 100% by comparison with the piston-engined Vickers Viking; it
carried two or three times as many passengers (according to type) and
offered increased range. In early 1953, not long after the Viscount
entered service with British European Airways (BEA), discussions began
to initiate the design of a successor. Both BEA and Trans-Canada
Airlines were interested in a generally similar aircraft; compromise
in design to satisfy the views of these two operators resulted in the
low-wing configuration and 'double-bubble' fuselage to provide a large
underfloor cargo hold beneath the main cabin.

The power plant considered originally for inclusion in the design was
the Rolls-Royce Dart. But Rolls-Royce intimated that development of a
new engine, the RB.109, was then well under way and it (later known as
the Tyne) was chosen to power this new transport. Construction was
entirely conventional except for the wing, which introduced integrally
machined skins of light alloy to provide spanwise stiffening at low
cost, and three shear webs instead of the single spar in the Viscount
wing. When tied together by closely spaced ribs it produced a rigid
box structure and outboard of the centre-section it was sealed to form
integral fuel tanks.

First flight of the prototype Vanguard, as the new aircraft had been
named, was made on 20 January 1959. But because of the normal
development programme of a new civil airliner - coupled with delays
caused by problems with the new power plant - it was not until 1
February 1961 and 1 March 1961 that these aircraft began regular
service with Trans-Canada Airlines and BEA respectively. By then this
and other second-generation turboprop-powered airliners had been
deposed by the development and introduction into service of economical
turbojet-powered airliners such as the Boeing Model 707. Consequently
production ended after the original orders had been completed: 20 for
BEA and 23 for Trans-Canada Airlines.
On 10 October 1969 the first of nine freighter conversions of the
Vanguard, called Merchantman, was flown for BEA.


Contents:-

1. Design and development
2. Operational history
(a). Cargo operations
3. Accidents and Incidents
4. Specifications (Type 952)
5. Perfomance
6. DIMENSIONS
7. MODEL Type
8. PASSENGERS 97-139
9. WEIGHTS



1.Design and development:-

The aircraft was designed to a BEA requirement for a 100-seat aircraft
to replace their Viscounts. The original Type 870 design was then
modified when TCA expressed their interest in the design as well, and
Vickers returned the updated Type 950 that filled both requirements.
The main difference between the Viscount and Vanguard was the
construction of the fuselage. The Vanguard started with the original
Viscount fuselage, but cut it off about halfway up from the bottom,
replacing the top section with a larger-diameter fuselage to give it a
double bubble cross-section (similar to the Boeing Stratocruiser). The
result of the larger upper portion was a roomier interior, with
increased cargo capacity below the floor.
With this larger, and heavier, fuselage came the need for a new engine
to lift it. Rolls-Royce delivered their new Tyne design with a nominal
4,000 hp/3,000 kW (as compared to the Viscount's Dart of about 1,700
hp/1,300 kW). This allowed for a much higher service ceiling and
cruising speed; the Vanguard had a service ceiling almost twice that
of the Viscount. The Vanguard was one of the fastest turboprops ever
and was faster than the present day Saab 2000 or de Havilland Canada
Dash 8. A [probably hyped] pilot report describes maintaining 10,000
ft altitude with three engines feathered and the port outer at maximum
cruise power; weight at start of that flight was about 112,000 lb.
This is notably better performance than a Lockheed C-130, an aeroplane
of similar weight and power that could not (in its introductory
version of 1957) maintain a constant altitude on a single engine.
Nevertheless, the Vanguard was certainly overpowered.
The first Type 950 prototype G-AOYW flew on 20 January 1959. The
flight, a transfer to Wisley 3 miles away, had been planned for
December but the engines were returned to Rolls-Royce for minor work.
Proper flight testing was then carried out from Wisley.

2.Operational history:-

The Vanguard entered service with BEA and TCA in late 1960. BEA
operated their first Vanguard schedule on 17 December from Heathrow to
Paris. Following delivery of their full fleet of six V951 and 14 V953
aircraft by 30 March 1962, the type took over many of BEA's busier
European and UK trunk routes. The aircraft received names of famous
Royal Navy warships; the first G-APEA was named "Vanguard", but these
tended to be dropped later in service. Initial seating was 18
first-class at the rear and 108 tourist, but this was changed to 139
all-tourist, in which configuration, the Vanguard had very low
operating costs per seat/mile. On flights up to 300 mi (480 km), such
as from London to Paris, Brussels and Amsterdam, the type could match
the block times of the pure jets which were being introduced in the
early 1960s. The remaining BEA fleet passed to British Airways on 1
April 1974 and the last BA passenger flight with the type was on 16
June 1974.
TCA initiated Vanguard schedules on 1 February 1961 with two flights
from Toronto and Montreal via intermediate stops to Vancouver. The
fleet was also used on services from Toronto and Montreal to New York
and Nassau, Bahamas.

2.1.Cargo operations:-

In 1966, Air Canada removed all the seats in CF-TKK and refitted the
aircraft for pure cargo work, in which role it could carry 42,000 lb
(19,050 kg) of freight. Known by the airline as the "Cargoliner," it
was the only such conversion, but survived to be the last Canadian
Vanguard to be retired in December 1972.
BEA operated nine Vanguards modified to the V953C "Merchantman"
all-cargo layout from 1969, with the first two conversions being
designed and carried out by Aviation Traders Engineering Ltd (ATEL) at
Southend Airport. BEA modified the remainder at Heathrow using kits
from ATEL. A large forward cargo door (139 in/353 cm by 80 in/203 cm
high) was incorporated. The Merchantmen continued in service with BA
until late 1979 when the remaining five were sold.
Air Bridge Carriers purchased several of the Merchantmen and operated
them until 1992, when its changed to Hunting Cargo Airlines. Hunting
Cargo operated their last V953C flight on 30 September 1996 and
donated G-APEP to Brooklands Museum on 17 October 1996.

3.Accidents and Incidents:-

1.On 27 October 1965, British European Airways Vickers Vanguard G-APEE
flying from Edinburgh Airport to London Heathrow Airport, during a
landing in poor visibility, attempted an overshoot but crashed on
runway 28R. All on board died, six crew and 30 passengers.
2.On 2 October 1971, British European Airways Flight 706. operated by
Vickers Vanguard G-APEC crashed near Aarsele in Belgium. The cause was
the failure of the rear pressure bulkhead and subsequent destruction
of the tailplane. All eight crew and 55 passengers died.
3.On 10 April 1973, Invicta International Airlines Flight 435,
operated by Vickers Vanguard G-AXOP crashed near Basel-Mulhouse
Airport Switzerland. Four crew and 104 passengers died.
4.On 29 January 1988, Inter Cargo Service Flight 1004, operated by
Vickers Vanguard F-GEJF crashed on takeoff from Toulouse-Blagnac
Airport when takeoff was attempted with only three fully operable
engines.
5.On 6 February 1989, Inter Cargo Service Flight 3132, operated by
Vickers Vanguard F-GEJE crashed on takeoff from Marseille-Marignane
Airport, France. Three crew died; no passengers were carried.

4.Specifications (Type 952):-

General characteristics
Crew: 2-3
Capacity: 139 passengers
Length: 122 ft 10 in (37.50 m)
Wingspan: 118 ft 7 in (36.10 m)
Height: 34 ft 11 in (10.60 m)
Wing area: 1,527 ft² (142 m²)
Empty weight: 82,500 lb (37,421 kg)
Loaded weight: 141,000 lb (63,977 kg)
Powerplant: 4 × Rolls-Royce Tyne RTy.11 Mk 512 turboprop, 5,545 hp
(4,700 shp, 4,135 kW) each.


5.Performance:-

Maximum speed: 425 mph (684 km/h)
Range: 1,830 mi (2,945 km)
Service ceiling: 30,000 ft [15] (9,145 m)
Wing loading: 92 lb/ft² (450 kg/m²)
Power/mass: 0.16 hp/lb (0.26 kW/kg)
Cruise speed 684 km/h 425 mph
Ceiling 9145 m 30000 ft
Range w/max.payload 2945 km 1830 miles


6.DIMENSIONS:-

Wingspan 36.14 m 119 ft 7 in
Length 37.45 m 123 ft 10 in
Height 10.64 m 35 ft 11 in
Wing area 141.86 m2 1526.97 sq ft



7.MODEL Type:-

952 "Vanguard"
CREW 2-3

8.PASSENGERS 97-139

ENGINE 4 x Rolls-Royce Tyne RTy.11 Mk 512 turbo-prop, 4135kW

9.WEIGHTS

Take-off weight 63977 kg 141046 lb
Empty weight 37421 kg 82500 lb


BRITAIN'S NEW TURBOPROP AIRLINER:-

Now a few days' time the first Vickers Vanguard is to make its first
flight.The following pages bring Flight's readers up to date with the
engineering and economic facts about the aircraft. It will be seen
that the Vanguard promises to be a highly efficient tool of the air
transport trade. But good engineering and good economics are not the
only guarantees of acceptance, prerequisite though these two things
may be. The overall design-strategy must be right, otherwise efficient
economics and sound nuts-and-bolts—the "tactical" considerations—may
be academic. What, then, is the strategy behind the Vanguard? There
are five answers to this question. One, the Vanguard is the first
British airliner which can truly claim to possess the star quality of
built-in airline experience—the quality which has ensured Lockheed's
and Douglas's domination of world airline markets to date. The
Vanguard is not—as was the Viscount when it first appeared—just "a
good aeroplane." This is the two-dimensional view of an aeroplane's
suitability for airline use; the third dimension must be added from a
depth of airline operating designexperience. Vickers and Rolls-Royce,
with 350 Viscounts in service, are acknowledged to possess this
experience, and it has all been built into the Vanguard.
Two, the Vanguard sprang from the requirements of a most economically
intransigent kind of air transport—the field of
international short-to-medium stage operations. It can be said without
fear of dissent that a transport designed to master the economics of
intra-European routes is basically master of the denser
short-to-medium stage networks anywhere.Three, the choice of turboprop
propulsion permits the Vanguard to exploit with greater margins of
profit these economically difficult short-to-medium stages. (The
average intra-European sector distance is less than 300 miles.) Such
stages tend to be too short to permit full economic use to be made of
the jet's speed; yet the Vanguard—with a cruising speed of 425 m.p.h.
and above—can offer block speeds which are highly competitive with the
500-550 m.p.h. jets. Such routes are the realm of the Vanguard even in
idealized airtraffic-control conditions. In the practical conditions
of dayto-day operations, in which airliners have to cruise or hold as
they are told, the more fuel-thrifty Vanguard may be a decisive
advantage.Four, the size of the Vanguard is a realistic attempt to
provide a vehicle which can shift annually increasing traffic flows at
a lower specific cost. The Vanguard represents a
breakaway from the past tradition that short-haul airliners are small
and long-haul airliners are big. There is as great a, if not greater,
need on the shorter stages to handle growing traffic
volumes by increased aircraft-size rather than by operating smaller
airliners at increased frequencies. In this way the
Vanguard reduces the specific cost of operation, and fares can be
lowered to produce a "benevolent" generation of more
traffic and a further reduction of specific costs. This is an
important aspect of the Vanguard's strategy, and it is no doubt the
justification for Vickers' claim that the aircraft is capable of
cutting air fares by half. There is, of course, the present limitation
of a fixed fare for all types of aircraft; but there are strong signs
that the inevitable eventual differentiation of price between jets and
propellers will come sooner rather than later. When this happens, the
Vanguard's low-cost capabilities can be exploited to the full. Thus
not only can the aircraft be easily topped up with bulky freight
during off-peak passenger periods, but it can also be regarded as a
realistic answer to the need for positive development of freight.
Hitherto the cargo market has been largely developed by passenger
aircraft, and the Vanguard's design recognizes this fact. For
specialist airfreight operators, however, a full freighter
version—with a 40,000 lb payload—is offered. Five, the Vanguard
uniquely offers the operator a complete solution to one of his biggest
economic problems: the economic unbalance of seasonal-type traffic.
With but small penalties in speed and weight, very large underfloor
freight capacity is available—enough, it is claimed, to permit full
design payload to be carried with but one quarter of the seats filled.
These are the factors which should make the Vanguard not just a good aeroplane, but a good airline aeroplane.
























VisionAire Vantage Entry level Single Engine Corporate Jet

VisionAire Vantage Entry level Single Engine Corporate Jet

History:  
The innovative Vantage is an all new single engine entry level corporate jet, designed to compete against the CitationJet and TBM 700 turboprop.

Self flying businessman James O Rice Jr established VisionAire in St Louis in 1988 after deciding that there existed a significant market for a low cost entry level business jet. Design aims with the new jet include jet comfort and altitude, good short field performance, a large cabin and low acquisition and operating costs.

The Vantage was designed by VisionAire with the assistance of Scaled Composites (whose president is Burt Rutan), with the aircraft's definitive arrangement settled upon in 1993. In February 1996 VisionAire contracted Scaled Composites to design and build a proof of concept prototype, and this aircraft was rolled out from the latter's Mojave, California facility on November 8 1996.

This aircraft successfully flew for the first time on November 16 1996 and it was used to demonstrate performance and handling characteristics before a production configuration was settled upon. VisionAire now aims to achieve certification for the Vantage in 2000. Scaled Composites will build Vantage's wing and vertical and horizontal stabilisers at VisionAire's new Ames, Iowa production facility where final assembly will be undertaken. AAR of Florida has been contracted to build production forward and rear fuselages.

The Vantage's most notable feature is its single JT15D turbofan engine, which is buried in the rear fuselage and fed by two air inlets on either side of the fuselage. The JT15D has been in operation since 1982 on the Beechjet 400 and Citation V, and VisionAire says the proven in service engine would have a shutdown rate per aircraft of once every 250 to 500 years if flown 500 hours per annum. Other notable features include the mid fuselage mounted forward swept wing of relatively large area and graphite composite airframe. It will be certificated to FAR Part 23 Amendment 51.

Performance:  
Max cruising speed 648km/h (350kt), economical cruising speed 463km/h (250kt). Initial rate of climb 4000ft/min. Max certificated altitude 41,000ft. Range at max cruising speed 1857km (1002nm), at economical cruising speed 2870km (1550nm).
Weights  
Standard empty 1950kg (4300lb), max takeoff 3402kg (7500lb).

Dimensions:  
Wing span 14.49m (47ft 6in), production aircraft length 12.65m (41ft 6in). Wing area 20.6m2 (222.0sq ft).
Capacity
One pilot and passenger on flightdeck. Main cabin seats four in standard configuration in a club arrangement. Toilet and baggage compartment in rear of cabin.
Production  
At late 1998 VisionAire held orders for 150 Vantages. First two production aircraft due to be completed in early 1999, certification and first deliveries planned for 2000. Unit price approx $US1.8m.

                               The VisionAire Vantage is really a single engine aircraft produced in the U . s . States. VisionAire and Scaly Composites worked with on the style of the Vantage. The entry-level corporate jet includes a JT15D turbofan single engine and benefits four individuals the primary cabin. The flight deck benefits a couple, such as the pilot.

The Vantage, when empty, weighs in at 4,300pounds and also the maximum takeoff weight is 7,500 pounds. The organization jet provides a total cruising speed of 402 miles per hour as well as an economical cruising speed of 287 miles per hour. The entire licensed altitude is 41,000 ft. The first rate of climb is 4,000 ft each minute. The aircraft is 41 ft lengthy having a 47-feet wing span and 222-square-feet wing area.
VisionAire bought the intellectual property from Eviation about six months ago, although Rice says Eviation owner Matt Eller continues to have a small stake in the new venture. “We are sticking to a single-engine concept. There was nothing like it on the market when the programme was launched [in the 1990s] and there is no comparable aircraft – a single-engine jet with an entry-level size cabin – now,” he adds.
                                The Vantage will be built in Newton, North Carolina, where the company is planning to open a manufacturing facility by the middle of the year. “In the meantime, we are establishing strategic alliances with composite manufacturers to build the tooling for the Vantage,” Rice says. “Our aim is to fly the first of four conforming aircraft within 20 months, leading to certification and first deliveries in 2016,” Rice adds.
VisionAire has received a positive response from foreign investors and is close to securing a letter of intent for “a large sum of money”. “The interest in the programme has come from offshore in countries such as a China,” Rice says. “In the long term this country could be a big market for the Vantage and we may consider setting up an second assembly base to cater for this demand,” he adds























Monday, 17 June 2013

Weatherly 201/620 agricultural Aircraft

Type:  
Agricultural Aircraft

History:  

The Weatherly 201/620 agricultural Aircraft were built in relatively small numbers from the late 1960s.
The Weatherly 201 and its successors date back to the Weatherly WM-62C agricultural aircraft, 19 of which were built between January 1961 and late 1965. The WM-62s were agricultural conversions of the basic Fairchild M-62 airframe, fitted with a chemical hopper, spray booms and either a Wright W-670 or Pratt & Whitney R-985 radial engine.
Weatherly used its experience in designing and converting the WM-62s in developing its own agricultural aircraft design. The resulting Model 201 was a larger aircraft overall of conventional ag aircraft configuration, with a low wing, a Pratt & Whitney R-985 radial, integral chemical hopper and spray booms and an enclosed cockpit for the pilot. The initial production 201, the 201A, was certificated in 1967, followed by the 201B, and the improved 201C was granted its type certificate in 1975. A unique feature was the use of wingtip vanes which were developed to increase the effective swath width, while reducing the amount of chemicals lost from the spraying swath (they could be folded back beneath the wings for hangar storage.
                  The Model 620 replaced the 201C in production from 1980. The 620 featured a longer span wing with optional wingtip vanes and a larger chemical hopper, but the same R-985 engine. The 620A had a 65USgal fuel capacity, the 620B had a 4in stretched fuselage to give a 88USgal capacity.
The Pratt & Whitney Canada PT6A-11AG turboprop powered 620TP joined the 620 in production in 1980, and featured a longer nose and a slightly larger chemical hopper. This 620TP was available as the 620A-TP and 620B-TP.
The 620B-TP was replaced by the 620B-TG which is powered by a 496kW (665shp) Honeywell TPE331-1 turboprop. The 620B and 620B-TG are still in low-rate production.

Powerplants:  

201C - One 335kW (450hp) Pratt & Whitney R-985 nine cylinder radial piston engine driving a two blade constant speed Hartzell propeller. 
620 - Same except for a three blade constant speed prop. 
620TP - One 375kW (500shp) Pratt & Whitney Canada PT6A-11AG turboprop.

Performance:  

201C - Typical cruising speed 170km/h (91kt). Initial rate of climb 960ft/min.
620 - Endurance 2hr 30min. 
620TP - Endurance 2hr 0min.

Weights:  

201C - Empty 1157kg (2550lb), max takeoff restricted category 2177kg (4800lb). 
620 - Empty 1270kg (2800lb), max takeoff restricted category 2495kg (5500lb), design takeoff 1815kg (4000lb). 
620TP - Empty 1135kg (2500lb), max takeoff restricted category 2450kg (5400lb), design takeoff 1815kg (4000lb).

Dimensions:  

201C - Wing span 11.89m (39ft 0in), length 8.29m (27ft 3in), height 2.48m (8ft 2in). Wing area 23.3m2 (251.5sq ft). 
620 & 620TP - Wing span 12.50m (41ft 0in), or 14.33m (47ft 0in) with optional wingtip guide vanes.

Capacity:  

Pilot only in all models. 
Hopper capacity in 201C is 1022 litres (270US gal/225Imp gal); 
Hopper capacity in 620 is 1268 litres (335US gal/280Imp gal); 
Hopper capacity in 620TP is 1287 litres (340US gal/283Imp gal).

Production:  

The three model types were built in relatively small numbers (including more than 100 Model 201s). By mid 2000 at least 155 Model 620/620TPs had been built.