/CS1 [/ICCBased 306 0 R] consist of: [phrasal verb] to be formed or made up of (specified things or people). >> /K 147 /P 438 0 R /Contents 377 0 R endobj /K [8 272 0 R] /Type /Font >> /S /Tabelle_content >> 221 0 obj >> /Type /Page -the center of pressure movement is limited, which makes it very desirable on helicopters, -Center of pressure is variable on this type of airfoil /ExtGState << >> 130 0 obj /Pg 24 0 R 75 0 obj endobj >> >> /K 6 The UH-1B is a real workhorse utility helicopter which can pack a punch with several different weapons load-outs and configurations utilising rockets, guns and missiles. endobj /Artifact /P /Contents 369 0 R /Mendeley#20Recent#20Style#20Id#204_1 (http://www.zotero.org/styles/chicago-author-date) /XObject << /Pg 42 0 R endobj /P 17 0 R endobj >> /Lang (EN-GB) /Fm0 295 0 R /brokenbar 168 /dieresis /copyright /ordfeminine 172 /logicalnot /.notdef /registered /macron /S /Tabelle_content /Lang (EN-GB) 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. 238 0 obj /P 17 0 R /Contents 331 0 R /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) It holds crew, passengers, or cargo.In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft the single engine is mounted on a pylon attached to the fuselage, which in turn is used as a floating hull. 197 0 obj >> /ProcSet [/PDF /Text /ImageC] /TT3 314 0 R /Type /Page /Underline /Span /Lang (EN-GB) /S /Normal 260 0 obj -lost at air speeds above 10mph, -additional lift obtained when entering horizontal flight due to increased efficiency of rotor system. /S /Normal /Title (4. /Lang (EN-GB) /P 17 0 R >> /Pg 35 0 R << /Pg 35 0 R Numerous designs and variations on the three types of main rotor systems exist. 174 0 obj null 170 0 R 171 0 R null 172 0 R null 173 0 R 174 0 R 175 0 R 176 0 R >> /Parent 16 0 R /S /Normal /CS0 [/ICCBased 287 0 R] /K 5 << << /K 2 endobj /Pg 35 0 R >> /Pg 43 0 R 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. /Fm4 299 0 R >> Where is the cyclic control stick located? /S /Tabelle_content /Lang (DE-DE) /TT1 289 0 R /P 17 0 R >> endobj areas are at the fuselage upper part and at the joints of the fuselage frames to the wing spars. 117 0 obj /S /Artifact << 236 0 obj 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] /K 7 << /P 608 0 R << /S /Normal >> >> >> /S /Tabelle_content /Oslash /Ugrave /Uacute /Ucircumflex /Udieresis /Yacute /Thorn /germandbls /agrave /aacute /ProcSet [/PDF /Text /ImageC] 153 0 obj >> /K 156 << /Font << 2. 24 0 obj Lugs are the most widely used connecting elements in aircraft. /S /Normal /Marked true endobj /S /Normal << << /K 1 437 0 R 438 0 R] /ColorSpace << << /Pg 35 0 R /S /Tabelle_content 100 0 obj /ZaDb 10 0 R endobj endobj /K 3 /S /P endobj >> 149 0 obj /K 180 Here we are only going to consider the semi-monocoque design philosophy, and how it relates to the fuselage structure. /Fm4 299 0 R /Lang (EN-GB) /Type /Page >> >> << 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. >> /Lang (EN-GB) /S /Tabelle_content /P 17 0 R /Pg 35 0 R /ColorSpace << /Pg 24 0 R /K 11 /P 631 0 R endobj /P 497 0 R /P 17 0 R /A 480 0 R /K 68 /TT1 313 0 R /Type /StructTreeRoot << /K 4 /K 35 /S /P /P 521 0 R In some models, the tail boom is nothing more than an aluminum frame. /K 165 200 0 obj >> /S /GoTo /S /Normal >> /GS0 288 0 R /A 641 0 R 82 0 obj >> endobj endobj << /Lang (EN-GB) /K 130 /K 3 The attachment bracket, also known as a wing box, consists of a lug and a portion of spar connected with several bolts. /Prev 21 0 R 210 0 obj 269 0 obj Two critical conditions are considered; horizontal crash landing and 6 g maneuver. /Lang (EN-GB) 211 0 obj /P 639 0 R /ExtGState << The tip path plane tilts forward, moving the helicopter forward. << 1 0 obj endobj /S /Tabelle_content /Type /Page endobj /First 11 0 R Customer satisfaction 4,2/5. /Metadata 3 0 R << endobj << /Tabs /S /A 406 0 R Typically, a composite component consists of many layers of fiber-impregnated resins, bonded to form a smooth panel. 11 0 obj /CS1 [/ICCBased 306 0 R] endobj /Lang (EN-GB) /Fm4 299 0 R /CropBox [0.0 0.0 595.32 841.92] << /Lang (EN-GB) 80 0 obj /P 17 0 R /Contents 372 0 R /Pg 42 0 R /Pg 30 0 R /formula /P /K 174 /A 627 0 R /S /Span /MediaBox [0.0 0.0 595.32 841.92] The company's customer base consists of the world's leading aerospace OEMs, and more than 80 percent of its . 14 132 0 R 16 133 0 R 18 134 0 R 20] /Fm1 296 0 R >> /K 5 endobj The wings and tail section are attached to the fuselage, and depending on the design of the aircraft, may include engine attachments too. /S /Span /Sh14 344 0 R /Title (Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment) $\begingroup$ @mins No, that's not even close. /Count 0 60 0 obj If you missed part one, then perhaps go back and read this before continuing as this provides an overview on structural loading and design. /Lang (EN-GB) 25 0 obj /ProcSet [/PDF /Text /ImageC] /Pg 42 0 R >> /K 76 >> The structural system, or frame, is similar to the fuselage of an airplane. /ProcSet [/PDF /Text /ImageC] /P 669 0 R fuselage: [noun] the central body portion of an aircraft designed to accommodate the crew and the passengers or cargo see airplane illustration. /Pg 33 0 R << /K << /S /Tabelle_content helicopter frames consist of the fuselage. endobj /Im1 374 0 R /Sh11 341 0 R These rotors are usually made of a composite structure. >> /Pg 35 0 R /K 9 /Lang (EN-GB) >> endobj 246 0 obj 3 0 obj /Fm1 296 0 R /A 20 0 R 207 0 R null 208 0 R null 209 0 R 210 0 R 211 0 R 212 0 R 213 0 R null /S /P << << >> 252 0 obj /K 77 >> 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. << /Type /Page /ProcSet [/PDF /Text] /Pg 42 0 R /XObject << >> /Fm4 299 0 R /Lang (EN-GB) /Resources << /Lang (EN-GB) /S /P >> /ColorSpace << 46 0 obj /Title /H1 endobj /K 122 /Pg 42 0 R /A 414 0 R /Pg 43 0 R 31 0 obj -through the use of a freewheeling unit, located w/in main gearbox assembly, Stops rotation of rotor head /GS0 307 0 R endobj endobj /S /Tabelle_content /Lang (EN-GB) << /Encoding << /P 434 0 R /Font << /K 88 127 0 obj /Lang (EN-GB) Foot pedals A pair of foot pedals controls the tail rotor. 84 0 R 85 0 R 86 0 R 87 0 R 88 0 R 89 0 R 90 0 R 91 0 R 92 0 R 93 0 R >> /S /Normal >> 7 0 obj >> The skins carry load through shear and transmit this shear into the stiffeners. /Lang (EN-GB) 62 0 obj /K 90 /Lang (EN-GB) << 2017-05-08T21:10:34+01:00 /Sh10 317 0 R /GS0 288 0 R Nature http://www.zotero.org/styles/american-medical-association /A 493 0 R /S /formula /K [184 263 0 R 188] In others, it's a hollow carbon-fiber or aluminum tube. 4 0 obj /ColorSpace << Most have the pilot seated on the right side, although there are some with the pilot seated on the left side or center. /Pg 35 0 R 57 0 obj endobj endobj 244 0 R null 245 0 R 246 0 R 247 0 R 248 0 R 249 0 R null 250 0 R null /P 535 0 R << /Lang (EN-GB) /Pg 35 0 R >> >> /Im0 330 0 R /S /Normal /P 17 0 R /PageLayout /SinglePage /A 566 0 R /CS1 [/ICCBased 306 0 R] At 1001hobbies, we share your p endobj << endobj Free shipping above 99. 182 0 obj "How Helicopters Work" /K 22 /XObject << /ProcSet [/PDF /Text /ImageC] /XObject << -sections: gas generator, power turbine, main drive shaft, -may be axial flow or combined axial/centrifugal flow gas turbine engine 105 0 obj /Lang (EN-GB) /A 485 0 R /Sh8 326 0 R 181 0 obj /Type /Catalog /Pg 35 0 R endobj /Pg 35 0 R >> << >> -as the angle of attack increases, canter of pressure moves forward along the airfoil surface 256 0 obj /P 17 0 R /TextBox /Art Water lines (WL) designate location in the height of the aircraft, from ground up. endobj endobj /Pg 35 0 R For example, during takeoff, the pilot uses the collective-pitch lever to increase the pitch of all the rotor blades by the same amount. /Lang (EN-GB) 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. << /S /Normal /Lang (EN-US) 277 0 obj /P 17 0 R /Fm4 299 0 R 133 0 obj 29 0 obj /P 592 0 R /Pg 24 0 R /A 598 0 R /Sh6 354 0 R << >> /Lang (EN-GB) /Lang (EN-GB) /Pg 35 0 R /Pg 30 0 R /TT1 313 0 R Normally, it supports the tail rotor assembly, although some tail rotors are mounted on the tail cone of the boom. /D [41 0 R /XYZ 104 267 0.0] /A 629 0 R /Sh5 323 0 R The fuselage does more than just house the occupants of the aircraft; it must be sized and designed to ensure that the wings and tail are positioned in such a way so as to keep the aircraft statically stable through the designed center of gravity envelope. /S /Normal << /Sh17 347 0 R 274 0 obj /P 549 0 R /Lang (EN-GB) 36 0 obj endobj /Producer (Adobe PDF Library 15.0) /Type /Pages From Wikipedia." airplane model kit at the price of 83.99 GBP with 1001hobbies, the AModel specialist. 9 0 obj 12 [82 0 R 83 0 R 84 0 R 85 0 R 86 0 R 87 0 R] /Title (3. One or more horizontal hinges provide for flapping on a fully articulated rotor system. /TT1 289 0 R /A 513 0 R << /P 514 0 R /Mendeley#20Document_1 (True) /A 398 0 R /Pg 35 0 R /A 400 0 R One of the helicopters came down and major components/assemblies were recovered . endobj << endobj /Lang (EN-GB) /K 24 /P 256 0 R << Torque, another problem associated with the physics of a rotating wing, causes the helicopter fuselage (cabin) to rotate in the opposite direction from the rotor, especially when the helicopter is moving at low speeds or hovering. >> endobj http://www.zotero.org/styles/american-sociological-association /Subtype /Type1 endobj /Lang (EN-GB) /Fm2 297 0 R /P 662 0 R /Lang (EN-US) nafems noble soccer tournament 2021 how to get gems in phase 10: world tour army covid pt test policy helicopter frames consist of the fuselage. /Type /Page endobj /TT0 290 0 R >> /A 393 0 R 5 0 obj /P 501 0 R /P 530 0 R >> /S /Tabelle_content >> >> >> 83 0 obj << /Pg 35 0 R << /K [185 442 0 R] >> endobj /Pg 35 0 R /StructParents 0 /A 452 0 R /Type /MCR Their primary aim is to transmit the axial loads (tension and compression) that arise from the tendency of the fuselage to bend under loading. /P 436 0 R /Pg 42 0 R endobj 167 0 obj /K 149 /C2_0 332 0 R 155 0 obj >> << Gas generator turbine The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. 55 0 obj /A 483 0 R << endobj /P 112 0 R /Lang (EN-GB) / Procedia Computer Science 176 (2020) 3217-3224 2 Author name / Procedia Computer Science 00 (2020) 000-000 1. /Type /Page << As such, they can absorb vibration that would normally be transferred by steel bearings. endobj >> /P 49 0 R /Tabs /S /A 410 0 R endobj >> endobj endobj << 106 0 obj /P 73 0 R 99 0 obj /P 17 0 R /K 13 /A 650 0 R The rotor consists of a mast, hub, and rotor blades. /Sh0 338 0 R /ExtGState << >> /Lang (EN-US) /S /Normal >> /GS0 307 0 R /Pg 35 0 R /S /Subscript 273 0 obj /Title (6. endobj null 110 0 R 270 0 R null 111 0 R] /Mendeley#20Recent#20Style#20Name#205_1 (Harvard Reference format 1 \(author-date\)) << /ExtGState << /Lang (EN-GB) >> /C2_0 365 0 R >> /Lang (EN-GB) These operators should modify the DayOfYear object so that it represents the previous day. >> << 45 0 obj CONTROLLED FLAMBING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT. << endobj /Lang (EN-GB) /P 615 0 R 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 /Lang (EN-GB) 293. /Mendeley#20Recent#20Style#20Name#209_1 (Nature) /P 417 0 R /S /Tabelle_content /TT2 314 0 R /Pg 35 0 R >> /MediaBox [0.0 0.0 595.32 841.92] /Parent 4 0 R endobj 19 0 obj /Lang (EN-GB) /K 43 << 1 April 2011. /Mendeley#20Recent#20Style#20Id#203_1 (http://www.zotero.org/styles/american-sociological-association) 113 0 obj /Fm3 298 0 R /Type /Page For instance, 53 percent of the aircraft consists of carbon-fiber composite parts. endobj >> /S /Normal /TT0 290 0 R << >> /Pg 41 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. /ColorSpace << >> >> /K 5 /Mendeley#20Recent#20Style#20Name#203_1 (American Sociological Association) Quick delivery of your "Curtiss H-75A-4 Hawk "French s" airplane model kit at the price of 21.99 GBP with 1001hobbies, the AZ Models specialist. /K 4 /TT3 291 0 R >> /CropBox [0.0 0.0 595.32 841.92] /Contents 302 0 R /K 168 /P 590 0 R >> /K 33 /S /Artifact /P 540 0 R << >> /Rotate 0 /K 100 /A 602 0 R The fuselage has also elements perpendicular to the skin that support it and help keep its shape. 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. /K 124 /S /Tabelle_content /P 17 0 R >> It's enough to make your stomach heave just thinking about all that endless circling. endobj /K 99 << /TT2 303 0 R /Pg 35 0 R /Lang (EN-US) /A 564 0 R >> /DA (/Helv 0 Tf 0 g ) 216 0 obj /Lang (EN-GB) /Parent 15 0 R /Pg 35 0 R /Pg 35 0 R Answer (1 of 3): Cloth, plywood, aluminum alloy from 1920, composites from 1990. The entire air frame, sometimes known as the body group. /Pg 35 0 R >> /K 69 When blade rotation reaches the point where the blade becomes the retreating blade, the extra lift is lost and the blade flaps downward. /P 567 0 R /Fm0 295 0 R << /S /Artifact << /Lang (EN-GB) /K 15 /K 93 It's also one of the most complex in terms of its construction and operation. /A 620 0 R endobj /Parent 16 0 R /Pg 26 0 R /P 437 0 R /P 17 0 R 101 0 obj /odieresis /divide /oslash /ugrave /uacute /ucircumflex /udieresis /yacute /thorn /ydieresis] >> /Pg 33 0 R The wings consist of two essential parts. /Creator (Acrobat PDFMaker 17 for Word) /Lang (EN-GB) /StructParents 11 endobj << /Pg 42 0 R /Sh7 355 0 R /S /Tabelle_content /Pg 35 0 R endobj /Lang (EN-GB) 206 0 obj /Pg 41 0 R 6 0 obj >> << >> They also do not require regular lubrication, which reduces maintenance. << A comparison between two types of helicopter fuselage panels with a traditional design of skin and stringers was carried out. /P 552 0 R /S /Subscript /Pg 33 0 R >> /A 591 0 R /Pg 42 0 R >> /S /Normal 0 %PDF-1.3 >> >> << /CS0 [/ICCBased 287 0 R] The mast is a cylindrical metal shaft that extends upwards from and . endobj >> /P 6 0 R << /Font << /Parent 5 0 R endobj /P 633 0 R 203 0 obj /TT3 314 0 R >> 116 0 obj /K 163 /S /Tabelle_content << 178 0 obj /P 622 0 R /A 607 0 R /ColorSpace << Introduction) endobj /Font << << Airframe design encompasses engineering. endobj >> /Pg 35 0 R /XObject << /GS0 307 0 R /S /Heading#201 /Lang (EN-GB) 16 0 obj >> Combustion /Fm2 297 0 R /Pg 35 0 R /A 544 0 R /P 635 0 R >> /S /Tabelle_content << >> >> /Shading << >> << endobj Like the stations, water line 0 is generally a bit below the aircraft, possibly to have WL 100 at the center of the fuselage, or WL 0 could be at the bottom of the fuselage. 254 0 obj endobj /A 600 0 R 54 0 obj /Font << >> /K 86 /Pg 26 0 R << Add the following overloaded operators: >> << << /Tabs /S /Parent 14 0 R /K 27 >> /S /Subscript http://www.zotero.org/styles/harvard1 196 0 obj /Lang (EN-GB) 427 0 R 428 0 R 429 0 R 430 0 R 431 0 R 432 0 R 433 0 R 434 0 R 435 0 R 436 0 R endobj >> 186 0 obj 120 0 obj /A 491 0 R /TT1 290 0 R What are the values of the SHGC and SC of a single-pane clear-glass window? /S /Normal /Sh16 346 0 R endobj /Pg 35 0 R /ExtGState << /Lang (EN-GB) /Sh4 352 0 R This action to the left causes an opposite reaction to the right, which is the direction needed to counter the main rotor torque. It is lightweight and it has good acceleration. >> /P 606 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 268 0 obj endobj /P 583 0 R endobj /MediaBox [0.0 0.0 595.32 841.92] /Pg 35 0 R << /P 17 0 R /K 415 0 R endobj 112 0 obj /ProcSet [/PDF /Text] /Im0 370 0 R >> /P 585 0 R /XObject << /Pg 35 0 R /Im0 363 0 R /S /Tabelle_content /S /P /TT3 314 0 R /Annots [301 0 R] /Lang (EN-GB) /Pg 24 0 R /TT0 313 0 R /S /Tabelle_content /MediaBox [0.0 0.0 595.32 841.92] >> /Pg 35 0 R << /K 1 /S /Tabelle_content << /P 73 0 R gearbox 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. /Resources << /K 138 /ProcSet [/PDF /Text] /ExtGState << /CropBox [0.0 0.0 595.32 841.92] Stringers are attached to join with the fixture. /K 107 126 0 obj /A 557 0 R The invention relates to a helicopter fuselage of the type including a central structure to which are linked 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 skeleton (16) fitted with covering elements which define the external shape of the . /P 17 0 R /Pg 35 0 R /Lang (EN-GB) 255 0 obj /A 487 0 R << >> /S /Tabelle_content /ColorSpace << The heavier the helicopter, the bigger the engine/s which requires a stronger fuselage. /TT1 310 0 R /Pg 35 0 R /Contents 367 0 R Maybe I wasn't clear. /Parent 14 0 R endobj /S /P /CS1 [/ICCBased 306 0 R] This design methodology was born out of the use of aluminium, rather than steel or wood, as the primary structural material used to manufacture airframe structures. hYmO6+} tBZ`yJ{VVU 5AIh}q}9D"4=i&Xdq,,6,pLX35c&LE)#1J3Q2"PDs3@1GK&'yK&Bo>|>:=. /K 128 /TT2 303 0 R endobj /Lang (EN-GB) << /P 435 0 R /A 462 0 R /K 126 223 0 obj >> 70 0 obj While held in check from sliding back and forth, the teetering hinge does allow the blades to flap up and down. /S /Tabelle_content /Lang (EN-GB) >> The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. ] 245 0 obj endobj >> /MediaBox [0.0 0.0 595.32 841.92] 164 0 obj -Consists of 1 main rotor and a rotary rudder. << >> endobj /S /Span FRAME FUSELAGE STATION 177.2 (Drawing 143F079) The frame at Fuselage Station 177.2 functions as a stiffening member for the fuel cell liner. Welcome to part two in this five-part series on airframe structures. endobj IEEE /S /Tabelle_content hb```"QfE``CKWrL`fk`e`gvZ8^"wk%rL 24:$n30V@`9>@^iOAmwX1z2u) 8 ~* endobj 163 0 R 164 0 R 165 0 R null 166 0 R null 167 0 R 168 0 R null 169 0 R /K 34 /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 /Pg 35 0 R /S /P 33 0 obj /Count 6 /Fm1 296 0 R 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 /Lang (EN-GB) << /P 17 0 R /P 644 0 R /K 164 /Tabs /S << /S /Tabelle_content Quick nationwide delivery of your "Antonov An-30. endobj /P 17 0 R >> /S /Tabelle_content endobj /K 0 A team of enthusiats at your service. Design Priorities Depend On The Plane's Purpose. 68 0 obj /K 1 endobj /K 7 /S /Span http://www.zotero.org/styles/nature >> /Lang (EN-GB) 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. endobj These metals offered more stability and greater protection from the elements. /Fm2 297 0 R << /Pg 33 0 R Modern Humanities Research Association 3rd edition (note with bibliography) >> /ExtGState << 78 0 obj /P 588 0 R /Lang (EN-GB) 141 0 obj This, in turn, changes the amount of countertorque, and the aircraft can be rotated about its vertical axis, allowing the pilot to control the direction the helicopter is facing. 111 0 obj Using a 2mm self tap screw, access the rear bracket hole and tap a drill hole for the rear bracket. /S /Normal 56 0 obj << /Mendeley#20Recent#20Style#20Id#206_1 (http://www.zotero.org/styles/ieee) /Pg 24 0 R /K 17 /Lang (EN-GB) 114 0 R 115 0 R 116 0 R 117 0 R 118 0 R] Anti-torque tail rotor Without a tail rotor, the main rotor of a helicopter simply spins the fuselage in the opposite direction. /P 543 0 R << /Length 608 Chicago Manual of Style 16th edition (author-date) 175 0 obj /XObject << /Kids [28 0 R 29 0 R 30 0 R 31 0 R 32 0 R 33 0 R] << /S /Normal >> /K 24 /S /Tabelle_content >> 98 0 obj /K [5 120 0 R] /Pg 35 0 R endobj 235 0 obj 121 0 obj << /Lang (EN-GB) 8 0 obj /Pg 35 0 R >> >> /MediaBox [0.0 0.0 595.32 841.92] /TT2 303 0 R /Lang (EN-GB) /S /Heading#201 /Lang (EN-GB) /Tabs /S /Lang (EN-GB) /S /Tabelle_content >> 275 0 obj /S /Normal /P 17 0 R /S /Normal /P 17 0 R /Contents 378 0 R /Pg 35 0 R endobj The fuselage (/ f ju z l /; from the French fusel "spindle-shaped") is an aircraft's main body section. /A 470 0 R /K 12 >> >> >> /K 114 /TT1 313 0 R /S /Tabelle_content /Lang (EN-GB) /Type /Metadata << << /P 576 0 R << /CropBox [0.0 0.0 595.32 841.92] /K 49 endobj See Figure 4.12. /K 2 /Resources << /Pg 42 0 R << /Contents 361 0 R /Parent 16 0 R /P 498 0 R /P 17 0 R helicopter frames consist of the fuselagetaylor phillips model age. /P 646 0 R /A 490 0 R >> /Pg 43 0 R uuid:1829709f-1569-4b41-ae83-38410010e776 << endstream endobj startxref /S /Tabelle_content /K 44 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, GIRAVION EQUIPPED WITH FUEL TANKS MOUNTED BY SUSPENSION UNDER MEDIAN FLOOR WORKING WITH FUSELAGE OF THE GIRAVION, Shrouded rotary assembly from segmented composite for aircraft and method for its manufacture, Subfloor structure with an integral hull for a rotary wing aircraft, 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, Unmanned helicopter upper plate and installation method thereof, Unmanned helicopter body middle plate and fixing method, An aircraft with an airframe that comprises a load carrying framework, An aircraft with a fuselage that comprises at least one hollow beam element, Universal aircraft cabin beam and design method thereof, structure of a FUSELAGE OF AN aircraft presenting a panel reinforced by a trellis, Unmanned helicopter fuselage force transmission structure assembly, CABIN OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH MOVING LAMP, Light aircraft structural layout - has two main bulkheads interconnected by main bream allowing rearward positioning of engine and wing spar, Mezzanine structure for wide-bodied passenger aircraft, SANITARY COMPLEX TO BE INSTALLED IN AN AIRCRAFT, OF A STANDARD TYPE, TO TRANSFORM IT INTO A AIRCRAFT IN SANITARY VERSION, Stowage structure for electronic equipment in aircraft - has supporting members formed as structural elements with channels for cooling components, Modular chassis for land, sea and air vehicles, Energy absorbing composite aircraft structure, Wide-body aircraft having efficient utilization of interior space and method therefor, Aircraft fore-structure and storage compartment for forward landing gear, Perfected aircraft fore-structure including a landing gear compartment, Multi-engine aircraft with a vertical shaft, STORAGE BOX FOR A FRONT TRAIN FOR AN AIRCRAFT, Aircraft for transporting e.g. /S /Artifact << 138 0 obj The wings and tail section are attached to the fuselage, and depending on the design of the aircraft, may include engine attachments too. /MediaBox [0.0 0.0 595.32 841.92] << 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. 176 0 obj /Mendeley#20Recent#20Style#20Id#208_1 (http://www.zotero.org/styles/modern-language-association) /Sh18 348 0 R >> Define the SHGC (solar heat gain coefficient), and explain how it differs from the SC (shading coefficient). Tilting the rotor plane of rotation causes the aircraft to move horizontally. The fuselage generates its own aerodynamic loads during flight which must be reacted by the structure. >> 11 [null null 135 0 R null null null 136 0 R null null 137 0 R 73 0 obj endobj << /K 80 << endobj Similar to a vertical stabilizer on the empennage of an airplane, a fin or pylon is also a common feature on rotorcraft. null] May 23, 2021 . >> /K 141 endobj /Lang (EN-US) /A 397 0 R endobj >> /S /Span /ProcSet [/PDF /Text] 215 0 obj Airframe design encompasses engineering, aerodynamics, materials technology, and manufacturing methods to achieve favorable balances of performance, reliability, and cost. 162 0 obj >> /TT3 291 0 R /A 589 0 R What does the landing gear group of helicopter include? /A 453 0 R The wing is covered in part three, flaps in part four, and the tail in part five. /K 136 The latter two are still in use. Smith, Michael Abbott, LP4 Valves/Valve Operators (Obj. /Sh13 343 0 R /Pg 35 0 R endobj /ColorSpace << The frame is made from very strong . 261 0 obj /Lang (EN-GB) /ExtGState << /Pg 30 0 R /S /Strong /ProcSet [/PDF /Text] Learn more about the design of a typical semi-monocoque fusealge structure, and the various structural components and loadings that contribute to the final design.

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