Information om | Engelska ordet SEMI-MONOCOQUE

Exempel på hur man kan använda SEMI-MONOCOQUE i en mening

• By contrast, a semi-monocoque is a hybrid combining a tensile stressed skin and a compressive structure made up of longerons and ribs or frames.
• The semi-monocoque wing has two main and one auxiliary spar and holds 4,500 kg (9,900 lb) of fuel, it has double-slotted fowler flaps and spoilers.
• Shear stresses within a semi-monocoque structure may be calculated by idealizing the cross-section of the structure into a set of stringers (carrying only axial loads) and webs (carrying only shear flows).
• The aircraft had a largely conventional semi-monocoque fuselage, with the engines in underwing nacelles.
• III biplane fighters featured semi-monocoque fuselages with load-bearing plywood skin panels glued to longitudinal longerons and bulkheads; it was replaced by the prevalent stressed skin structural configuration as metal replaced wood.
• The Firefly was a low-wing cantilever monoplane, featuring an oval-section metal semi-monocoque fuselage and a conventional tail unit with forward-placed tailplane.
• According to aviation author Philip Moyes, the decision to adopt the semi-monocoque fuselage was a significant advance in design; many Whitleys surviving severe damage on operations.
• Both single-seat, single-engine fighters used the same basic construction: all-metal alloys with semi-monocoque fuselages and three-spar wings, with alloy-framed, fabric-covered ailerons, elevators and rudders.
• The term semi-monocoque or semimonocoque refers to a stressed shell structure that is similar to a true monocoque, but which derives at least some of its strength from conventional reinforcement.
• The airframe had a semi-monocoque fuselage with bicycle-type landing gear, short cropped delta wings of 37° leading edge sweep, with 5° anhedral, attached to the fuselage in a mid position.
• The wings, fuselage, and empennage are manufactured using conventional semi-monocoque construction techniques, the primary structure being composed of aluminium; the central structure retains critical strength despite the cutout areas for the sliding doors of the main cabin.
• The fuselage is a semi-monocoque structure, with exterior skin sheets riveted to formers and longerons.
• The tail boom uses conventional semi-monocoque construction, supported by closely spaced notched channel-section frames and continuous stringers, absent of any major longitudinal sections or longerons.
• Derived from the He 70, furnished with an all-new semi-monocoque duralumin fuselage and powered by a total of four newly-developed Hirth HM 508C V8 inverted piston engines, the He 116 was designed specifically for this role, specifically the airline's route over the Pamir Mountains in Afghanistan.
• The fuselage is a semi-monocoque structure, with exterior skin sheets riveted to formers and longerons.
• Aft of the cockpit bulkhead, the ARV is conventionally built, with frames, longerons and a stressed skin forming a semi-monocoque.
• Greeves 250DCX Sportsman, with cast alloy "downtube", tubular steel rear subframe and semi-monocoque spine.
• The fuselage was semi-monocoque with a squared cross-section, having unswept wings and swept tailplanes.
• The I-3 had an oval-section semi-monocoque fuselage covered with 'shpon', molded birch plywood, with a small headrest faired into the fuselage, although the engine was enclosed in a metal cowling.
• The fuselage is composed of a prefabricated composite forward fuselage and a semi-monocoque aft fuselage, and features steeply reclined seating and a side-stick controller although modifications using a conventional stick have been made.

Förberedelsen av sidan tog: 301,16 ms.