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The Tipsy B was a small sports two-seat monoplane designed by E.O.Tips, and built in both Belgium and the UK. A total of 42 was built, and a few are still flying. ==Design and development== Avions Fairey, the Fairey Aviation Company's Belgian subsidiary, was set up in 1930-1 to produce Fairey Fox and Firefly aircraft for the Belgian Air Force. Once production of the military aircraft was under way, its manager Ernest Oscar Tips found the time to design and build light aircraft of his own, first the single-seat Tipsy S and S.2 in 1935, then the two-seat Tipsy B. Although the latter was larger, the two aircraft types had much in common; both were single-engined low wing cantilever monoplanes, with wings that carried strong taper on their trailing edges. In detail, though, the planforms of the two aircraft were different. Both were built in Belgium by Avions Fairey and in the UK under licence. The Tipsy B was a wooden framed machine, covered with a mixture of plywood and canvas. The wing was built around an I-section main spar at about one quarter chord and an auxiliary rear box spar. These spars were linked by a rigid diagonal pyramid bracing. Stressed plywood skin was used from the main spar forward, with the rest of the wing fabric covered over wooden ribs. The leading edge was almost straight, and the trailing edge straight but strongly forward swept except at the centre section. Differential ailerons were carried on the tapering section, so their hinge line was also strongly forward swept.〔 The fuselage was based on four spruce longerons, flat sided and plywood covered apart from a rounded decking. The depth of the decking behind the cockpit depended on whether the seating was open or closed.〔 The Tipsy B had an open cockpit, with almost side-by-side seating in the sense that the seats were slightly staggered fore and aft to minimise fuselage width, with the left hand seat 8 in (200 mm) further forward.〔 The Tipsy Bc had the same seat arrangement, but enclosed under a Rhodoid (cellulose acetate) canopy, faired into the fuselage rearwards by a much deeper decking.〔 Some Tipsy Bs had an asymmetric windscreen formed out of a single Rhodoid sheet, with its free edge further forward on the left to match the displaced seating,〔 but symmetric screens became common. Both seats were equipped with controls.〔 The control column was on the mid-line between the seats, with a horizontal extension that could be rotated over either position.〔(''General Aviation'' December 2008 p 40 )〕 A 60 hp (45 kW) Walter Mikron four cylinder inverted in-line engine drove a two-bladed propeller.〔 At the rear the fin was almost triangular, and built as an integral part of the fuselage.〔 The fabric covered rudder was rounded, and moved between the separate elevators, which with the tail plane formed an elliptical shape.〔 As a result, the elevator hinges, like those of the ailerons were strongly forward swept.〔 The tailplane was supported from the fin near the rudder post with a pair of external struts. There was a long tailskid. The main undercarriage had two cantilever forks with rubber-in-compression springing, its legs faired and the wheels spatted.〔 On 8 May 1937, the Tipsy B first flew from the Avions Fairey factory airfield at Gosselies, near Charleroi, with A.J.Eyskens at the controls.〔(Tipsy B )〕 A week later, the Tipsy was being demonstrated in the UK at Great West Aerodrome.〔 On 5 June 1937, the Tipsy Light Aircraft Company of London Air Park, Hanworth was established to build the Tipsy B under licence. In total, twenty-four Tipsy B and Bc aircraft were built at Avions Fairey before the invasion of Belgium by Germany in World War II. About eight had open cockpits (Tipsy B) and the rest were enclosed (Tipsy Bc).〔 The Tipsy seems to have been mostly nice to fly but, as with other aircraft with pointed wing tips, its low speed behaviour could be unforgiving, dropping a wing at the stall without much warning. During the British production run, some of these issues were addressed.〔 The fourth British aircraft was the first to be modified. To improve the stalling behaviour, it had a strengthened wing with washout at the tips, so that this part of the wing should not stall first, and camber-changing flaps were added to the straight centre section to delay the stall. To meet British airworthiness concerns about control surface flutter, all were mass-balanced. The rudder balance was external, projecting from its leading edge just above the tip of the fin. The elevator was also revised to a single unit with a straight hinge and trailing edge, and the bottom of the rudder slightly cropped to allow it to move. Subsequent British Tipsys included these changes, and from the sixth aircraft onwards also featured fixed letter box slots. In August 1938, during the Certificate of Airworthiness tests at Martlesham Heath, there were concerns about rudder authority, so Tipsy Light Aircraft added 18% to the rudder area, leading to successful certification. At that point, the name of the aircraft changed from Tipsy B to Tipsy Trainer. The ninth aircraft was approved at an increased all up-weight of 1,200 lb (544 kg), and from then on the name was revised to Tipsy Trainer 1.〔 In all, Tipsy Light Aircraft built eighteen aircraft, all with open cockpits. The last three were completed after the war, the final example first flying in April 1948.〔Jackson's list of British register aircraft does not include ''VT-AKQ'' (c/n 7), that went straight onto the Indian register〕 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Tipsy B」の詳細全文を読む スポンサード リンク
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