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Grahame-White Type VI military

Страна: Великобритания

Год: 1913

Grahame-White - School 'bus - 1913 - Великобритания<– –>Grahame-White - Type VII Popular - 1913 - Великобритания


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


Deleted by request of (c)Schiffer Publishing


P.Lewis British Aircraft 1809-1914 (Putnam)


Grahame-White Type 6

  J. D. North designed the Type 6 Military Biplane which was exhibited at the 1913 Olympia Aero Show. The tail was supported on three booms, the uppermost of which was used as a bearer for the propeller, with the control wires for the tail passing through the centre of the propeller boss. This arrangement originated with Horatio Barber. The 120 h.p. Austro-Daimler scheduled for the machine was not fitted at the Show, its place being taken by the 90 h.p. Austro-Daimler. This was mounted at the front of the deep nacelle, an extension shaft passing to the rear to drive the propeller by a chain. The Colt machine-gun in the nose had a 50° vertical and 180° horizontal field of fire. In addition to the pilot, two passengers were carried at the front of the nacelle and were accommodated on sprung seats over the tool boxes on each side of the engine. The controls were mounted on ball-bearings. Span, 42 ft. 6 ins. Length, 33 ft. 9 ins. Wing area, 440 sq. ft. Weight empty, 2,200 lb. Weight loaded, 2,950 lb. Maximum speed, 70 m.p.h. Landing speed, 50 m.p.h. Endurance, 6 hrs.


H.King Armament of British Aircraft (Putnam)


Grahame-White

1913 War Plane (Type 6). A Browning machine-gun on a British fighting aeroplane of 1913: this was but one blood-quickening feature of this pusher biplane, exhibited at Olympia early in the year mentioned. A second feature was the arrangement of the power plant to allow the free mounting of a gun. Thus The Aero:
  "The engine is coupled up to a long shaft mounted on ball bearings which extends back t o behind the pilot's seat, where it carries a chain sprocket driving the propeller through a twin roller chain. The propeller is mounted so that the upper longitudinal member of the triangular-section fuselage is taken through its hub, the principal reason for this being that with this design the arrangement of the fuselage is simplified, and the engine can be carried in front without introducing the necessity for the pilot and passengers to sit immediately in the slip stream of the screw."
  Almost as an afterthought there was appended to a lengthier description the simple observation:
  'The machine is shown equipped with a quick-firing gun'.
  Let it now be placed on record, after well over half a century, that this layout was schemed bv Horatio Barber; that the detail design was the work of John D. North, who was to adapt a Box Kite for a Lewis gun demonstration at Bisley in November of the same year (the War Plane never flew) and who in later years became a pre-eminent figure in aircraft armament development; and that the gun at Olympia, though correctly described by the commercial name Colt, was of the type called Browning Model of 1895 (or 'potato digger'). Like the later Lewis, this gun was air-cooled. The gun-pillar was associated with a quadrant fixed in a vertical plane under the gun. Elevation was said to be possible over an arc of 50 deg and traverse over 180 deg. The allusion to 'passengers', it may be noted, signified that an observer was carried in this aeroplane as well as a gunner.


Jane's All The World Aircraft 1913


GRAHAME-WHITE. The Grahame-White Aviation Co., Ltd., 166 Piccadilly, London, W. Works and Flying Ground: Hendon. Founded by C. Grahame-White, the well-known aviator, who in 1909 commenced operations with a school at Pau. Later this was removed to England, and a general agency for the sale of aeroplanes, etc., established. This developed, and early in 1911 the firm was handling a special British agency for the U.S. Burgess type known as "The Baby." The Hendon Aerodrome was acquired, and a factory established, which has grown continually ever since. In April, 1912, a monoplane to special design was completed. By the close of the same year biplanes of advanced design were constructed. Capacity of the works, March, 1913, was equal to 150 machines a year if necessary.

   | 1913. |1913. |1913. |1913 |1913.
   |Military |"Popular" |"Popular" |Tractor |Monoplane.
   |biplane. | biplane |biplane |hydro- |Type IX.
   |Type VI. |Type VII. |Type VII. |biplane | single-
   |2-seater |2-seater. |2-seater. |2-seater.| seat.
-----------------|-----------|-------------|-------------|---------|----------
Length...feet(m.)|33? (10.10)|20-5/6 (6.40)|26-5/6 (8.22)|25 (7.60)|21 (6.40)Span.....feet(m.}|42 (12.80)|29-1/6 (8.85)|38 (11.60)|42? (13) |32 (9.75)
Area..sq.ft.(m?.)|435 (40?) |230 (21) |475 (44) |380 (35) |208 (19)
Weight, total ...| | | | |
.......lbs.(kgs.)|2200 (997) | ... | ... |850 (385)| ... Weight, useful...| | | | |
.......lbs.(kgs.)| 750 (340) | ... | ... |450 (204)| ...
Motor | 120 Aust. | 50 Gnome | 50 Gnome |80 Gnome |50 Gnome
   | Daimler | | | |
Speed, max... | | | | |
...m.p.h (k.p.h.)|70 (110) |60 (95) |50 (80) |65 (105) |65 (105)
Speed, min... | | | | |
...m.p.h (k.p.h.)|55 (90) |50 (80) |40 (65) |50 (80) | ... Endurance....hrs.| 6 | 4 | 4 | 4 | 4
Number built | | | | |
   during 1912 | 1 | ... | ... | 1 | ...
-----------------|-----------|-------------|-----------------------|-----------
   |Also built | Also built | |Also built|Also built
   |with a 90 | with a 35 | |with a 60 |with a 35
   |Aust.Daimler.| Anzani. | |Anzani. |Anzani. Two
   |Designed to| | | |main floats
   |carry a gun| | | |with 12?
   |on the bow.| | | |ft. track.
   |Very good | | | |Floats are
   |view. Very | | | |15 ft.long,
   |strong | | | |2 ft. wide,
   |landing | | | |1 ft. 3 in.
   |carriage. | | | |deep.


Журнал Flight


Flight, February 8, 1913.

WHAT THERE WILL BE TO SEE AT OLYMPIA.

THE MACHINES.

The Grahame-White Aviation Co., Ltd.

  This progressive firm, the proprietors of the popular London Aerodrome at Hendon, will be showing two biplanes, one a land machine and the other designed for water flying. The first of these machines is equipped with a 90-h.p. Austro-Daimler motor which drives through a steel shaft and chains, a large diameter propeller arranged to the rear of the main planes so that the machine may be used for offensive tactics in war. The motor is mounted at the front of a streamline nacelle. The pilot, sitting behind it, is in a position that makes for maximum safety, should the machine for any reason suffer an unusually heavy landing. The main planes are of the extensioned type, the top plane being considerably longer in span than the lower. For the landing gear, it is exceptionally strong, and has the original feature that each of its two running wheels is flexibly mounted in a slot cut in each of the two unusually wide built-up skids. The tail is supported by an open triangular construction, the top member of which passes through the propeller boss. The second machine that the Grahame-White Co. will be showing will be a two-seater tractor hydro-biplane, driven by a 60-h.p. Anzani air-cooled motor. Its body will be somewhat reminiscent of Nieuport design, and it will be fitted with a pair of main floats of the long catamaran type. In addition, there will be exhibited on the stand various specimens of workmanship, such as a set of propellers, showing them in different stages of manufacture.


Flight, February 15, 1913.

GRAHAME WHITE AVIATION CO., LTD.

  Two notable biplanes figure on their stand, one a 90-h.p. military machine, and the other a hydro-biplane of a sporting type, driven by a 60-h. p. Anzani motor. Both bear evidence of much thought on the part of the designers, and of much painstaking care spent upon them in the constructing shops. The design of the first of these machines was due originally to Mr. H. Barber, but in its working out he was assisted by Mr. J. D. North, who also prepared the drawings for the hydro-biplane. Let us confine our attention for the moment to the military machine.

  The Grahame-White Military Biplane, as its title conveys, is a machine specially devised for military purposes, and particularly so that its occupants may be able to undertake offence tactics. So that the occupants may have a clear outlook in front of their respective cockpits, the propeller is arranged to the rear, while by using shaft drive the front engine position is retained, a disposition of the motor that is generally thought to be the best from the point of view of the passengers' safety. This machine was originally designed for a motor of 120 h.p., but it appears at the Show temporarily fitted with one of only 90 h.p. To illustrate its application as an aeroplane for attack purposes, a Colt quick-firing gun is mounted in the nose of the machine, and it has a range of 50° in a vertical plane, and 180° horizontally. It would, of course, be impossible for the gunner to make use of the gun's full extent of horizontal range - he would probably only be able to sight it through a deviation of 45° on either side of the longitudinal axis of the machine.
  The body of the biplane is essentially a lattice girder with ash longerons, and ash and spruce cross-members, ash being used for the latter members in the neighbourhood of the engine and propeller. That perfect rigidity may be assured, and this is doubly essential in the case of the body of this particular machine on account of its having a transmission shaft mounted inside it, it is double cross-braced with 10-gauge piano wire. In plan, the body is shaped to a careful streamline form, and it is an interesting point that the strut cross-sections are of the same shape, excepting that their curves are plotted to a shorter longitudinal axis. The Austro-Daimler motor is mounted on high ash bearers in front, and drives the propeller, a 10 ft. Chauviere, through shaft and chain transmission. The shaft is a large diameter steel tube turning in self-aligning ball-bearings, and the chain employed is a duplex Brampton. Fitted at the extreme nose of the body is a honeycomb radiator, specially made by the Austro-Daimler firm, and so shaped that it preserves the lines of the body. There is room on either side of the engine for a passenger to sit. They are provided with unusually comfortable spring seats, while under their feet are tool boxes. The pilot sits behind them and controls the machine by a vertical lever governing the elevation and wing warping, and by a pivoted foot lever which operates the rudder. To ensure sweet working, all the controls are carefully mounted on ball-bearings, and all the pulleys used to guide the control wires are turned from vanalium and fitted with ball-bearing centres. Below the pilot's feet is a large petrol tank sufficient for a 6-hours' flight. From that tank, petrol is fed under pressure, automatically provided by the engine exhaust, to a service tank in front, above the level of the engine. The pilot can at all times acquaint himself as to the state of his petrol supply by a specially devised gauge on his left.
  Plane construction. - The planes span respectively 42 ft. and 23 ft. and, having a chord measurement of 6 ft., they have a supporting area of 390 sq. ft. The cross-section employed is that of the Eiffel plane No. 8. The interior construction of the plane is particularly interesting. The front span is of generous dimensions, shaped from spruce. The rear span is a wide diameter steel tube. Over the spars are loosely fitted the ribs in such a manner that continual warping of the planes does not fatigue the structure. The ribs are built up of spruce webs and flanges, and where the spars are threaded through them they are thickened up to the full width of the flanges. To strengthen the planes against drift, they are cross-braced inside with 5/32 in. stranded cable, and so that the tension of the braces shall not cause the spars to pull together and so bind the ribs, they are separated by adjustable steel rods.
  The landing gear is composed of two built-up skids, each a little over a foot wide, in the centres of which are mounted the landing wheels. These latter organs each have two rims to the one wheel and are so designed to prevent the wheel from canting over sideways, which is, with a single tyre wheel, a very likely thing to happen with the method of suspension used. One of our sketches illustrates this point. The body of the machine is supported from the skids by 10 hollow spruce struts, the front two of which are taken straight to the engine bearers.
  The tail, consisting of a flat stabilizing surface 50 sq. ft. in area, two elevator flaps of a combined area of 25 sq. ft., and a vertical rudder of 20 sq. ft. surface, is stayed at the end of an open girder construction, built up of three steel tubular longerons and hollow spruce struts. The top member of this girder, as will be seen from our sketches, passes through the propeller boss.
  The Grahame-White military biplane weighs, without passengers or fuel, 2,103 lbs., and is designed to carry a useful load of 750 lbs. With her 120-h.p. engines fitted, she is expected to have a speed range of from 50 to 70 miles per hour.
<...>

M.Goodall, A.Tagg - British Aircraft before the Great War /Schiffer/
THE NEW 90-H.P. MILITARY GRAHAME-WHITE BIPLANE. - It will be seen that a quick-firing gun is mounted on the nose of the body. It can operate throughout a range of 50° vertically and 90° horizontally.
GW Type VI Military biplane was never used by the RFC.
P.Lewis - British Aircraft 1809-1914 /Putnam/
M.Goodall, A.Tagg - British Aircraft before the Great War /Schiffer/
P.Lewis - British Aircraft 1809-1914 /Putnam/
This photograph ot the 90-h.p. Grahame-White Type 6 military biplane gives a good idea of the intricacy of its internal construction. The finely-constructed framework showing the extension shaft from the engine to the propeller chain drive, and the upper tail-boom through which passed the tail-unit control wire.
Журнал - Flight за 1913 г.
The 90-h.p. Grahame White military biplane.
Jane's All The World Aircraft 1913 /Jane's/
Military Type VI. UAS.
Журнал - Flight за 1913 г.
The 90-h.p. Grahame-Whlte military biplane.
Журнал - Flight за 1913 г.
The propeller mounting of the 90-h.p. Grahame-White biplane. Notice the manner in which the control wires are taken through the top member of the tail outrigger construction which passes through the propeller boss.
Журнал - Flight за 1913 г.
The tail of the 90-h.p. Grahame-White military biplane.
Журнал - Flight за 1913 г.
Details of the landing chassis of the 90-h.p. Grahame-White biplane, showing how the double-tyred wheels are sprung in the wide built-up landing skids.
Журнал - Flight за 1913 г.
AT OLYMPIA. - A study in tail-skids.
Журнал - Flight за 1913 г.
A study in tails.