Informasjon om | Engelsk ordet INTERPLANE

Eksempler på bruk av INTERPLANE i en setning

• The departing cowling damaged his top wing, along with the lower left interplane strut, but Greim managed to land the machine successfully.
• It had elliptical wings and great care had been taken to reduce drag, with the number of interplane struts and bracing wires minimised.
• On 13 December 1935, another Holyman DH86, Lepina, forced-landed on Hunter Island off northern Tasmania with the lower port interplane strut having "vibrated loose".
• The lower wing was in two parts and mounted on the lower fuselage, braced to the upper wing with a pair of outward-leaning, parallel interplane struts made of profiled steel tubes.
• It was a single bay biplane braced with outward-leaning N-form interplane struts, with the upper plane held a little above the upper fuselage by cabane struts.
• Both the interplane and trailing-edge ailerons on these early aircraft did not use a hand or foot-operated mechanism to operate them, but very much like the earlier Santos-Dumont 14-bis had adopted in November 1906, required the pilot to "lean-into" the turn to operate the ailerons — on the Curtiss pushers, a transverse-rocking, metal framework "shoulder cradle", hinged longitudinally on either side of the pilot's seat - initially as straight metal tubes resting against the pilot's upper arms; and later achieved with "armrests" in a similar location; achieved the connection between the pilot and aileron control cabling.
• The "unrotated projectiles" (UPs) were Le Prieur rockets mounted on the interplane struts of Nieuport fighters.
• 51 shared its basic configuration with his other aircraft of the period, being a biplane with a swept upper wing and unswept lower wing, joined by I-shaped interplane struts.
• Further successful flights were made on 22 February, after which the rear stabilisers were removed and the ailerons repositioned, now being placed on short outriggers trailing from the forward interplane struts, and the front rudder was moved to a position above the elevator.
• The wing cellule was derived from the Model E landplane and was of two-bay, unstaggered, equal-span construction with large ailerons mounted on the interplane struts and extending past the span of the wings themselves.
• The continuous inmost interplane struts were replaced by short struts between the lower longerons and the lower wing and a cabane consisting of two sets of inverted V struts supplemented by a single strut between the centre of the upper wing and the nose of the aircraft.
• The design was a conventional biplane flying boat with equal-span unstaggered wings and two engines mounted in a single nacelle in tractor-pusher configuration on struts in the interplane gap.
• 73 was an inverted sesquiplane with a biplane tail, a rigid central section, and powered by a pair of engines mounted in a push-pull configuration within a common nacelle that was mounted on struts in the interplane gap above the fuselage.
• The CK-2 was a biplane with single-bay biplane that utilized a Fokker scheme of N-shaped interplane struts and metal cabane.
• They differed from the earlier design in having shorter fuselages, more severely staggered wings, and I-struts for both the interplane and cabane bracing, where the W.
• The wings did not fold, but two people could dismantle both sets in about two minutes, first unclipping the bottom of the interplane strut, folding it and unhooking the centre section from the cabane for each upper wing in turn.
• A demountable upper wing, attached by N form interplane struts and several cabane struts and of markedly smaller span and deep central chord allowed the IIIA to be flown either as monoplane or biplane.
• Four booms ran rearwards from the wings, two on each side converging in the vertical plane from the inner interplane struts to the tail, with rectangular bracing to stiffen them.
• To convert to a biplane (strictly a sesquiplane) the lower wings were attached to the fuselage at the base of the lift struts and supported by the original, unusual, integral asymmetric X interplane struts from the Mayfly, running out and down from the top of the lift struts at about 45DEG to meet their own wing well outboard.
• In 1920, Marchetti redesigned the MVT, giving it wings of longer span and splayed interplane bracing struts, a new cabane structure, and a more powerful engine, the SPA 62a rated at 234 kilowatts (285 horsepower).

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