helicopter frames consist of the fuselage

13 0 obj 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 /A 546 0 R /K 3 /P 512 0 R >> 175 0 obj /Strikeout /Span << /Encoding << /CropBox [0.0 0.0 595.32 841.92] /Title (7. << /K 110 A NOTAR antitorque system has no visible rotor mounted on the tail boom. 277 0 obj << /CS1 [/ICCBased 306 0 R] /Pg 35 0 R /K 173 /Pg 33 0 R /Type /Pages endobj /ParentTree 18 0 R /Lang (EN-GB) -rotary rudder counteracts torque developed by the rotor head. /Mendeley#20Recent#20Style#20Id#204_1 (http://www.zotero.org/styles/chicago-author-date) 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. /MediaBox [0.0 0.0 595.32 841.92] << /S /Tabelle_content /TT0 313 0 R Some modern helicopter main rotors have been designed with flextures. 80 0 obj <>stream << /S /Tabelle_content << /S /Normal /Pg 42 0 R << /S /Normal /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 /P 17 0 R >> /ProcSet [/PDF /Text] /Pg 35 0 R 148 0 R null 149 0 R 150 0 R 151 0 R 152 0 R 153 0 R null 154 0 R null /Count 0 /Fm0 295 0 R /A 408 0 R 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 73 0 R The structural system, or frame, is similar to the fuselage of an airplane. 3218 Kalle Saastamoinen et al. /Rotate 0 endobj 1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6 /A 672 0 R 170 0 obj << /XObject << /A 380 0 R /MarkInfo << /Pg 43 0 R >> /K [44 0 R 45 0 R 46 0 R 47 0 R 48 0 R 49 0 R 50 0 R 51 0 R 52 0 R 53 0 R /ProcSet [/PDF /Text /ImageC] The rotor consists of a mast, hub, and rotor blades. /S /Subscript /Lang (EN-GB) >> /MediaBox [0.0 0.0 595.32 841.92] 251 0 obj /P 563 0 R /K 1 >> 257 0 obj /K 5 In front and center of the pilot's and co-pilot's seats (interconnected). /S /P /Fm4 299 0 R /CS1 [/ICCBased 306 0 R] /P 17 0 R >> /Pg 35 0 R A few models have skids with two ground-handling wheels. 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. /Pg 43 0 R /S /Tabelle_content 18 0 obj >> /A 511 0 R /Kids [24 0 R 25 0 R 26 0 R 27 0 R] /Type /Page 45 0 obj endobj /Pg 41 0 R /Next 12 0 R >> << /A 397 0 R /Superscript /Span /Pg 35 0 R << The tail boom and tail rotor, or antitorque rotor, counteract this torque effect. /D [41 0 R /XYZ 104 373 0.0] endobj >> << 156 0 obj Fuselage. >> The tip path plane tilts forward, moving the helicopter forward. >> /S /Tabelle_content /Font << /Parent 5 0 R /K 9 Products include fuselages, wings, empennages, nacelles and helicopter cabins. /S /Artifact Helicopter cabins have a variety of seating arrangements. >> /Name /ZaDb /A 531 0 R 255 0 obj endobj /Lang (EN-GB) /GS1 308 0 R by | Jun 10, 2022 | durham university sports and societies | northstar refrigerator reviews | Jun 10, 2022 | durham university sports and societies | northstar refrigerator reviews /P 648 0 R 243 0 obj /Lang (EN-GB) /P 588 0 R /K 118 >> /ExtGState << >> << /S /Tabelle_content /TT3 314 0 R [Figure 1-13] Helicopter airframes consist of the fuselage, main rotor and related gearbox, tail rotor (on helicopters with a single main rotor), and the landing gear. >> << 195 0 obj 186 0 obj endobj /P 17 0 R /Resources << /Parent 14 0 R /ColorSpace << endobj /Pg 33 0 R The horizontal and vertical tails are rigidly attached to the fuselage as indicated. >> /Subtype /Type1 << endobj 108 0 obj << endobj /P 17 0 R /TT4 314 0 R [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. /P 17 0 R /S /Tabelle_content /P 17 0 R /Metadata 3 0 R /Tabs /S /K 83 21 0 obj /Pg 41 0 R /Pg 35 0 R /Pg 35 0 R 51 0 obj /CropBox [0.0 0.0 595.32 841.92] Some of the forces acting on a wing spar are: Upward bending loads resulting from the wing lift force that supports the fuselage in flight. /K [8 264 0 R] >> 46 0 obj /Pg 35 0 R /A 598 0 R >> << /MediaBox [0.0 0.0 595.32 841.92] %PDF-1.3 /K [5 120 0 R] << required input parameters up to the structural analysis of the fuselage. 53 0 obj The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. >> 88 0 obj What is the purpose of the cyclic control stick? /P 423 0 R /Rotate 0 126 0 obj /GS2 309 0 R /StructParents 17 /TT0 290 0 R << /Im0 330 0 R /Sh10 340 0 R endobj /Lang (EN-GB) >> /Parent 15 0 R /quotesingle 96 /grave 128 /bullet /dagger /daggerdbl /ellipsis /emdash /endash /Fm1 296 0 R >> 55 0 obj >> /S /Sect 93 0 obj /ExtGState << endobj /K [16 268 0 R 269 0 R] /CropBox [0.0 0.0 595.32 841.92] 19 [112 0 R 271 0 R null 113 0 R 114 0 R 115 0 R 116 0 R 117 0 R 118 0 R 272 0 R /A 539 0 R /Mendeley#20Citation#20Style_1 (http://www.zotero.org/styles/harvard1) /S /Tabelle_content /Rotate 0 << /Mendeley#20Recent#20Style#20Name#207_1 (Modern Humanities Research Association 3rd edition \(note with bibliography\)) /A 493 0 R >> /Lang (EN-GB) 81 0 obj /MediaBox [0.0 0.0 595.32 841.92] /A 661 0 R 31 0 obj ciusss sud ouest; city of kent wa noise ordinance hours; what is the main idea of the albertosaurus mystery; mackenzie bezos new husband age endobj >> /K 124 /Lang (EN-US) With this hinge, when one blade flaps up, the other flaps down. /DropCap /Figure 196 0 obj /Pg 24 0 R /Pg 35 0 R /GS0 288 0 R >> /P 109 0 R /A 652 0 R /K 51 /A 548 0 R 190 0 obj << /K 126 This is in contrast with helicopters or other rotary wing ight vehicles that generate lift using rotating blades. >> It features frames designed to create the shell of the fuselage, which are secured via cross sections on a rigid fixture. /P 17 0 R 12 [82 0 R 83 0 R 84 0 R 85 0 R 86 0 R 87 0 R] endobj /P 17 0 R /Lang (EN-GB) 96 0 obj The cyclic, or "stick," comes out of the floor of the cockpit and sits between the pilot's legs, enabling a person to tilt the craft to either side or forward and backward. >> /Fm1 296 0 R endobj /Oslash /Ugrave /Uacute /Ucircumflex /Udieresis /Yacute /Thorn /germandbls /agrave /aacute << /K 13 179 0 obj >> /S /Tabelle_content >> >> True /A 520 0 R /Rotate 0 116 0 obj endobj If the day is already the end /Shading << << /Lang (EN-GB) >> endobj /P 541 0 R /ProcSet [/PDF /Text /ImageC] /Sh0 315 0 R /TT3 313 0 R >> /Pg 35 0 R /A 591 0 R << /S /P 9 [73 0 R 74 0 R 75 0 R 76 0 R 77 0 R 127 0 R 73 0 R 128 0 R 73 0 R 129 0 R One or more horizontal hinges provide for flapping on a fully articulated rotor system. American Psychological Association 6th edition /Tabs /S /Pg 35 0 R /ColorSpace << /P 433 0 R /igrave /iacute /icircumflex /idieresis /eth /ntilde /ograve /oacute /ocircumflex /otilde /Resources << /Lang (EN-GB) /P 17 0 R /TT1 312 0 R << /ProcSet [/PDF /Text] /A 515 0 R << << /Resources << /P 572 0 R /A 405 0 R /CS0 [/ICCBased 287 0 R] Acrobat PDFMaker 17 for Word /Font << << Enthusiats at your service : at 1001hobbies, we share yo >> /Type /Page 168 0 obj >> /ColorSpace << /Lang (EN-GB) - 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 whole body frame is made of an FE beam structure 4 with a cross-section of 0.22410 3 m 2, while the lift section (around the fuselage to support hub and fuselage) and the tail section are thicker, 0.910 3 and 1.492310 3 m 2 respectively, offering stronger support. Panels were made with the same geometrical shape and dimensions but . The aircraft is made up of an airframe, specifically fuselage, booms, nacelles, cowlings, fairings, airfoil surfaces, and landing gear. 59 0 obj >> >> >> endobj /Resources << /Pg 35 0 R >> 72 0 obj /Lang (EN-GB) /StructParents 2 >> /K 156 /K [1 265 0 R] /S /Title /BaseFont /ZapfDingbats /S /Artifact << 220 0 obj << endstream endobj 53 0 obj <> endobj 54 0 obj <>/Font<>/ProcSet[/PDF/Text]/Properties<>>>/Rotate 0/Type/Page>> endobj 55 0 obj <>stream << >> /K 6 << Special Offer on Antivirus Software From HowStuffWorks and TotalAV Security. /P 576 0 R /Lang (EN-GB) /P 49 0 R >> /P 610 0 R << /P 581 0 R /S /P /Type /Page /Lang (EN-GB) Airframe design encompasses engineering. Please refer to our privacy policy for further information. >> endobj /Icircumflex /Idieresis /Eth /Ntilde /Ograve /Oacute /Ocircumflex /Otilde /Odieresis /multiply /K 61 << /P 660 0 R /K 85 endobj 250 0 obj Numerous designs and variations on the three types of main rotor systems exist. -produces thermal or heat energy to drive power turbine, Front frame 181 0 obj /S /Normal endobj Introduction The design of a new rotorcraft is generally considered as a highly challenging task. /CS0 [/ICCBased 287 0 R] /MediaBox [0.0 0.0 595.32 841.92] /S /P >> /florin /fraction /guilsinglleft /guilsinglright /minus /perthousand /quotedblbase /quotedblleft /quotedblright /quoteleft /K 9 /Lang (EN-GB) /Mendeley#20Document_1 (True) /Lang (EN-US) /A 629 0 R << /Pg 41 0 R /P 612 0 R /Pg 35 0 R /K 4 150 0 obj /TT2 329 0 R /Lang (DE-DE) /Pg 35 0 R /Sh9 327 0 R In addition, the purpose of an airplane goes a long way in the manufacturers' decision to use a particular type of metal, especially the metal used in the plane's frame and body. endobj gearbox >> /ColorSpace << /P 424 0 R /A 401 0 R /K 69 /A 480 0 R >> /Pg 35 0 R null] /K 2 /K 0 /K 48 What are the values of the SHGC and SC of a single-pane clear-glass window? By - June 6, 2022. /Font << /Pg 35 0 R /Contents 337 0 R helicopter frames consist of the fuselagetaylor phillips model age. /TT2 313 0 R >> >> In the late 1920s and early 1930s, airplane manufacturers started producing more fuselages from aluminum and steel. 142 0 obj /Encoding 8 0 R /Lang (EN-GB) endobj 216 0 obj << For design and analysis, engineers group parts which have the same function into systems. /CropBox [0.0 0.0 595.32 841.92] << 208 0 obj 177 0 R null 178 0 R null 179 0 R 180 0 R 181 0 R 182 0 R 183 0 R null /S /P /Pg 35 0 R D. Schwinn, P. Weiand, M. Schmid << /Pg 30 0 R >> /Lang (EN-GB) 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 endobj /Pg 35 0 R Thin sheets of the material can be stacked in various ways to meet specific strength or . /Rotate 0 >> /S /Normal endobj 17 0 obj Graphite-epoxy is one of several types of composite materials that are becoming widely used for many aircraft structures and components. /Lang (EN-GB) /Lang (EN-GB) 73 0 R 130 0 R 73 0 R 131 0 R 73 0 R 132 0 R 73 0 R 133 0 R 73 0 R 134 0 R , " "" ( " ""), Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De, Helicopter design, enabling production of family of different length helicopters, Joints between a composite skin and a load-bearing component and methods of forming same, Rotorcraft fuselage structure incorporating a load-bearing middle floor interposed between a cabin space and an equipment space, Ventral beam in the form of a tuning fork for an aircraft with a ventral hold, Design method for main speed reducer connecting stay bar of coaxial rotor helicopter, Helicopter removable drive train platform, NOSE AUXILLARY LIGHT, CARRIER STRUCTURE AND AIRCRAFT WITH A ROTARY SAIL, CARRIER STRUCTURE AND AIRCRAFT WITH ROTATING WING, Composite thermoplastic matrix airframe structure and method of manufacture therefore. /Count 6 >> /Lang (EN-GB) Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment 182 0 obj /ProcSet [/PDF /Text] /S /P << >> /K 41 /Lang (EN-GB) endobj /Mendeley#20Unique#20User#20Id_1 (1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6) In a pressurized aircraft the skin works with the frames to oppose the internal pressure load. /Pg 35 0 R /CS1 [/ICCBased 306 0 R] /Pg 35 0 R >> 264 0 obj /Contents 302 0 R endobj /A 444 0 R 235 0 obj /S /Artifact 44 0 obj 211 0 obj Single Rotor. /K 182 >> /TT2 311 0 R /S /Artifact Large frames are required at the wing-fuselage and tail-fuselage interface to transmit the loads generated by these lifting surfaces into the fuselage. /TT0 303 0 R << /K 13 /K [2 119 0 R] /P 617 0 R /Lang (EN-GB) /P 17 0 R /S /Normal >> endobj /Parent 5 0 R /Pg 41 0 R 146 0 obj << endobj /Lang (EN-GB) /ExtGState << /P 556 0 R /Fm4 299 0 R /Lang (EN-GB) /P 601 0 R endobj 176 0 obj << >> /P 17 0 R /Lang (EN-GB) /CS0 [/ICCBased 287 0 R] << /Pg 42 0 R -effective to a height of approximately half the rotor diameter endobj << 83 0 obj /A 600 0 R endobj /Parent 14 0 R /A 275 0 R 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. /Lang (EN-US) /Pg 43 0 R uuid:1829709f-1569-4b41-ae83-38410010e776 Please copy/paste the following text to properly cite this HowStuffWorks.com article: Tom Harris & Talon Homer << /Fm2 297 0 R /S /Span Water lines (WL) designate location in the height of the aircraft, from ground up. /A 412 0 R /Lang (EN-US) /ExtGState << /P 17 0 R The fuselage also houses the engine, the transmission, avionics, flight controls, and the powerplant. endobj /Sh11 318 0 R Tilting the rotor plane of rotation causes the aircraft to move horizontally. /D [25 0 R /XYZ 104 520 0.0] >> endobj /P 535 0 R /Lang (EN-GB) /K 74 /P 537 0 R /Parent 14 0 R 1. /S /Normal /P 17 0 R . << << /Fm3 298 0 R /S /Tabelle_content >> /MediaBox [0.0 0.0 595.32 841.92] /Fields [] /MediaBox [0.0 0.0 595.32 841.92] /Sh8 356 0 R >> << /Lang (EN-GB) 143 0 obj >> /Pg 35 0 R >> /Pg 24 0 R /Mendeley#20Recent#20Style#20Name#203_1 (American Sociological Association) >> -rotation about this axis is called YAW and is controlled by anti-virus pedals, -Runs from one side of the Aircraft to the other side /P 73 0 R /P 554 0 R /XObject << /Mendeley#20Recent#20Style#20Name#205_1 (Harvard Reference format 1 \(author-date\)) /degree /plusminus /twosuperior /threesuperior /acute /mu 183 /periodcentered /cedilla /onesuperior 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. /MediaBox [0.0 0.0 595.32 841.92] endobj /K 6 /Lang (EN-GB) endobj Figure 1 shows the major components of a typical helicopter. A typical helicopter fuselage structure shown in Fig 1 consists of several key components: (a) Subfloor box, (b) Energy absorbing beam, (c) Box beam frame members, (d) Longitudinal beam, and (e) Outer fuselage skin. /P 528 0 R /Pg 35 0 R Fuselage The main body of the helicopter is known as the fuselage. /Im0 359 0 R /Lang The wings and tail section are attached to the fuselage, and depending on the design of the aircraft, may include engine attachments too. /Pg 35 0 R 198 0 obj /XObject << /MediaBox [0.0 0.0 595.32 841.92] /P 17 0 R All these load cases, and the interaction between cases must be considered to arrive at a final design. /A 471 0 R /MediaBox [0.0 0.0 595.32 841.92] 171 0 obj endobj Adobe PDF Library 15.0 80 0 obj /RoleMap 19 0 R /K [185 442 0 R] /K 67 << << /S /Artifact /K [12 267 0 R] endobj /S /P >> /K 152 consist of: [phrasal verb] to be formed or made up of (specified things or people). 135 0 obj /S /Tabelle_content /Lang (DE-DE) passenger, has fuselage with straight sections whose maximal height is continuously evolved between maximal height of central zone in connection section and reduced end height at concerned edge of fuselage, Storage compartment for the nose gear of an aircraft, Frame for an opening provided in an aircraft fuselage, Method to increase the safety in air transportation, AIRCRAFT COMPRISING A PASSENGER CAB EXTENDING A SPACE EXTERIOR TO THE CABIN PROVIDED WITHIN THE AIRCRAFT, FUSELAGE AIRCRAFT PROVIDED WITH SIDE EXCREASES DELIMINATING STORAGE SPACES, Aircraft turbine engine assembly comprising a hinged cover, Module for front landing gear for an aircraft, Rotorcraft equipped with fuel reservoirs mounted suspended under a load carrying median floor of the rotorcraft fuselage, REAR AIRCRAFT PART PROVIDED WITH SUPPORT STRUCTURE OF OPTIMIZED SHAPE ENGINES, Utility vehicle cabin comprises lattice work structure forming chassis on which protection, insulation and bodywork elements are fixed, Public reference made under article 153(3) epc to a published international application that has entered the european phase, Gb: translation of ep patent filed (gb section 77(6)(a)/1977), Reply of patent proprietor to notice(s) of opposition, Nl: opposition has been filed with the epo, Party data changed (patent owner data changed or rights of a patent transferred), Nl: modifications (of names), taken from the european patent patent bulletin, Nl: modifications of names registered in virtue of documents presented to the patent office pursuant to art. 1. iis express not working with ip address. 246 0 obj /CS0 [/ICCBased 287 0 R] /K << /P 530 0 R /ViewerPreferences << /P 628 0 R /Pg 24 0 R 261 0 obj /SourceModified (D:20170502160949) /CS0 [/ICCBased 287 0 R] 41 0 obj -mechanically connected to the main transmission gearbox through a main driveshaft, Transmits torque from the power turbine to the main gearbox and is dynamically balanced, Main transmission gearbox /StructParents 0 /TT1 333 0 R /StructParents 9 /Pg 35 0 R << >> /P 658 0 R 48 0 obj /S /Normal Additionally, a horizontal member called a stabilizer is often constructed at the tail cone or on the pylon. /XObject << /P 256 0 R << endobj /P 47 0 R << /A 571 0 R /K 171 /Endnote /Note /K 140 /K 166 /K 30 endobj /P 46 0 R >> << /S /Tabelle_content /Font << >> /P 17 0 R During the early days of aviation, primitive fuselages were built with wood. /P 590 0 R >> [Figure 7]. /GS0 307 0 R 242 0 obj /TT0 313 0 R 7 0 obj hbbd``b` /Sh17 347 0 R << Acknowledgements) 114 0 obj /Lang (EN-GB) /S /Normal /Pg 30 0 R /A 589 0 R /Lang (EN-GB) /P 630 0 R /P 532 0 R /P 517 0 R /Sh5 323 0 R Landing loads introduced into the fuselage can be particularly severe if the landing is executed poorly. >> << /A 455 0 R /K 12 /P 17 0 R 69 0 obj endobj /Pg 42 0 R /A 650 0 R endobj stream >> /Lang (EN-GB) /Count 4 ] /Lang (EN-GB) /Resources << /A 460 0 R /Rotate 0 /K 50 /Pg 35 0 R /Pg 41 0 R endobj /Pg 35 0 R /S /Normal /S /Normal In twin-rotor helicopters, the torque produced by the rotation of the front rotor is offset by the torque produced by a counter-rotating rear rotor. /CS1 [/ICCBased 306 0 R] /Parent 4 0 R /K 27 . The fuselage generates its own aerodynamic loads during flight which must be reacted by the structure. endobj 165 0 obj /S /Tabelle_content /K 107 /ColorSpace << helicopter frames consist of the fuselage. /S /P 71 0 obj /Sh10 317 0 R /K 102 /CropBox [0.0 0.0 595.32 841.92] 237 0 obj /Lang (EN-GB) /Pg 42 0 R /P 577 0 R >> endobj /Rotate 0 /Lang (EN-GB) /P 552 0 R << /Contents 379 0 R endobj Tail boom The tail boom extends out from the rear of the fuselage and holds the tail rotor assemblies. /P 494 0 R >> /Fm3 298 0 R endobj Customer satisfaction 4,2/5. 115 0 obj << /K 4 /K 80 >> 259 0 obj 75 0 obj /K 3 << /Lang (EN-GB) endobj /Pg 41 0 R 74 0 obj /ProcSet [/PDF /Text] /P 17 0 R Rotary wing aircraft which obtains lift and thrust from mechanically driven airfoils. /A 454 0 R /K 121 0 R /A 468 0 R /S /Tabelle_content /Lang (EN-GB) /Title (1. In the next section, we'll peer at the rotor assembly of a typical helicopter. endobj >> /P 631 0 R /K 142 /Parent 16 0 R -Can be thought of as the Aircraft pivot pts. /Lang (EN-GB) /A 382 0 R /TT1 291 0 R >> 1. endobj /Pg 30 0 R /K 11 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. >> endobj endobj endobj /K 46 /Fm1 296 0 R >> /Mendeley#20Recent#20Style#20Id#206_1 (http://www.zotero.org/styles/ieee) /A 620 0 R >> /P 510 0 R FRAME FUSELAGE STATION 177.2 (Drawing 143F079) The frame at Fuselage Station 177.2 functions as a stiffening member for the fuel cell liner. >> /P 507 0 R /StructParents 19 Monocoque endobj << >> /K 183 /S /Tabelle_content endobj Many military and reconnaissance planes today are made from titanium or . /P 17 0 R /Contents 360 0 R /P 543 0 R endobj << /Lang (EN-US) /ExtGState << /P 17 0 R The loading consists of Internal pressure applied by the fuel. >> /brokenbar 168 /dieresis /copyright /ordfeminine 172 /logicalnot /.notdef /registered /macron /P 579 0 R /XObject << /Lang (EN-US) 234 0 obj Introduction) /K 100 /CS1 [/ICCBased 306 0 R] /A 659 0 R endobj Top customer satisfaction 4,2/5. << /Title (6. endobj >> /S /Tabelle_content >> << /A 638 0 R /TT1 311 0 R << 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 Definition of a Helicopter. << 214 0 R null 215 0 R 216 0 R 217 0 R 218 0 R 219 0 R null 220 0 R null /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] >> The heavier the helicopter, the bigger the engine/s which requires a stronger fuselage. Determine the suitable material for each of the component. >> /ExtGState << /S /Tabelle_content >> /A 381 0 R The skins ability to carry and transmit shear is reduced if the skin is allowed to buckle; this forms a constraint that determines the spacing of the stringers and frames. /K 10 /S /Tabelle_content /S /P /P 646 0 R /Pg 35 0 R /XObject << >> << /S /Heading#201 /K 4 /TT0 290 0 R /P 17 0 R /Lang (EN-GB) /Pg 41 0 R /Type /Font /A 524 0 R /GS0 307 0 R /ColorSpace << 266 0 R null 107 0 R 267 0 R null 108 0 R 109 0 R 268 0 R null 269 0 R

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