M.Goodall, A.Tagg British Aircraft before the Great War (Schiffer)

P.Lewis British Aircraft 1809-1914 (Putnam)

Bristol Prier Monoplanes

   Among the top-ranking pilots of all nationalities attracted to the "Bristol" living-schools at Brooklands and Larkhill was Mons. Pierre Prier. During 1911, the Filton factory built his P.I single-seat monoplane for training at their schools, of which Prier was appointed chief flying instructor.
   The Prier Monoplane represented a considerable advance in design and comfort over the Boxkite then in use, and possessed a far better performance on the same 50 h.p. Gnome rotary engine. The first P.I built was works number 46, and two further examples, 56 and 57, were intended to participate in the 1911 Circuit of Britain. All, however, were converted for school flying and had their Gnome engines replaced by 35 h.p. three-cylinder Anzanis. Number 56 was powered temporarily with a 40 h.p. Isaacson radial, thus turning it into an all-British machine to enable James Valentine to fly it in the contest for the 1911 British Michelin Cup No. 2. Another proposed power plant was the flat-twin 40 h.p. Clement-Bayard, but this installation was abandoned before completion.
   Mons. Prier's monoplane was of straightforward construction with a wooden airframe covered with fabric. Warping was used on the wings, and the tail unit comprised rudder and one-piece elevators without a fixed fin or a tailplane. Metal cowling panels were fitted to the nose as far to the rear as the cockpit area, and the curved hooks on the front of the undercarriage skids were sprung to absorb shocks. A further eleven examples, works numbers 58, 71, 72, 73, 74, 75, 76, 83, 84, 90 and 94, were built as tandem two-seaters with 50 h.p. Gnome engines. Number 75 was bought by the War Office, and several of the batch went to Italy and Spain. Number 73 was fitted with aerials mounted above the fuselage and took part in wireless experiments at Hendon in 1912.
   In collaboration with Captain Bertram Dickson, Prier redesigned the two-seater with a longer fuselage and a fixed tailplane. Eight of the new version were built, works numbers 82, 85, 87, 89, 91, 130, 155 and 156, with 91 going to the War Office as Army aircraft 261. The machines used the 50 h.p. Gnome as power, but two further examples, works numbers 86 and 88, were constructed for Turkey. They were the same as 82, but were given the extra power of the 70 h.p. Gnome. No. 75 was later rebuilt to the same standard as No. 91 and became Army aircraft 256.
   A pair of Prier School single-seaters, numbers 95 and 96, based on 57 and equipped with the 35 h.p. Anzani, were supplied to Italy. Three additional single-seat Prier School monoplanes, works numbers 97, 98 and 102, with 35 h.p. Anzanis and otherwise the same as numbers 95 and 96 except that they had fixed tailplanes, were delivered to the school at Larkhill. At the 1911 Paris Aero Show a Bristol Prier monoplane was the sole representative from the United Kingdom.
   The final variant of the Prier monoplane design was the Sociable side-by-side two-seater, of which three were produced in 1913 for export to Germany. Designed by Prier and Dickson and based on number 82, they were given works numbers 107, 108 and 109 and used the 50 h.p. Gnome.
   Although the Prier monoplanes were used successfully at the constructor's flying-schools and also abroad, they were not adopted by the War Office owing to the prevailing prejudice against the supposedly weak monoplane brought about by several accidents at that time. Thirty-three Prier monoplanes of all types were constructed.

SPECIFICATION

   Description: Single- or two-seat tractor training monoplane. Wooden structure, fabric covered.
   Manufacturers: The British and Colonial Aeroplane Co. Ltd., Filton, Bristol.
   Power Plant: 50 h.p. Gnome, 35 h.p. Anzani, 70 h.p. Gnome, 40 h.p. Isaacson, 40 h.p. Clement-Bayard.
   Dimensions: Span (Standard), 30 ft. 2 ins.; (Military), 34 ft. Length, 24 ft. 6 ins. Height, 9 ft. 9 ins. Wing area (Standard), 166 sq. ft.; (Military), 200 sq. ft.
   Weights: Empty, 640 lb. Loaded, 1,080 lb.
   Performance: Maximum speed, 68 m.p.h.

J.Herris Halberstadt Aircraft of WWI. Volume 1: A-types to C.III (A Centennial Perspective on Great War Airplanes 44)

Halberstadt Bristol Coanda

  The Halberstadt Coanda was a license-built version of the Bristol Coanda trainer. It was a two-seat monoplane powered by an 80 hp Gnome rotary. Some modifications, such as a modified tail, side by side seating, and an extended fuselage were made. Halberstadt built a few examples,- work numbers 2 and 27 are known. Two examples bought in Britain had military serials A.21/12 and A.27/12.

Журнал Flight

Flight, September 30, 1911.

THE BRISTOL MONOPLANE.

   As more rumour than fact has generally formed the basis of current aerodrome discussion of the merits of the new Bristol monoplane, the accompanying illustrations and description of its construction may prove of exceptional interest. The machine, itself, is undoubtedly the centre of many thoughts, but its comparative inaccessibility on Salisbury Plain does not contribute much to the general fixing of ideas as to its leading characteristics.
   To those who follow the trend of aeroplane design and are sufficiently au fait with events to know that Pierre Prier - one time Bleriot pupil, now one of the best of modern pilots - is now associated with the British and Colonial Company, it will come as no surprise to learn that a good deal of the credit for this model is due to him. Indeed, the machine itself is in some respects not unlike his old Bleriot mount, although needless to say it shows marked originality at many points, more particularly in respect to the tail planes and under-carriage. In the former, a fan-shaped surface is pivoted about a horizontal axis to perform the double duty of stabiliser and elevator, thereby departing from the common practice of using a hinged extension to a fixed plane.
   The main body is constructed on the usual box girder principle, with the important differences that strainers are altogether dispensed with, and that the longitudinal members are not pierced except by small wooden screws that serve to keep in position the steel plates to which the cross-bracing wires are attached.
   At the forward end of the body is mounted the 50-h.p. Gnome engine, with its direct driven 8 ft. 6 in. Normale propeller. There is no support between the engine and propeller, a feature that renders the motor extremely accessible for tuning or cleaning purposes.
   While the front engine bearer follows customary design, the rear support is quite original, for, in place of the usual pressed steel mounting, the Gnome crank-shaft is anchored in position by four adjustable steel rods, arranged diagonally, in tension. An aluminium dome above the engine prevents any oil reaching the pilot.
   The landing carriage is of the skid and wheel variety, the common axle between the two wheels being flexibly attached to the skids by rubber shock-absorbers. Very little wire bracing is resorted to in the under-carriage as rigidity is given to the structure by diagonal struts.
   Projecting in front are two short upturned skids, which pivot about horizontal bolts against the action of strong steel compression springs. The idea is sound besides being original, for should a landing be made at too steep an angle these skids will give upwards and ease the descent. Rigid skids of this type are unsatisfactory in that they have the habit of digging into the ground and snapping off short under such conditions. The wings, which have a slight dihedral angle, are of notably strong construction.
   The front and rear spars are fashioned from steel tubing of circular section cored with wood.
   Three trusses of substantial stranded steel cable attached to the front spar of each wing take the weight of the machine in flight. Tne two outer "haubans" are connected to a fitting on the undercarriage skids, and the inner one is attached to a clip round the bottom main body "longeron." Both the camber and the angle of incidence of the wings are exceptionally slight, and to these features must be attributed the fine turn of speed that the Bristol monoplane exhibits. A pyramid of oval-section steel tubing supports the weight of the wings, the warp-compensating wire from the rear spar passing through tubes brazed in a fining provided at its apex.
   The fan-shaped elevating-surface is balanced, in order that its operation should call for little exertion on the part of the pilot. Steering laterally is effected by a balanced vertical rudder mounted at the rear extremity of the main body. The tail unit is protected from contact with the ground by a double skid of rattan cane.
   Control, in the three dimensions of elevation, lateral balance, and direction, is maintained by the usual universally-jointed vertical lever and pivoted foot bar, which is employed by almost every monoplane descended from the paternal Bleriot. All wires leading to the controlling organs are fitted in duplicate, thereby reducing to a minimum the risk of mechanical failure in the air. The pilot is kept well acquainted with the condition of his fuel supply by a petrol gauge fitted to a small dashboard before him, and a revolution indicator by its side tells him his engine speed.
   As soon as the Bristol single-seater emerges from its trial stage, and its construction upon standardised lines is embarked upon, the British and Colonial Aeroplane Co. propose to carry out experiments with a passenger-carrying monoplane of similar design. Such a machine should be most valuable for military reconnaissance work, both on-account of the wide range of view that is obtained from the pilot's seat, and also because of the exceptional speed that it is hoped, and with good reason, such a machine would attain.


Flight, December 23, 1911.

A British Aeroplane Over Paris.

   To Mr. James Valentine belongs the proud distinction of having been the first Britisher to look down on Paris from an aeroplane. On Thursday of last week he started up from Issy on the Bristol two-seater monoplane, and circling the Eiffel Tower, crossed the Seine and the Place de la Concorde to Notre Dame. After circling the dome, he continued on to Vincennes, and afterwards flew back to Issy.


The Bristol Monoplane in Paris.

   THE only British machine on exhibition at the Grand Palais is the Bristol monoplane, and naturally President Fallieres, on the opening day, paid a visit to the British and Colonial Aeroplane Co.'s stand, where, after admiring the machine, he accepted from Mr. Stanley White a magnificent album bound in vellum, and suitably decorated, containing views of the works and flying school of the Company. In view of Mr. Valentine's flight over the French capital on the British monoplane, the stand on which it is exhibited has proved a centre of attraction, while the design and construction of the machine have evoked favourable comments on all sides.


Flight, December 30, 1911.

PARIS AERO SHOW.

British and Colonial Aeroplane Co.

   OCCUPYING one of the central stands in the Salon was the Bristol two-seater monoplane, a thoroughly worthy example of British enterprise, design and workmanship. As far as excellence of finish was concerned, although there were many machines in the show which were perfection in this respect, none could be said to be superior to the Bristol. In its main features the machine presents little difference from the monoplane described in these pages some few weeks since, although naturally being a passenger-carrying machine, it is somewhat larger all round. Passenger and pilot are seated in tandem, the passenger being seated approximately over the centre of pressure. The landing carriage is a greatly improved A-type wheel and skid construction, possessing natural advantages of strength, simplicity, and neatness. A great improvement that the Bristol Company have effected in this type of landing-gear is the extension in a backward direction of the skids. These extensions are in length some 3 ft., and are composed of several super-imposed strips of wood, forming in effect a laminated spring. They take the place of a tail-skid, and serve to rapidly bring the machine to rest after a landing has been made. One interesting little detail that the writer noticed, one that is typical of Bristol thoroughness, was the self-locking screw-on hub caps of the landing-wheels, which have replaced the much less mechanical method of attaching such organs by means of washers and split-pins. Mounted at the front of the fuselage is the power unit, a Gnome engine of 50 h.p. driving a Bristol propeller, the former being fed by Zenith carburettor, a practice which is steadily coming into favour in France. Surrounding the passenger are quite a number of useful accessories to help him in his observation work. There is a map roller, compass, thermos flask, field glasses, and a small writing tablet. The seats themselves are attached in a very interesting manner, they being supported from the main framework by steel wires in tension, a feature which allows them to be adjusted for the personal convenience of the occupants, and ensures safety against bodily damage that might be caused by broken splinters in case of a smash. At the Salon considerable interest was manifested in the machine, which had become widely known because of its flight over Paris, with Valentine at the lever, on the Thursday preceding the opening.

Principal dimensions, &c.
Length 23 ft.
Span 34 ft.
Area 200 sq. ft.
Weight 650 lbs.
Speed 65 m.p.h.
Motor 50-h.p. Gnome.
Price L950


Flight, April 20, 1912.

Brooklands to Salisbury on Bristol Monoplane.

   MR. C. H. PIXTON has shown himself as clever a pilot of a monoplane as he is of a two-decker machine, and his flight from Brooklands to Salisbury on Friday of last week still further emphasizes his capabilities as a cross-country flyer. Leaving Brooklands at 5.30 on a Bristol two-seater monoplane, and accompanied by a pupil, Mr. Lane, he set off in the direction of Salisbury, taking his course by the railway line. He arrived at Salisbury at half past six and the distance covered in the hour was a little over sixty miles, the railway being a little further than going straight. Mr. Pixton who was somewhat impeded by a cross wind, maintained an altitude of about 3,000 ft. during his flight.


Flight, May 25, 1912.

MODELS.

Messrs. Rolfe Bros. Models.

   We give this week two illustrations of models made by the above firm. The makers state that the Bristol-type model has made over 100 flights. Also that the other model illustrated is the identical machine which won the Flight Golf Competition in a gale at Coventry last July, and that it has flown in all weathers (rain, hail and snow). Also that the propellers (distinctive type) of bentwood have not in any way lost their shape - a fact which the makers attribute to the special method of making them.