اصطلاحات بخش های اصلی هواپیما (انگلیسی)

صفحه 1:
بسم الثه الرحمن الرحيم 

صفحه 2:
MAIN ELEMENTS IN AIRCRAFT 5 ‏لوو انم‎ 5 Control > Wings Landing gear Engine mount Nacelle Stabilizers 

صفحه 3:
350 

صفحه 4:
Airplane Fuselage Description Main structure (or body) of the aircraft Wings and tail units are attached it Houses the crew, passengers, cargo, and power plant. ‘Multi-engine aircraft, the power plants mounted on nacelles. 4 

صفحه 5:
Major Airplane Componen Nacelles are separate units that are similar in design and to the fuselage. attached to the wing structure or fuselage. constructi Nacelles soo 

صفحه 6:
Airplane Engine Mounts — Attach power plant to the aircraft single-engine aircraft, they are ‘mounted on the front end or nose of the fuselage.multi-engine tached to or incorporated into the nacelle sngine aircraft, are incorporated into the Ps 1 attached to the fuselage on the sides of the fuselage. ithe back of the aircraft. 

صفحه 7:
Airplane Componeniges Wings constitute the main lifting surface of the aircraft while in flight and are designated as right and left. The right and left sides of an aircraft are relative to the right- and left-hand sides, ‘respectively, of the ated in the cockpits ۳ ۵۵٩ 

صفحه 8:
Major Airplane Components Stabilizers (or tail surfaces) are airfoils whose primary purpose Is. to increase aircraft ity. They are mounted at the rear end of the fuselage and consist of the fin oF fins and the horizontal stabilizer. 

صفحه 9:


صفحه 10:
‘The structures of most flight vehicles are thin walled structures (shells) که ۵عزاموه کاعاعع8* 00 ‎wing structure)‏ عمقطة امهم لمعه عطا كع لآبر0رم» (00)؟ كأمع امم عطا كه ]0م مع ممم انرمع ۵0۵9 29۵ عواوصه ا ل 5و cad Definitions 

صفحه 11:


صفحه 12:


صفحه 13:
‘A critical load-bearing structure on an. aircraft. Ifthis structure Is severely damaged, the aircraft cannot fly. Structural elements mainly to provide ‘enhanced jerodynamics. Fairings, for instance, are found where the wing meets the body or at various locations on the leading or trailing edge af the wing. a Airplane 

صفحه 14:
Major Airplane Components 7 reacts the applied torsion and shear forces transmits aerodynamic forces to the longitudinal and transverse Supporting members acts with the longitudinal members in resisting the applied bending and axial loads acts with the ‘members in reacting the hoop, or circumferential 2 hen the structure is pressurized. 14 

صفحه 15:
Major Airplane Components stringers 5 ‘resist bending and axial loads along with the skin ‘divide the skin into small panels and thereby increase its buckling and failing stresses ‘act with the skin in resisting axial loads caused by essurization. كد 01 

صفحه 16:


صفحه 17:


صفحه 18:
Major Airplane Components ‎ee Asis is a form of construction in which a number‏ ره ‎‘of members are joined to form a rigid structure. Many‏ ‎arly aircraft used the Pratt truss, in which, wooden‏ ‎ongerons served as the main longitudinal structural‏ ‎mb ‏05 مد 

صفحه 19:
Major Airplane Components — ay _ Monocoque structures; Unstiffened shells. must be relatively thick to resist bending, compressive, and torsional loads.Does not use formers, frame assemblies, or bulkheads to give shape to the fuselageThe biggest challenge: maintaining enough strength while keeping within allowable limits, ۳ ۵ ‏ری‎ ‎ight within 1 1 

صفحه 20:
Major Airplane Components cot hE EU Ge, to diffuse concentrated loads into the cover. ‘More efficient type of construction that permits much thinner covering shel 

صفحه 21:
25 

صفحه 22:


صفحه 23:
200 Major Airplane Components Structural integration of the wing and fuselage *Keep the wing in its aerodynamic profile 

صفحه 24:
Major Airplane Components resist bending and axial loads form the wing box for stable torsion resistance ol > OG 

صفحه 25:
Airplane Components Structure & Fuel Volume Front Spar & Rear spar (Wing box) is usually ‘Tank ‘The Space Betw: Displacement of Fi 25 

صفحه 26:
Major Airplane Component: angle booms Those skin {All spanwise bending loads reacted by substantial booms or ی 2 0 

صفحه 27:
«9 

صفحه 28:
front rear Skat ack spt Pg dap vane 7 dap 5 spar layout Airbus A319 2 Oo 

صفحه 29:
Airplane Components Fixed landing gear Fixed landing gear is attached to the airframe so that it Is held in 

صفحه 30:
۳ Control surface 

صفحه 31:
200 

صفحه 32:


صفحه 33:
<: 

صفحه 34:
Landing Gear 

صفحه 35:
Major Airplane Components Itis Landing Gear Not Takeoff Gear! 3 To 5 Percent of Aircraft Weight 

صفحه 36:
Major Airplane Components Retractable landing gear is carried partially or completely inside the airframe structure to reduce drag. When necessary for landing, the gear is extended by some mechanism. The gear is Into the airfr takeoff 25 

صفحه 37:
Retractable landing ge ناك — lof 7 Oo 

صفحه 38:
Major Airplane Components 2 “Quadra cycle. “inline Skids. 01 «5 

صفحه 39:
Major Airplane Components 

صفحه 40:
Major Airplane Components Centerline landing gear is often found on aircraft such as sailplanes and gliders. This configuration has one main landing wheel mounted on the centerline of the fuselage and near the center of gravity of the aircraft. Small auxiliary wheels or skids foeated on the nose, tall, and wing tps of these type 

صفحه 41:
Major Airplane Components Quadracycle landing gear normally consists of two nose wheels and two main wheels. This configuration Is found on some helicopters and on most float-equipped aircraft that incorporate retractable wheels in the float design ago 

صفحه 42:
Major Airplane Components Tricycle layout preferable in vast majority of cases Interference with sensitive electronic payloads (SAR Radar, etc ) force using retractable landing gears 2d 

صفحه 43:
Major Airplane Components ‘Skid-type landing gear is usually reserved for use on helicopters ‘as the normally take off and land vertically and do not require a landing or take-off run. ۰ 

صفحه 44:
1 landing gear 

صفحه 45:


صفحه 46:
Airplane Components Tail Dragger Constant AOA (4-5 Degree) {ow cost Pilot visibility is Zero 46 

صفحه 47:
Major Airplane Components ‘Takeoff Rotation Problem ‘Same Cost Like Tall Dragger No Steering Problem 5 

صفحه 48:
Airplane Components 2111111118 with Single ERE n tor heavy high wing military transports with retraction into fuselage bilsters. | 43 

صفحه 49:
Removing L.G.(Arado234) 

صفحه 50:
Airplane Design Loads Vertical loads : dependent on magnitude of touchdown rate. Longitudinal loads : caused by “spin-up’ and braking loads. Lateral loads : caused by cross-wind landings and ground turning. so 

صفحه 51:
Nose Gear Failure one of the case should be consider for structure design 

صفحه 52:


صفحه 53:


صفحه 54:


صفحه 55:
Retraction Dynamics 9 smo 

صفحه 56:
THANK YOU Leite ‏ی‎ 

صفحه 57:
MAHDI RAHNAMA, 00 :«