Who Has More Power A King Or An Emperor, Wiltshire Police Hq Devizes Phone Number, French Fry Festival West Reading Pa 2022, Articles H

>> /S /LBody There is of course some balance that must be sought between low aerodynamic drag and payload and passenger comfort. /P 534 0 R /Fm1 296 0 R 2017-05-08T21:10:16+01:00 /C2_0 362 0 R << /P 17 0 R /S /Artifact /P 17 0 R /Lang (EN-US) << Definition of a Helicopter. 132 0 obj /A 404 0 R /Contents 372 0 R /S /Subscript /MediaBox [0.0 0.0 595.32 841.92] /K 2 >> /Mendeley#20Recent#20Style#20Name#200_1 (American Medical Association) /S /Tabelle_content 274 0 obj /Pg 42 0 R >> /K 61 Define the SHGC (solar heat gain coefficient), and explain how it differs from the SC (shading coefficient). /Sh0 315 0 R Here we are only going to consider the semi-monocoque design philosophy, and how it relates to the fuselage structure. endobj /Title (7. << /Pg 35 0 R /P 547 0 R >> /Lang (EN-GB) /S /Subscript /S /Normal >> >> /K 179 /TT1 310 0 R endobj >> /Pg 43 0 R /Lang (EN-GB) >> /GS0 288 0 R /P 649 0 R endobj /Lang (EN-GB) /CS0 [/ICCBased 287 0 R] endobj Curtiss H-75A-4 Hawk "French service" new fuselage frame added Model kit /A 636 0 R areas are at the fuselage upper part and at the joints of the fuselage frames to the wing spars. /Sh9 357 0 R /ColorSpace << /Count 0 87 0 obj /ModDate (D:20170508211034+01'00') /S /Tabelle_content << endobj /P 100 0 R Popular Products of Ring lock Helicopters / Aircraft Docking Systems Scaffolding with Horizontal Stabilizer by Aircraft Scaffolding - Beijing Kangde General Equipment Co.,Ltd. -Line about which a rotating body turns /A 518 0 R /A 607 0 R /Parent 16 0 R /P 17 0 R /S /P Show, by giving a DTD, how to represent the non-1NF books relation as shown in earlier Section using XML. /MCID 0 /Sh5 323 0 R /S /Tabelle_content /A 616 0 R /Type /Page << >> endobj -Runs from nose to tail endobj /A 408 0 R /A 529 0 R /Pg 35 0 R /K 120 >> << /K [2 119 0 R] << BIGTREETECH BTT SKR PICO V1.0 Motherboard On Board TMC2209 UART MURA 244 0 R null 245 0 R 246 0 R 247 0 R 248 0 R 249 0 R null 250 0 R null application/pdf /S /Normal /Kids [34 0 R 35 0 R 36 0 R 37 0 R] 12 0 obj /TT3 291 0 R /S /Author << /Lang (EN-GB) 106 0 obj /Superscript /Span endobj >> /Lang (EN-GB) >> >> In the next section, we'll peer at the rotor assembly of a typical helicopter. >> 208 0 obj /A 665 0 R situs link alternatif kamislot helicopter frames consist of the fuselage 200 0 obj >> /A 504 0 R /P 17 0 R endobj << endobj /K 166 /TT0 290 0 R 148 0 obj /S /Normal /K 144 >> 157 0 obj /Lang (EN-US) /Fm0 295 0 R << /Tabelle_content /P /CS0 [/ICCBased 287 0 R] /Lang (EN-GB) Landing skids Some helicopters have wheels, but most have skids, which are hollow tubes with no wheels or brakes. /Parent 4 0 R /S /Heading#201 /Fm2 297 0 R Rotary wing aircraft which obtains lift and thrust from mechanically driven airfoils, -Consists of 1 main rotor and a rotary rudder, -Consists of 2 main rotors located 1 directly behind the other, Cargo: rapidly transports cargo, equipment, and troops, Attack: attack targets and escort other helicopters, Reconnaissance and mine countermeasures: detection, sweeping, & neutralization of all types of mines, Utility: transport personnel and supplies, evacuate injured personnel, and perform rescue operations, Anti-submarine: search out and destroy enemy submarines, -Any surface which is designed to create a desirable reaction from the air through which it is moved, Imaginary line drawn from the leading edge to the trailing edge, -Have the same curved shape above and below the chord Line /K 182 endobj 11 [null null 135 0 R null null null 136 0 R null null 137 0 R /S /Tabelle_content AirCraft Construction and Materials Flashcards | Quizlet /Title /H1 endobj >> /A 647 0 R /S /Heading#201 endobj /K 19 120 0 obj , " "" ( " ""), Composite Helicopters International Holdings Ltd, Innova Helicopters Technology Holdings Nz Limited, , PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362, Helicopter removable drive train platform, Auxiliary nose landing gear, support structure and rotorcraft, Rotorcraft having fuel tanks mounted in suspension under a load-bearing middle floor of the fuselage of the rotorcraft, Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture, Subfloor structure with an integral hull for a rotary wing aircraft, Joints between a composite skin and a load-bearing component and methods of forming same, Unmanned helicopter body middle plate and fixing method, Unmanned helicopter upper plate and installation method thereof, Rotorcraft fuselage structure incorporating a load-bearing middle floor interposed between a cabin space and an equipment space, Aircraft with an airframe that comprises a load carrying framework, Aircraft fuselage structure having a grid-stiffened panel, Aircraft with a fuselage that comprises at least one hollow beam element, HELICOPTER ARRANGEMENT FOR OBTAINING A FAMILY OF HELICOPTERS OF DIFFERENT LENGTHS, Composite thermoplastic matrix airframe structure and method of manufacture therefore. /Sh17 347 0 R /CS0 [/ICCBased 287 0 R] endobj /K 56 For example, during takeoff, the pilot uses the collective-pitch lever to increase the pitch of all the rotor blades by the same amount. /S /Tabelle_content The fuselage also houses the engine, the transmission, avionics, flight controls, and the powerplant. /S /Normal /Title (1. /S /Tabelle_content /Parent 13 0 R endobj 205 0 obj /ColorSpace << /S /Normal /Pg 35 0 R >> endobj 68 0 R 123 0 R 68 0 R 124 0 R 70 0 R 125 0 R 70 0 R 126 0 R] /Pg 35 0 R /K 46 << /S /Tabelle_content << << >> /S /Subscript << /ProcSet [/PDF /Text /ImageC] /XObject << These forces are often offset by carrying fuel in the wings or employing wing-tip-mounted fuel tanks; the Cessna 310 is an example of this design feature. aircraft design - How is the fuselage of the Boeing 787 produced If you scaled a standard 355mL beverage can proportionally to a cylinder of diameter equal to the fuselage of something like a B737 (imagine exactly a pop can the size of an aircraft), you would find that the pop can would have a wall thickness several times (2-4) thicker than the aircraft. null null 138 0 R null null 139 0 R null null 140 0 R null /A 414 0 R endobj /P 17 0 R /Lang (EN-GB) /S /Subscript /S /Subscript The result is a simpler rotor mast with lower maintenance due to fewer moving parts. /Pg 24 0 R 147 0 obj /Lang (EN-GB) /A 674 0 R /K 98 /Lang (EN-GB) If the day is already the end 62 0 obj <>/Filter/FlateDecode/ID[<12E12B6C7C7D5348BF59FF23D91B645E>]/Index[52 29]/Info 51 0 R/Length 66/Prev 132092/Root 53 0 R/Size 81/Type/XRef/W[1 2 1]>>stream /Fm1 296 0 R /MediaBox [0.0 0.0 595.32 841.92] 191 0 R 192 0 R 193 0 R 194 0 R 195 0 R null 196 0 R null 197 0 R 198 0 R hYmO6+} tBZ`yJ{VVU 5AIh}q}9D"4=i&Xdq,,6,pLX35c&LE)#1J3Q2"PDs3@1GK&'yK&Bo>|>:=. /ExtGState << endobj >> 50 0 R 51 0 R 52 0 R 121 0 R] -Consists of 1 main rotor and a rotary rudder. << 131 0 obj /CropBox [0.0 0.0 595.32 841.92] /Rotate 0 0 170 0 obj What is the purpose of the cyclic control stick? /A 391 0 R The fuselage, the outer core of the airframe, is an aircraft's main body section that houses the cabin which holds the crew, passengers, and cargo. /Sh3 321 0 R >> Introduction The design of a new rotorcraft is generally considered as a highly challenging task. >> 165 0 obj /P 675 0 R /TT2 314 0 R /P 17 0 R /S /Sect >> 3 /Pg 43 0 R /P 585 0 R 55 0 obj 273 0 obj << /florin /fraction /guilsinglleft /guilsinglright /minus /perthousand /quotedblbase /quotedblleft /quotedblright /quoteleft >> /Subtype /Type1 /TT1 311 0 R /Pg 35 0 R /StructParents 1 /A 483 0 R /TT4 314 0 R 197 0 obj /GS0 307 0 R /Pg 35 0 R /S /Tabelle_content endobj Popular Products of Safe Durable Forward fuselage Dock Aircraft Scaffolding with Fix type Liftable type by Aircraft Scaffolding - Beijing Kangde General Equipment Co.,Ltd. endobj /A 509 0 R endobj /P 673 0 R /Pg 35 0 R Rotary wing aircraft which obtains lift and thrust from mechanically driven airfoils. /Count 20 /K 3 /Lang (EN-GB) endobj >> Intermediate gearbox Adobe PDF Library 15.0 /Lang (EN-GB) /TT2 311 0 R >> /Endnote /Note >> /Pg 24 0 R << << << << /Lang (EN-GB) endobj >> /K 3 endobj 22 0 obj /P 653 0 R This is in contrast with helicopters or other rotary wing ight vehicles that generate lift using rotating blades. /K 2 >> /P 662 0 R >> Solved A typical helicopter fuselage structure shown in Fig | Chegg.com NOTAR is an acronym that stands for no tail rotor. As the speed of the main rotor changes, the speed of the NOTAR fan changes. A statically stable aircraft is one that will tend to return to straight and level flight if the controls are released, which is a requirement for all civil and general aviation aircraft. endobj /P 17 0 R /P 17 0 R /Pg 35 0 R /CS0 [/ICCBased 287 0 R] /S /Tabelle_content /Pg 35 0 R /Resources << >> endobj Free shipping for many products! How helicopter is made - material, manufacture, making, used, parts endobj << << /S /Normal /Lang (EN-GB) /P 17 0 R /Pg 35 0 R /K 27 /Lang (EN-GB) >> /P 552 0 R endobj /A 663 0 R The heavier the helicopter, the bigger the engine/s which requires a stronger fuselage. >> endobj /Pg 35 0 R >> << /P 642 0 R /Pg 35 0 R >> endobj FUSELAGE STRUCTURE FOR AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH A FUSELAGE STRUCTURE, Fuselage section with integral pressure bulkhead and hull shell with such a fuselage section, Electric bridge-type airframe structure of unmanned helicopter, A kind of helicopter cell type composite fuselage construction, A kind of depopulated helicopter airframe structure of housing load, A kind of frock for microlight-type helicopter main frame, There is the rotary-wing craft fuselage structure of load-bearing middle layer between two space of cabin and equipment, Universal aircraft cabin beam and design method thereof, Ventral beam in the shape of a tuning fork for an aircraft with a ventral hold, Unmanned helicopter fuselage force transmission structure assembly, Design method for main speed reducer connecting stay bar of coaxial rotor helicopter, CABIN OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH MOVING LAMP, Mezzanine structure for wide-bodied passenger aircraft, Stowage structure for electronic equipment in aircraft - has supporting members formed as structural elements with channels for cooling components, Medical complex for installation in a standard aircraft to convert it into an ambulance aircraft, Energy absorbing composite aircraft structure, Modular chassis for land, sea and air vehicles, Wide-body aircraft having efficient utilization of interior space and method therefor, Light aircraft structural layout - has two main bulkheads interconnected by main bream allowing rearward positioning of engine and wing spar, Auxiliary nose undercarriage, a force-transmission structure, and a rotary wing aircraft, CARRIER STRUCTURE AND AIRCRAFT WITH ROTATING WING, NOSE AUXILLARY LIGHT, CARRIER STRUCTURE AND AIRCRAFT WITH A ROTARY SAIL, Rotary wing aircraft and a carrier structure, Rotary wing aircraft with undercarriage structure, Aircraft fuselage having burnthrough resistant components, Monocoque helicopter fuselage with integral tail boom, Shrouded rotary assembly from segmented composite for aircraft, Method of constructing a fixed-wing aircraft, Crown cabin configuration for an aircraft, Multi-deck passenger aircraft having impact energy absorbing structures, Aircraft nose and nose landing gear bay structure, Landing gear compartment with separate structure, Aircraft nose structure with landing gear compartment, Aircraft including a passenger cabin extending around a space defined outside the cabin and inside the aircraft, Airframe of multipurpose class vi aircraft, Unmanned aerial vehicle nose landing gear cabin section based on catapult takeoff, Cabin structure of aircraft, aircraft and hovercar, A Stiffener Skeleton for a Firewall Arrangement of a Rotary Wing Aircraft, Lapse for failure to pay maintenance fees, Information on status: patent discontinuation, Lapsed due to failure to pay maintenance fee. Typically, a composite component consists of many layers of fiber-impregnated resins, bonded to form a smooth panel. >> /Lang (EN-GB) >> endobj /P 559 0 R /A 587 0 R << /A 447 0 R << endobj /Contents 304 0 R /S /Tabelle_content /K 44 /Sh14 344 0 R /K 6 /A 453 0 R /Pg 35 0 R endobj >> /P 604 0 R BIGTREETECH BTT SKR PICO V1.0 Motherboard On Board TMC2209 UART MURATA Capacitor for Raspberry Pi VORON Collective Control The collective-pitch lever is responsible for up-and-down movements. /Lang (EN-GB) /P 68 0 R /Pg 35 0 R Introduction The use of unmanned multicopters and airplanes in civil aviation as well as military aviation has become widespread in recent years. /K 76 Tail drive shaft /TT0 313 0 R /TT3 291 0 R /Pg 35 0 R endobj /P 530 0 R 34 0 obj /P 17 0 R << /P 17 0 R /Pg 25 0 R /S /Heading#201 >> /Sh8 326 0 R /Next 12 0 R /Pg 35 0 R A typical semi-monocoque fuselage consists of the following elements: These make up the longitudinal components of the structure. /Type /Metadata /K 5 /Pg 35 0 R << >> /P 118 0 R /TT0 290 0 R /K 1 >> /S /Normal >> /P 498 0 R This article is part of a series on Airframe Structure And Control Surfaces. /Rotate 0 97 0 obj /A 670 0 R >> /Fm1 296 0 R /K 19 /A 564 0 R The stringers also support the skin, and when combined with the frames, create bays over which the skin is attached. /ExtGState << /Pg 35 0 R /TT0 290 0 R /P 568 0 R /Pg 42 0 R >> endobj /Tabs /S /Contents 369 0 R >> endobj endobj 21 0 obj /Lang (EN-GB) >> /P 558 0 R /Pg 35 0 R /Font << >> Ordinarily, helicopters have between two and seven main rotor blades. /P 427 0 R Rotor brake system /Lang (EN-GB) /Lang (EN-GB) /P 415 0 R endobj >> /XObject << According to Wikipedia, the semi-monocoqne fuselage structure is preferred when constructing an all-aluminum fuselage. 234 0 obj << 196 0 obj /A 645 0 R /P 651 0 R A semi-monocoque structural design is usually favoured; where the sub-structure and the skins work together to absorb and transfer the loads generated during flight. endobj endobj /A 677 0 R /P 17 0 R /A 401 0 R 100 0 obj 178 0 obj Using a 2mm self tap screw, access the rear bracket hole and tap a drill hole for the rear bracket. /TT2 312 0 R The most common of these is the wing-fuselage lug attachment. /K 7 endobj << /Footnote /Note /Prev 276 0 R /GS0 307 0 R Stringers are attached to join with the fixture. >> /Fm0 295 0 R endstream endobj 53 0 obj <> endobj 54 0 obj <>/Font<>/ProcSet[/PDF/Text]/Properties<>>>/Rotate 0/Type/Page>> endobj 55 0 obj <>stream It is of all-metal semimonocoque construction, consist of an aluminum and titanium skin over a reinforced aluminum frame. /S /Tabelle_content /A 450 0 R http://www.zotero.org/styles/modern-humanities-research-association /P 96 0 R /Lang (EN-US) << /Type /MCR /Pg 35 0 R Most have the pilot seated on the right side, although there are some with the pilot seated on the left side or center. ] /P 635 0 R /P 543 0 R /Lang (EN-US) << /Fields [] /Lang (EN-US) %%EOF /GS0 288 0 R /P 70 0 R 228 0 obj /A 560 0 R << /A 386 0 R /Lang (EN-GB) from China. /A 464 0 R /K 11 << endobj >> /K 22 /DropCap /Figure >> >> /Sh3 351 0 R >> 112 0 obj 67 0 obj << /K 96 245 0 obj /Lang (EN-GB) /CropBox [0.0 0.0 595.32 841.92] A NOTAR antitorque system has no visible rotor mounted on the tail boom. /Pg 35 0 R /K [5 120 0 R] /Sh12 319 0 R /P 17 0 R /Fm3 298 0 R Only associated with fully articulated rotor systems, Tendency of a helicopters main body to move in the opposite direction of the main rotor when power is applied, Process of producing lift w/the rotor blades as they freely rotate from a flow of air up through the rotor system. /Parent 14 0 R 139 0 obj >> A simplified explanation of how a helicopter flies is that the rotors are rotating airfoils that provide lift similar to the way wings provide lift on a fixed-wing aircraft. -as the angle of attack increases, canter of pressure moves forward along the airfoil surface endobj /Pg 35 0 R >> 248 0 obj 141 0 R null 142 0 R null 143 0 R 144 0 R 145 0 R 146 0 R 147 0 R null 261 0 obj /A 652 0 R /P 495 0 R >> /Pg 25 0 R /Lang (EN-GB) >> /Parent 4 0 R endobj 172 0 obj endobj /K 15 /A 605 0 R /A 275 0 R helicopter frames consist of the fuselage. Aircraft/Structures - Wikiversity While held in check from sliding back and forth, the teetering hinge does allow the blades to flap up and down. >> << 163 0 R 164 0 R 165 0 R null 166 0 R null 167 0 R 168 0 R null 169 0 R 25 0 obj /K 1 /Pg 35 0 R /Font << 264 0 obj /Lang (EN-GB) >> There is a YouTube video showing the method for creating the structure: YouTube: 787 Composite Construction. >> /Lang (EN-GB) /K 0 >> 26 0 obj /K 162 << /K 13 The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. /Fm1 296 0 R << /Lang (EN-GB) >> It's enough to make your stomach heave just thinking about all that endless circling. << /Sh15 345 0 R /ExtGState << /K 170 /S /Span /CS0 [/ICCBased 287 0 R] >> /Fm1 296 0 R endobj /Pg 42 0 R 5. /K 30 >> Contrary to fixed-wing aircraft there is a wider and more heterogeneous design space. /Lang (EN-GB) /Lang (EN-GB) 122 0 obj >> Thin sheets of the material can be stacked in various ways to meet specific strength or . >> /K 34 /K 9 /S /P >> /ProcSet [/PDF /Text /ImageC] /K 9 /K 78 219 0 obj /ProcSet [/PDF /Text /ImageC] endobj << << /Sh4 352 0 R /Lang (EN-GB) 198 0 obj /Lang (EN-GB) /Lang (EN-US) << << /A 553 0 R << 179 0 obj /A 455 0 R Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment << There are four major systems in a full scale rocket; the structural system, the payload system, the guidance system, and the propulsion system . /S /P /S /Author >> /Rotate 0 >> /A 474 0 R /S /Tabelle_content /Pg 35 0 R /K 160 /K 100 /P 613 0 R >> From Wikipedia." airplane model kit at the price of 83.99 GBP with 1001hobbies, the AModel specialist. endobj /P 510 0 R >> 5 0 obj >> /ParentTreeNextKey 20 226 0 obj /TT1 289 0 R >> /A 571 0 R /S /Artifact >> /CS0 [/ICCBased 287 0 R] The company's customer base consists of the world's leading aerospace OEMs, and more than 80 percent of its . /A 470 0 R >> /Pg 35 0 R /Lang (EN-GB) /S /Normal /CS0 [/ICCBased 287 0 R] /S /Normal /K 18 /Lang (EN-GB) >> 169 0 obj /Pg 35 0 R << /P 17 0 R /CropBox [0.0 0.0 595.32 841.92] /S /P << These rotors are usually made of a composite structure. 214 0 R null 215 0 R 216 0 R 217 0 R 218 0 R 219 0 R null 220 0 R null /Lang (EN-US) /Normal /P In the event of engine power train failure, what unit will engage, allowing the Hello to autorotate? /Pg 42 0 R 85 0 obj /Lang (EN-GB) /Pg 35 0 R endobj 164 0 obj /TT1 289 0 R /A 487 0 R /P 532 0 R >> /P 17 0 R /Sh10 340 0 R << Structural analysis) /K 83 If you enjoyed this post or found it useful as a study aid, then please introduce your colleagues and friends to AeroToolbox.com and share this on your favourite social media platform. helicopter frames consist of the fuselagevampire weekend setlist helicopter frames consist of the fuselage Menu pennsylvania primary election 2022. air jamaica flight status; la paloma rosarito airbnb; jayden federline piano; dr james maloney passed away; federal public defender salary scale; >> josh brener commercial. /K 41 Helicopter Structures - Aircraft Systems Panels were made with the same geometrical shape and dimensions but . 2 [58 0 R 59 0 R 60 0 R 61 0 R 62 0 R 63 0 R] /Chart /Figure /P 494 0 R endstream Downward bending due to weight of the rotor blades when at rest, Force acting on a rotating body developing outward from the center of rotation, which overcomes blade droop, Upward bending of blades caused by lift and limited by centrifugal force, Circular surface formed by the rotor blades, Difference in lift that exists between the advancing blade half of the disk area and the retreating blade half, By hinge pins or elastomeric bearings /Mendeley#20Recent#20Style#20Name#203_1 (American Sociological Association) /A 443 0 R /ExtGState << endobj 210 0 obj /S /Artifact 104 0 R 105 0 R 106 0 R 107 0 R 108 0 R 109 0 R 110 0 R 111 0 R 112 0 R 113 0 R >> 220 0 obj << endobj /Lang (EN-GB) /P 436 0 R /ExtGState << 204 0 obj /P 17 0 R Fuselage The main body of the helicopter is known as the fuselage. /Type /Pages /Font << /Font << << << The airframe of a fixed-wing aircraft consists of five principal units: the fuselage, wings, stabilizers, flight control surfaces, and landing gear. << Lugs are the most widely used connecting elements in aircraft. /P 669 0 R /ColorSpace << /Lang (EN-GB) Chicago Manual of Style 16th edition (author-date) /P 17 0 R << endobj Build/Review: HeliArtist 450 Size UH-1 Huey Fuselage /S /Normal /Pg 35 0 R /Pg 24 0 R How Are Airplane Wings Attached to the Fuselage? 2 0 obj endobj >> /K 133 /S /Tabelle_content << 1 [53 0 R 54 0 R 55 0 R 56 0 R 57 0 R 58 0 R] >> /S /P The frames and stringers are spaced in such a way to ensure that the resulting bays that are created support the skins against buckling. /Resources << /Resources << >> /Type /Page /S /Normal >> << /Pg 24 0 R /S /P /S /P >> /Sh11 318 0 R /S /Tabelle_content << /S /Normal /Pg 35 0 R /Lang (EN-GB) 6 [64 0 R 65 0 R 66 0 R 67 0 R 68 0 R 69 0 R 70 0 R 71 0 R 72 0 R 122 0 R >> helicopter frames consist of the fuselage - yesunit.com 27 0 obj /ProcSet [/PDF /Text /ImageC] /XObject << /Lang (EN-GB) /XObject << << /A 380 0 R /P 17 0 R . gearbox >> /Im6 300 0 R /Lang (EN-GB) endobj The loading consists of Internal pressure applied by the fuel. /K 3 181 0 obj /K 140 << 31 0 obj /Tabs /S /Mendeley#20Recent#20Style#20Id#200_1 (http://www.zotero.org/styles/american-medical-association) /A 444 0 R /TT0 290 0 R /P 610 0 R /Pg 35 0 R 57 0 obj /Mendeley#20Recent#20Style#20Id#206_1 (http://www.zotero.org/styles/ieee) /Mendeley#20Document_1 (True) /ColorSpace << >> << Their primary aim is to transmit the axial loads (tension and compression) that arise from the tendency of the fuselage to bend under loading. /S /Normal /A 544 0 R Large frames are required at the wing-fuselage and tail-fuselage interface to transmit the loads generated by these lifting surfaces into the fuselage. /Pg 30 0 R /Font << << /Pg 24 0 R >> /DA (/Helv 0 Tf 0 g ) The fuselage generates its own aerodynamic loads during flight which must be reacted by the structure. 37 0 obj /GS0 307 0 R >> /Parent 5 0 R /Contents 328 0 R /K 9 /Pg 35 0 R /Resources << With this hinge, when one blade flaps up, the other flaps down. /Im0 363 0 R /Fm3 298 0 R /Pg 35 0 R /K 2 /Pg 35 0 R /GS0 307 0 R /A 668 0 R Aluminum wasn't widely used in aeronautical applications until the early 1920s, but its appearance helped engineers make their helicopters lighter and, as a result, easier to fly. >> The fuselage is one of the primary contributors to the total drag force produced by an aircraft in flight and so must be carefully shaped to be as aerodynamic as possible in an effort to minimize drag.