/InlineShape /Figure >> << >> /Pg 35 0 R /S /P << /Pg 35 0 R /Fm3 298 0 R >> << /S /Tabelle_content /Sh12 319 0 R /Mendeley#20Recent#20Style#20Id#206_1 (http://www.zotero.org/styles/ieee) /S /Span /D [25 0 R /XYZ 104 520 0.0] Provides data that is required by the CIPS unit for blade tracking analysis, Mounted accelerometers on or around the component under test provide to the CIPS the data required to calculate a balance or soothing solution, Helicopter flying handbook, ch 1-3 intro / Ae, Introduction to Chemical Engineering Thermodynamics, Hendrick Van Ness, J.M. >> >> /K 4 /Pg 42 0 R /Pg 35 0 R >> /Lang (EN-GB) Design process) 295. /K 56 /Last 12 0 R << /Fm4 299 0 R /Mendeley#20Recent#20Style#20Name#203_1 (American Sociological Association) FRAME FUSELAGE STATION 177.2 (Drawing 143F079) The frame at Fuselage Station 177.2 functions as a stiffening member for the fuel cell liner. << /Strong /Span /A 670 0 R >> /XObject << /TT0 290 0 R /S /Normal /A 602 0 R Fabric-covered fuselage of the Heath Parasol, 1931 1931: Giant Flying Boat for Navy: the first of nine huge twin-engined Martin flying boats, the largest craft of their kind in th. http://www.zotero.org/styles/nature >> /A 408 0 R endobj /Pg 35 0 R /RoleMap 19 0 R /Pg 41 0 R >> >> >> One or more horizontal hinges provide for flapping on a fully articulated rotor system. << >> /K 80 111 0 obj /GS0 307 0 R /P 17 0 R >> 79 0 obj /Type /Page /Fm0 295 0 R >> /ParentTree 18 0 R /S /Normal /A 504 0 R << /Tabs /S Anti-torque tail rotor Without a tail rotor, the main rotor of a helicopter simply spins the fuselage in the opposite direction. /A 388 0 R >> /Lang (EN-GB) /Contents 366 0 R /K 82 /A 564 0 R /Lang (EN-GB) endobj << /Lang (EN-GB) /P 565 0 R << >> /Pg 35 0 R -sections: gas generator, power turbine, main drive shaft, -may be axial flow or combined axial/centrifugal flow gas turbine engine /K << /ColorSpace << /Lang (EN-GB) >> /PageLayout /SinglePage << /Lang (EN-GB) >> 102 0 obj fuselage shell geometry calculations; optional integration of a cylindrical fuselage midsection between the nose and tail sections; addition of landing and bump maneuvers to the load cases sizing the fuselage; ability to introduce an elliptical spanwise lift load distribution on the wing; variation of wing thickness ratio from tip to root; ability /Parent 15 0 R >> /K 164 /Pg 35 0 R /Creator (Acrobat PDFMaker 17 for Word) /Contents 377 0 R endobj /Im0 368 0 R << /CS1 [/ICCBased 306 0 R] These supports are called frames if they are . /K 3 /P 17 0 R >> 237 0 obj /Lang << /Lang (EN-GB) >> -Runs from nose to tail << For instance, 53 percent of the aircraft consists of carbon-fiber composite parts. /A 473 0 R /Lang (EN-GB) /Sh7 355 0 R According to Wikipedia, the semi-monocoqne fuselage structure is preferred when constructing an all-aluminum fuselage. /K 72 /S /Tabelle_content 110 0 obj /Im0 330 0 R , " "" ( " ""), 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. /Lang (EN-GB) endobj /S /Subscript /Lang (EN-GB) endobj /Lang (EN-GB) These rotors are usually made of a composite structure. endobj /Pg 35 0 R 115 0 obj endobj << endobj The latter two are still in use. /Pg 33 0 R << /Lang (EN-GB) /StructParents 6 << /GS0 307 0 R /florin /fraction /guilsinglleft /guilsinglright /minus /perthousand /quotedblbase /quotedblleft /quotedblright /quoteleft /Parent 4 0 R /K 157 << /K 155 Typically, a composite component consists of many layers of fiber-impregnated resins, bonded to form a smooth panel. /P 17 0 R /Pg 43 0 R /S /P /S /Heading#201 endobj /K 3 /Im0 334 0 R /Rotate 0 << /Lang (EN-GB) /P 17 0 R /Type /Page endobj 199 0 R 200 0 R 201 0 R null 202 0 R null 203 0 R 204 0 R 205 0 R 206 0 R /Pg 24 0 R As far as the other plane parts are concerned, the engine's piston is usually made out of steel whereas many other major parts are made of aluminum alloys. /Lang (EN-GB) /P 640 0 R /CropBox [0.0 0.0 595.32 841.92] /K 8 In this post well be focusing on the fuselage; specifically, we discuss the design of a typical semi-monocoque structure, and the various structural components and loadings that contribute to the final design. 163 0 obj /Font << /K 38 /Rotate 0 endobj -Can be thought of as the Aircraft pivot pts. /ProcSet [/PDF /Text /ImageC] Where is the cyclic control stick located? /Pg 36 0 R /Pg 35 0 R The semi-monocoque construction, which is virtually standard in all modern aircraft, consists of a stressed skin with added stringers to prevent buckling, attached to hoop-shaped frames. /P 73 0 R /Rotate 0 /S /Normal /Lang (EN-GB) 222 0 obj /Pg 25 0 R << /Pg 30 0 R /P 17 0 R . >> /Lang (EN-GB) /Pg 35 0 R << stream /Pg 35 0 R >> /S /Tabelle_content /Pg 35 0 R /K 67 /Contents 328 0 R << /Length 7746 /TT2 314 0 R /CS1 [/ICCBased 306 0 R] /K 170 << endobj /Pg 35 0 R /TT0 313 0 R /TT1 313 0 R %PDF-1.3 /A 441 0 R >> /Sh10 317 0 R >> endobj /Lang (EN-GB) /Parent 4 0 R endobj /A 575 0 R /ProcSet [/PDF /Text] /S /Normal 73 0 obj Helicopters are made from an array of alloys, composites, laminates, resins, and plastics all designed to give incredible strength, stiffness, flexibility & durability while keeping the helicopter as light as possible. 16 a, paragraph 1, Information on the status of an ep patent application or granted ep patent, Gb: translation of amended ep patent filed (gb section 77(6)(b)/1977), Nl: receipt of modified translations in the netherlands language after an opposition procedure, Annual fee paid to national office [announced via postgrant information from national office to epo], Nl: lapsed or anulled due to non-payment of the annual fee, Lapsed in a contracting state [announced via postgrant information from national office to epo], Gb: european patent ceased through non-payment of renewal fee. >> >> >> /Im0 363 0 R 188 0 obj /CS1 [/ICCBased 306 0 R] 78 0 obj << /TT2 329 0 R << /Next 276 0 R Monocoque H|SMo0+, Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment. /Lang (EN-GB) /P 586 0 R /GS1 308 0 R /Parent 16 0 R endobj endobj Introduction The design of a new rotorcraft is generally considered as a highly challenging task. /K 77 /P 532 0 R /Sh15 345 0 R Engineers continually search for ways to reduce vibration and noise caused by the rotating parts of the helicopter. /P 70 0 R /Pg 25 0 R /S /Normal << << << /K 3 /P 419 0 R 132 0 obj /ProcSet [/PDF /Text /ImageC] 10 0 obj /Pg 35 0 R It's enough to make your stomach heave just thinking about all that endless circling. Please copy/paste the following text to properly cite this HowStuffWorks.com article: Tom Harris & Talon Homer /A 390 0 R /K 124 /K 86 /Tabs /S 42 0 obj endobj /Lang (EN-GB) /A 553 0 R /Type /Pages /K 149 141 0 obj /GS2 309 0 R /C2_0 365 0 R >> 104 0 obj /Lang (EN-GB) >> /S /Subscript /TT1 313 0 R /Type /Font Customer satisfaction 4,2/5. American Psychological Association 6th edition >> /K 32 /Kids [34 0 R 35 0 R 36 0 R 37 0 R] /K 148 6 0 obj /Pg 42 0 R /Sh17 347 0 R >> /Name /Helv Piper PA-18 Super Cub with a Space Frame Fuselage. /Lang (EN-GB) << << The stringers also support the skin, and when combined with the frames, create bays over which the skin is attached. The A-129 International is a fast, manoeuvrable helicopter. /A 584 0 R /A 520 0 R /Pg 35 0 R The fuselage structure must be sufficiently strong to ensure safe operation throughout the flight envelope. >> /Type /Page >> endobj The density of an aluminium alloy is approximately one-third that of steel which allows for thicker structural sections to be built without any weight penalty. /MediaBox [0.0 0.0 595.32 841.92] /K 116 229 0 obj /ExtGState << /CS1 [/ICCBased 306 0 R] /A 598 0 R /S /P /Lang (EN-GB) /Count 6 /Marked true /P 17 0 R /Parent 5 0 R /K 112 >> /DropCap /Figure /Pg 35 0 R Cyclic Control A helicopter pilot controls the pitch, or angle, of the rotor blades with two inputs: the cyclic- and collective-pitch levers, often just shortened to the cyclic and the collective. << /S /Tabelle_content /S /Tabelle_content of the year, the new value of the object will represent the first day of the year. /Fm2 297 0 R /S /Tabelle_content 270 0 obj >> /S /Subscript >> /Lang (EN-GB) /MediaBox [0.0 0.0 595.32 841.92] >> /Pg 35 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. During the early days of aviation, primitive fuselages were built with wood. /Lang (EN-US) /TT3 314 0 R endobj << /P 421 0 R /Type /Page /K [417 0 R 418 0 R 419 0 R 420 0 R 421 0 R 422 0 R 423 0 R 424 0 R 425 0 R 426 0 R /K 6 >> Main transmission gearbox accessory section 3434 carolina southern belle; why is austria a developed country; helicopter frames consist of the fuselage. << << /K 144 /Next 21 0 R /Mendeley#20Recent#20Style#20Id#203_1 (http://www.zotero.org/styles/american-sociological-association) What is the blade pitch movement controlled by? /Lang (EN-GB) /P 604 0 R /P 73 0 R /Type /Pages /A 536 0 R endobj Tubular and sheet metal substructures are usually made of aluminum, though stainless steel or titanium are sometimes used in areas subject to higher stress or heat. The main rotor, of course, is the most important part of a helicopter. "How Helicopters Work" /Fm0 295 0 R << << >> /Lang (EN-GB) << /DisplayDocTitle true /S /Table /Metadata 3 0 R 101 0 obj /Strikeout /Span /K 15 >> /Prev 11 0 R In many models, a frameless plastic canopy surrounds the pilot and connects in the rear to a flush-riveted aluminum frame. /Sh6 324 0 R /P 17 0 R /Fm2 297 0 R /A 445 0 R Tail gearbox, -supports and drives rotor head assembly >> endobj << /Lang (EN-GB) /S /P << 149 0 obj /S /Tabelle_content References) In a semi-monocoque structure both the outer skin and the internal substructure are load bearing, and both contribute to the overall stiffness of the structure. /K 154 /K 94 << hb```"QfE``CKWrL`fk`e`gvZ8^"wk%rL 24:$n30V@`9>@^iOAmwX1z2u) 8 ~* << /P 675 0 R The wings consist of two essential parts. /S /Strong /Lang (EN-GB) 1 0 obj /StructParents 19 endobj /GS0 288 0 R /Pg 35 0 R /Mendeley#20Recent#20Style#20Name#200_1 (American Medical Association) endobj >> /K 415 0 R endobj 2 0 obj /S /Title /S /Tabelle_content If the day is already the end /A 560 0 R Aluminium has many advantages over steel. /K 178 47 0 obj In front and center of the pilot's and co-pilot's seats (interconnected). /AcroForm 2 0 R /S /Tabelle_content >> /Pg 35 0 R NAFEMS World Congress 2017 << /K 12 null] /Parent 15 0 R /GS0 307 0 R endobj /S /Tabelle_content endobj /Kids [38 0 R 39 0 R 40 0 R 41 0 R 42 0 R 43 0 R] /P 17 0 R >> endobj josh brener commercial. /P 6 0 R /K 172 endobj /K 150 /A 488 0 R 258 0 obj /Parent 5 0 R >> >> 178 0 obj /S /P << /S /Tabelle_content /Font << . /Pg 33 0 R /A 548 0 R >> /A 676 0 R - The invention relates to a helicopter fuselage of the type including a central structure to which are attached a front structure, a rear structure and a landing gear, and which supports a transmission gearbox, a main rotor and at least one engine (50), and of the type in which the central structure includes a framework (16) fitted with cladding elements which define the external shape of the . The attachment bracket, also known as a wing box, consists of a lug and a portion of spar connected with several bolts. /P 538 0 R /BaseFont /ZapfDingbats /igrave /iacute /icircumflex /idieresis /eth /ntilde /ograve /oacute /ocircumflex /otilde /Parent 16 0 R /Keywords (NAFEMS World Congress 2017) /TT3 291 0 R endobj /CropBox [0.0 0.0 595.32 841.92] << The heavier the helicopter, the bigger the engine/s which requires a stronger fuselage. /K 13 66 0 obj /S /Tabelle_content /Lang (EN-GB) Add the following overloaded operators: /Pg 35 0 R << 147 0 obj % /TT0 290 0 R /Fm3 298 0 R >> >> /S /Normal /P 610 0 R /Lang (EN-US) >> 140 0 obj endobj >> Thicker skins are advantageous as these are less likely to buckle under load, resulting in a more efficient structure. /Lang (EN-GB) /Fm2 297 0 R >> /K 181 /Mendeley#20Recent#20Style#20Id#204_1 (http://www.zotero.org/styles/chicago-author-date) endobj endobj /P 17 0 R endobj /Pg 35 0 R /P 608 0 R endobj endobj 125 0 obj /Pg 35 0 R >> /Pg 35 0 R << /Pg 35 0 R /ExtGState << 208 0 obj /Pg 24 0 R /Lang (EN-GB) June 22, 2022. ilive code for dish remote . Using a 2mm self tap screw, access the rear bracket hole and tap a drill hole for the rear bracket. /GS0 307 0 R >> /Fm3 298 0 R /A 273 0 R /CS0 [/ICCBased 287 0 R] /Pg 43 0 R Determine the suitable material for each of the component. /TT2 291 0 R /S /Artifact >> /Pg 42 0 R >> /Pg 35 0 R /Pg 35 0 R 151 0 obj endobj /S /Tabelle_content >> /Lang (EN-GB) /TT3 336 0 R /Parent 13 0 R 20 0 obj -through the use of a freewheeling unit, located w/in main gearbox assembly, Stops rotation of rotor head [Figure], The fuselage, the outer core of the airframe, is an aircrafts main body section that houses the cabin which holds the crew, passengers, and cargo. /Lang (EN-GB) /K 1 >> /A 492 0 R /Sh5 323 0 R Customer satisfaction 4,2/5. [Figure 7]. /Type /Page endobj /TT0 290 0 R /Pg 35 0 R /A 672 0 R /Lang (EN-US) << >> /Rotate 0 << /BaseFont /Helvetica /Pg 26 0 R /Lang (EN-GB) /Count 20 /K 17 >> 3 Wing Contents Providing lift is the main function of the wings of an aircraft. << >> /CS0 [/ICCBased 287 0 R] >> /Title (7. /K 126 >> /S /Tabelle_content /A 392 0 R /P 68 0 R /Lang (EN-GB) /Sh13 343 0 R 266 0 obj endobj /TT1 289 0 R /S /P /Font << The various structural design methodologies were discussed in part one of this series. /CropBox [0.0 0.0 595.32 841.92] /K 18 /P 17 0 R /K 69 << -moves the thrust of the rotor and the lift of the helicopter, pulling it in the direction of the tip path plane. 259 0 R 260 0 R 261 0 R 80 0 R 81 0 R 82 0 R 262 0 R 263 0 R 81 0 R] /Prev 276 0 R Chicago Manual of Style 16th edition (author-date) /P 669 0 R /Type /Page /Mendeley#20Recent#20Style#20Id#200_1 (http://www.zotero.org/styles/american-medical-association) /Pg 30 0 R /S /Normal endobj endobj /K 59 /GS0 307 0 R >> /K 158 /P 537 0 R >> endobj /A 391 0 R << /Rotate 0 hbbd``b` /A 518 0 R >> 30 0 obj /Fm4 299 0 R << << << /Rotate 0 << /K 1 /Lang (DE-DE) /P 501 0 R /P 17 0 R /S /Subscript /S /Heading#201 Thin sheets of the material can be stacked in various ways to meet specific strength or . 67 0 obj /Lang (EN-GB) /K 42 >> endobj /Pg 35 0 R /A 454 0 R /P 17 0 R >> 166 0 obj /S /Normal /MediaBox [0.0 0.0 595.32 841.92] << /CropBox [0.0 0.0 595.32 841.92] /Title (4. /A 414 0 R -effective to a height of approximately half the rotor diameter /TT3 313 0 R /K 34 55 0 obj >> By - June 6, 2022. 2017-05-08T21:10:16+01:00 /S /Normal /Rotate 0 /Lang (EN-GB) /A 578 0 R /Contents 331 0 R 18 0 obj /ColorSpace << /Pg 30 0 R >> << /P 17 0 R << endobj 12 0 obj >> The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. /A 397 0 R /Pg 30 0 R >> /TT2 303 0 R Accessories, -extracts & converts thermal or heat energy into mechanical energy to drive main transmission gearbox /ExtGState << /TT2 303 0 R 2023 acura integra type s; denmark size compared to massachusetts; accidentes de frontier airlines; how old was laura marano in austin and ally; chicago tribune death notices last 3 days << >> /Tabs /S << /TT4 314 0 R /Fm4 299 0 R endobj Panels were made with the same geometrical shape and dimensions but . 185 0 obj /A 661 0 R /Lang (EN-GB) Some modern helicopter main rotors have been designed with flextures. >> /Lang (EN-GB) /S /Normal 52 0 obj <> endobj Define the SHGC (solar heat gain coefficient), and explain how it differs from the SC (shading coefficient). 195 0 obj /Lang (EN-US) /K 2 The wing is covered in part three, flaps in part four, and the tail in part five. Combustion /Fm0 295 0 R /Subtype /Type1 273 0 obj /S /Tabelle_content /K 4 /Pg 33 0 R << << Quick nationwide delivery of your "Antonov An-30. /A 643 0 R American Sociological Association endobj << /Pg 42 0 R /P 17 0 R /Parent 13 0 R 128 0 obj << /Lang (EN-GB) /Pg 42 0 R /Lang (EN-US) /StructParents 18 /K 5 >> /K [12 267 0 R] /CS1 [/ICCBased 306 0 R] /K 19 >> endobj %PDF-1.6 % /S /P /S /formula /K 7 /Tabs /S /P 417 0 R /Resources << 148 0 obj >> >> >> /ProcSet [/PDF /Text /ImageC] endobj 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 /Tabs /S /Pg 33 0 R /Lang (EN-GB) /Kids [13 0 R 14 0 R 15 0 R 16 0 R] /Pg 30 0 R /P 657 0 R 174 0 obj /Pg 35 0 R /K 88 endobj endobj /K 4 276 0 obj /ExtGState << /Pg 35 0 R >> /Lang (EN-GB) /Pg 35 0 R endobj 14 132 0 R 16 133 0 R 18 134 0 R 20] endobj Tandem Rotor. endobj >> 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; When blade rotation reaches the point where the blade becomes the retreating blade, the extra lift is lost and the blade flaps downward. << All these load cases, and the interaction between cases must be considered to arrive at a final design. /K 123 /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /Lang (EN-GB) Definition of a Helicopter. /Lang (EN-GB) /Sh2 350 0 R /ExtGState << -allows blades to flap up, down, lead, and lag, -Air cushion formed when hovering close to the ground /S /Tabelle_content /K 2 endobj This article is part of a series on Airframe Structure And Control Surfaces. << /Pg 35 0 R >> /S /Tabelle_content 106 0 obj 155 0 R 156 0 R 157 0 R 158 0 R 159 0 R null 160 0 R null 161 0 R 162 0 R /Lang (EN-GB) /Lang (EN-GB) /A 412 0 R endobj /Type /Page /CropBox [0.0 0.0 595.32 841.92] /Subtype /XML << Graphite-epoxy is one of several types of composite materials that are becoming widely used for many aircraft structures and components. /Lang (EN-GB) /K 1 /P 70 0 R /K 8 /Lang (EN-GB) 170 0 obj May 23, 2021 . /P 503 0 R 265 0 obj /S /Span >> /S /Heading#201 /S /Normal Additionally, the remainder of the air from the fan is sent through the tail boom to a vent on the aft left side of the boom where it is expelled. /P 621 0 R /A 459 0 R /S /P << This is done by changing the pitch of the tail rotor blades. 54 0 R 55 0 R 56 0 R 57 0 R 58 0 R 59 0 R 60 0 R 61 0 R 62 0 R 63 0 R /Pg 43 0 R Position the helicopter and drill holes for the front mounting bracket. endobj << >> /S /P /A 500 0 R /P 17 0 R >> /A 275 0 R Popular Products of Safe Durable Forward fuselage Dock Aircraft Scaffolding with Fix type Liftable type by Aircraft Scaffolding - Beijing Kangde General Equipment Co.,Ltd. /Sh8 326 0 R /K 147 helicopter frames consist of the fuselage. /P 17 0 R /S /Subscript /S /LBody /Mendeley#20Recent#20Style#20Name#205_1 (Harvard Reference format 1 \(author-date\)) << 217 0 obj >> /P 17 0 R << These are hubs and hub components that are made out of advanced composite materials. /TT1 290 0 R -Consists of 1 main rotor and a rotary rudder. 235 0 obj 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. endobj 180 0 obj >> 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 endobj D. Schwinn, P. Weiand, M. Schmid 28 0 obj >> << /A 529 0 R >> /Fm4 299 0 R "Integral frames made of CFRP may replace differential constructions, due to higher stiffness, and . >> /Pg 35 0 R /Rotate 0 The load-bearing skins are attached to the stringers and frames of an aluminium aircraft through rivets. $\begingroup$ @mins No, that's not even close. -as the angle of attack increases, canter of pressure moves forward along the airfoil surface Hydraulically operated http://www.zotero.org/styles/american-political-science-association -independent from gas generator, -exhaust gases from the gas generator turbine drive the power turbine >> /S /Normal Popular Products of Ring lock Helicopters / Aircraft Docking Systems Scaffolding with Horizontal Stabilizer by Aircraft Scaffolding - Beijing Kangde General Equipment Co.,Ltd. /CS0 [/ICCBased 287 0 R] /Pg 35 0 R endobj /P 535 0 R /Pg 35 0 R /Lang (EN-GB) >> /S /Normal >> /P 512 0 R >> /K 91 /Font << >> /Contents 305 0 R /Type /Page /Lang (EN-GB) /K 133 endobj /Count 6 << /S /Tabelle_content /Lang (DE-DE) >> /A 665 0 R /Lang (EN-US) /A 663 0 R http://www.zotero.org/styles/american-medical-association /GS0 288 0 R >> 72 0 obj /Sh4 322 0 R /S /Subscript The fuselage (/ f ju z l /; from the French fusel "spindle-shaped") is an aircraft's main body section. 209 0 obj 68 0 R 123 0 R 68 0 R 124 0 R 70 0 R 125 0 R 70 0 R 126 0 R] endobj /Pg 35 0 R endobj /Lang (EN-US) >> /MediaBox [0.0 0.0 595.32 841.92] Most have the pilot seated on the right side, although there are some with the pilot seated on the left side or center. /StructParents 11 endobj Free shipping for many products! /Author (D. Schwinn, P. Weiand, M. Schmid) 82 0 obj /K 15 /GS1 308 0 R >> /dotlessi /lslash /oe /scaron /zcaron 160 /Euro 164 /currency 166 >> /Pg 24 0 R 14 0 obj /Pg 35 0 R /K 1 /P 17 0 R /Lang (EN-GB) 196 0 obj 256 0 obj >> << >> /Fm0 295 0 R /quotesingle 96 /grave 128 /bullet /dagger /daggerdbl /ellipsis /emdash /endash << /S /Tabelle_content /P 17 0 R >> endobj << << /P 517 0 R /XObject << /K 78 /S /Normal << /ExtGState << /P 543 0 R /A 413 0 R /Count 4 http://www.zotero.org/styles/modern-language-association /Pg 26 0 R >> /Rotate 0 /Pg 35 0 R As such, they can absorb vibration that would normally be transferred by steel bearings. Contrary to fixed-wing aircraft there is a wider and more heterogeneous design space. /XObject << What type of design is used on many Navy helicopters? /Pg 35 0 R /PDFDocEncoding 8 0 R /Type /Outlines >> At 1001hobbies, we share your p /TT0 303 0 R /TT0 310 0 R /A 557 0 R /K 6 /XObject << /Contents [277 0 R 278 0 R 279 0 R 280 0 R 281 0 R 282 0 R 283 0 R 284 0 R 285 0 R 286 0 R] /K 33 >> /Tabs /S /ProcSet [/PDF /Text] 236 0 obj /A 596 0 R endobj 183 0 obj /Lang (EN-US) /K 3 7 0 obj /Pg 25 0 R /Contents 367 0 R /K 182 >> endobj << << /A 411 0 R 244 0 obj >> /Mendeley#20Recent#20Style#20Id#208_1 (http://www.zotero.org/styles/modern-language-association) /Pg 42 0 R /K 90 >> /Pg 35 0 R >> /S /Tabelle_content endobj /K 62 /GS2 309 0 R << /TT0 310 0 R /K 6 endobj << /A 674 0 R << /K 163 /ProcSet [/PDF /Text /ImageC] /Lang (EN-GB) /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /MarkInfo << /A 531 0 R /Pg 35 0 R /Sh1 316 0 R endobj The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. /Pg 35 0 R /Rotate 0 /S /Span /P 423 0 R >> /P 633 0 R /GS0 307 0 R 0 52 0 obj 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. 84 0 obj /Parent 13 0 R /P 49 0 R >> What does the helicopter fuselage consist of? 48 0 obj /Pg 35 0 R /S /P /K 152 /GS0 288 0 R /Lang (EN-GB) /P 612 0 R << /MediaBox [0.0 0.0 595.32 841.92] >> A NOTAR antitorque system has no visible rotor mounted on the tail boom. /K 140 /Pg 35 0 R /Pg 35 0 R /K 146 CONTROLLED FLAMBING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT. Acrobat PDFMaker 17 for Word >> << endobj >> /A 551 0 R /Sh10 340 0 R Thankfully, Igor Sikorsky had the idea to install a tail rotor to counter this torque reaction and provide directional control. The large rotating mass of the main rotor blades of a helicopter produce torque. >> /K << /Pg 33 0 R endobj /ExtGState << << The rotor consists of a mast, hub, and rotor blades. /Superscript /Span /P 73 0 R /S /Normal /Pg 35 0 R endobj /ProcSet [/PDF /Text /ImageC] /Lang (EN-GB) >> endobj 249 0 obj >> >> /A 444 0 R /Sh7 325 0 R /P 601 0 R endobj >> endobj >> /K 11 /Pg 35 0 R /S /Artifact endobj Please refer to our privacy policy for further information. 108 0 obj Fuselage The main body of the helicopter is known as the fuselage.
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