endobj /Fm1 296 0 R endobj 196 0 obj /Parent 4 0 R The A-129 International is a fast, manoeuvrable helicopter. /Pg 35 0 R 11 0 obj endobj >> /P 633 0 R endobj 169 0 obj << endobj >> /K [185 442 0 R] /K [176 262 0 R] /P 651 0 R /P 660 0 R /XObject << /P 664 0 R /CS0 [/ICCBased 287 0 R] /Pg 35 0 R /Rotate 0 endobj << /K 19 /Tabs /S /CS0 [/ICCBased 287 0 R] 53 0 obj << >> /Pg 30 0 R These rotors are usually made of a composite structure. /P 433 0 R 47 0 obj /A 480 0 R /CS1 [/ICCBased 306 0 R] >> /Sh10 340 0 R /ProcSet [/PDF /Text] >> /K [5 120 0 R] /Lang (EN-GB) /StructParents 6 /Author /P endobj << endobj /A 562 0 R /K 4 >> /Pg 42 0 R /K 41 >> 200 0 obj /ProcSet [/PDF /Text /ImageC] >> endobj /Font << 68 0 R 123 0 R 68 0 R 124 0 R 70 0 R 125 0 R 70 0 R 126 0 R] -- prefix and postfix decrement operators. << endobj >> >> /F5 293 0 R "How Helicopters Work" /Producer (Adobe PDF Library 15.0) 168 0 obj The latter two are still in use. 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. /Resources << /S /Artifact FRAME FUSELAGE STATION 177.2 (Drawing 143F079) The frame at Fuselage Station 177.2 functions as a stiffening member for the fuel cell liner. /A 453 0 R >> /S /GoTo /Lang (EN-GB) Frames also provide a means to introduce point loads into the fuselage. endobj /XObject << A comparison between two types of helicopter fuselage panels with a traditional design of skin and stringers was carried out. /ColorSpace << June 22, 2022. ilive code for dish remote . >> endobj /A 384 0 R /Resources << /K 88 193 0 obj << >> endobj Aluminium has many advantages over steel. >> /S /Tabelle_content /Lang (EN-GB) /K 49 endobj >> /K 3 Please refer to our privacy policy for further information. >> /P 17 0 R -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 /P 639 0 R They also do not require regular lubrication, which reduces maintenance. >> /Pg 35 0 R /P 47 0 R /CropBox [0.0 0.0 595.32 841.92] All these load cases, and the interaction between cases must be considered to arrive at a final design. 3218 Kalle Saastamoinen et al. /K 13 /TT3 313 0 R << /K 7 /K 182 >> /S /Strong << /K 17 /Contents 302 0 R /Pg 35 0 R /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 . 98 0 obj /GS0 307 0 R >> /K 142 >> /A 569 0 R /GS0 288 0 R /A 472 0 R /XObject << /Pg 35 0 R These polymer bearings have the ability to deform and return to their original shape. /Subscript /Span /Fm4 299 0 R /P 17 0 R /A 542 0 R >> /A 405 0 R /Pg 26 0 R NAFEMS World Congress 2017 /Lang (EN-GB) D. Schwinn, P. Weiand, M. Schmid << /Parent 4 0 R endobj /K [8 264 0 R] /S /Author << /Pg 26 0 R << 189 0 obj /Pg 43 0 R << /A 524 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 << /K 109 << /A 553 0 R 3 /P 17 0 R /XObject << In the late 1920s and early 1930s, airplane manufacturers started producing more fuselages from aluminum and steel. /Pg 35 0 R Airframe design encompasses engineering. /Pg 24 0 R /A 411 0 R /Pg 24 0 R From Wikipedia." airplane model kit at the price of 83.99 GBP with 1001hobbies, the AModel specialist. /Lang (EN-GB) endobj 84 0 obj /Pg 43 0 R /Resources << endobj >> /Lang (EN-GB) /Resources << 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 /A 388 0 R /Pg 42 0 R endobj /K 0 << 77 0 obj /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /TT2 312 0 R /Rotate 0 endobj << /A 627 0 R /Parent 4 0 R /K [2 119 0 R] /A 529 0 R /Pg 33 0 R << /Sh14 344 0 R 253 0 obj << << 70 0 obj << /Resources << 273 0 obj 124 0 obj /K 85 54 0 obj /Resources << endobj /Title (4. /Pg 35 0 R /K 3 62 0 obj /A 531 0 R /S /Subscript << endobj /Type /Pages /P 17 0 R /K 1 /P 552 0 R /P 603 0 R /Pg 42 0 R << endobj /Lang (EN-GB) << /GS0 307 0 R /TT0 290 0 R /P 646 0 R /Pg 30 0 R /Rotate 0 >> /Pg 35 0 R /K 80 << /TT0 290 0 R /A 650 0 R endobj /Pg 26 0 R /P 530 0 R /S /Tabelle_content >> /S /Normal /A 451 0 R /Pg 35 0 R /F4 292 0 R /S /Tabelle_content >> /Lang (EN-US) 269 0 obj >> /S /Tabelle_content /S /Tabelle_content /A 602 0 R /Lang (EN-GB) /A 605 0 R 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. >> /Mendeley#20Recent#20Style#20Id#200_1 (http://www.zotero.org/styles/american-medical-association) << /MediaBox [0.0 0.0 595.32 841.92] /Pg 35 0 R CONTROLLED FLAMBING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT. /S /Normal /Pg 33 0 R /S /Tabelle_content endobj /S /Tabelle_content /dotlessi /lslash /oe /scaron /zcaron 160 /Euro 164 /currency 166 >> >> /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /Pg 33 0 R /Sh7 325 0 R /Lang (EN-GB) 143 0 obj /Lang (EN-GB) Rotary wing aircraft which obtains lift and thrust from mechanically driven airfoils. /K 5 /S /Tabelle_content << >> What happens when the cyclic control stick is moved forward? Tilting the rotor plane of rotation causes the aircraft to move horizontally. /CropBox [0.0 0.0 595.32 841.92] The main rotor, of course, is the most important part of a helicopter. /K 68 /ProcSet [/PDF /Text] << 188 0 obj The fuselage (/ f ju z l /; from the French fusel "spindle-shaped") is an aircraft's main body section. /TT0 310 0 R /quoteright /quotesinglbase /trademark /fi /fl /Lslash /OE /Scaron /Ydieresis /Zcaron << stream 73 0 R] /P 17 0 R endobj << /Tabs /S endobj /K [6 124 0 R 14 125 0 R 16 126 0 R] /Pg 35 0 R endobj Show, by giving a DTD, how to represent the non-1NF books relation as shown in earlier Section using XML. -Consists of 1 main rotor and a rotary rudder. /Resources << /K << Free shipping above 99. /P 543 0 R The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. Hydraulically operated [Figure 8] Controlled with foot pedals, the countertorque of the tail rotor must be modulated as engine power levels are changed. /A 676 0 R /S /Tabelle_content -effective to a height of approximately half the rotor diameter endobj 197 0 obj endobj endobj /A 398 0 R /ProcSet [/PDF /Text /ImageC] 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 >> Air is vented out of two long slots on the right side of the tail boom, entraining main rotor wash to hug the right side of the tail boom, in turn causing laminar flow and a low pressure (Coanda Effect). /Lang (EN-GB) 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. /S /Normal endobj /P 17 0 R >> << /S /Subscript >> References) Customer satisfaction 4,2/5. << /A 659 0 R endobj /P 535 0 R 238 0 obj 120 0 obj of the year, the new value of the object will represent the first day of the year. /S /Tabelle_content /P 17 0 R /Pg 43 0 R /A 400 0 R wreck me meaning; how to stop youtube update required /CS1 [/ICCBased 306 0 R] 2. endobj /P 17 0 R endobj 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. >> 96 0 obj << /Sh1 339 0 R /Fm4 299 0 R 2017-05-08T21:10:34+01:00 /Pg 35 0 R >> /K 5 Monocoque 275 0 obj /Mendeley#20Recent#20Style#20Name#202_1 (American Psychological Association 6th edition) 141 0 obj /K 11 American Sociological Association << /Length 7746 80 0 obj 229 0 obj /P 17 0 R /Type /Page /CS0 [/ICCBased 287 0 R] /TT0 290 0 R /Shading << << >> /Lang (EN-GB) 128 0 obj /S /Tabelle_content 255 0 obj >> << /S /Normal endobj << /S /P hb```"QfE``CKWrL`fk`e`gvZ8^"wk%rL 24:$n30V@`9>@^iOAmwX1z2u) 8 ~* /S /Normal << /TT0 290 0 R >> << /P 637 0 R >> /P 540 0 R endobj /K 52 As such, they can absorb vibration that would normally be transferred by steel bearings. << /Lang (EN-GB) /S /P /Lang (EN-GB) /S /Artifact << endobj /Count 6 situs link alternatif kamislot helicopter frames consist of the fuselage 229 0 R 230 0 R 231 0 R null 232 0 R null 233 0 R 234 0 R 235 0 R 236 0 R /P 17 0 R /Sh3 351 0 R /Contents 331 0 R /A 654 0 R /P 592 0 R /CS1 [/ICCBased 306 0 R] /A 580 0 R endobj /Pg 42 0 R /K 5 /Lang (EN-GB) /Contents 360 0 R >> /GS1 308 0 R /A 475 0 R >> /Helv 9 0 R noble soccer tournament 2021 how to get gems in phase 10: world tour army covid pt test policy helicopter frames consist of the fuselage. http://www.zotero.org/styles/chicago-author-date /P 427 0 R /Im6 300 0 R 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. /S /P >> >> /Diagram /Figure >> >> endobj /Parent 14 0 R /A 439 0 R endobj << /C2_0 332 0 R uuid:ce5ad891-f06f-4f16-9f52-42c508d454cd endobj /S /Tabelle_content /Mendeley#20Recent#20Style#20Id#205_1 (http://www.zotero.org/styles/harvard1) /Lang (EN-GB) >> /Pg 41 0 R endobj From Wikipedia." airplane model kit at the price of 84.99 USD with 1001hobbies, the AModel specialist. 153 0 obj /Pg 35 0 R /Outlines 4 0 R Large bending loads are introduced from the wing and tail sections, as well as a torsional load from the pitching moment of the wing. endobj >> /Fm1 296 0 R endobj /Parent 4 0 R /Tabs /S What does the landing gear group of helicopter include? /K 121 0 R This video from British Airways shows the joining process: Fuselage Section Joining Process which you can see is not welded, but riveted together. The horizontal and vertical tails are rigidly attached to the fuselage as indicated. endobj nafems endobj /Pg 30 0 R endobj /Lang (EN-GB) /ProcSet [/PDF /Text /ImageC] /Lang (EN-GB) /Font << >> IEEE /Pg 35 0 R endobj endobj << /A 478 0 R /Type /Page /XObject << /S /Tabelle_content /S /Artifact 210 0 obj endobj /Fm3 298 0 R 3. Skin Fwd Inbd, Skin Fwd Fuselage Top, Skin Fwd Fuselage Rh, Skin Fwd Fuselage Bot, Skin Fwd Fuselage are just some of the many aviation components that we offer at Aerospace Aces. May or may not actuate during blade folding, -self exited vibration, which occurs on the ground << /K 120 214 0 obj << /P 17 0 R /S /Normal /TT1 289 0 R /ColorSpace << 251 0 obj /Pg 24 0 R /Subtype /Type1 /S /P /A 632 0 R >> /Fm4 299 0 R /K 4 >> /Lang (EN-GB) endobj The skins carry load through shear and transmit this shear into the stiffeners. /Lang (DE-DE) 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. helicopter frames consist of the fuselage. /P 495 0 R /TT0 310 0 R /S /Tabelle_content /K 126 /Fm4 299 0 R You can probably guess by now that these are holdovers from the marine industry. << /Lang (EN-GB) >> /A 20 0 R /P 599 0 R /P 17 0 R endobj /Lang (EN-GB) 166 0 obj >> >> 12 0 obj endobj 170 0 obj >> /A 520 0 R /A 677 0 R /Pg 42 0 R 237 0 R null 238 0 R null 239 0 R 240 0 R 241 0 R 242 0 R 243 0 R null /P 17 0 R << << endobj endobj >> 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 /Pg 24 0 R /Pg 35 0 R /D [41 0 R /XYZ 104 373 0.0] /Rotate 0 -Can be thought of as the Aircraft pivot pts. /TT2 291 0 R /P 586 0 R D:20170502160949 /P 17 0 R 1. /Pg 35 0 R /GS0 288 0 R /Pg 42 0 R /P 619 0 R 262 0 obj /Pg 35 0 R 38 0 obj /S /Artifact /DisplayDocTitle true By continuing here you are consenting to their use. /Lang (EN-GB) endobj 2017-05-08T21:10:16+01:00 >> endobj /ColorSpace << 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. /C2_0 365 0 R Other important ight subsystems, illustrated in Figure 1.1, are the horizontal tail, the vertical tail, and the engines. -as the angle of attack increases, canter of pressure moves forward along the airfoil surface 2 x 7.62 mm M134 Minigun machine guns (1,500 rpg = 3,000 total) 2 x 7.62 mm M134 Minigun machine guns (6,000 rpg = 12,000 total) + 38 x FFAR Mighty Mouse rockets. /DA (/Helv 0 Tf 0 g ) 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. << >> /A 511 0 R Piper PA-18 Super Cub with a Space Frame Fuselage. In front and center of the pilot's and co-pilot's seats (interconnected). /P 418 0 R /A 578 0 R /S /Normal >> endobj 225 0 obj /Type /Page /P 73 0 R /Pg 30 0 R /MediaBox [0.0 0.0 595.32 841.92] /A 387 0 R /K 134 /P 420 0 R /CS0 [/ICCBased 287 0 R] /Fm2 297 0 R << << << /Sh6 324 0 R /Pg 41 0 R /ZaDb 10 0 R Anti-torque tail rotor Without a tail rotor, the main rotor of a helicopter simply spins the fuselage in the opposite direction. endobj endobj /Pg 35 0 R /K 8 /ColorSpace << /CropBox [0.0 0.0 595.32 841.92] /Pg 35 0 R /K 117 /S /Normal << /MediaBox [0.0 0.0 595.32 841.92] /A 486 0 R The heavier the helicopter, the bigger the engine/s which requires a stronger fuselage. /CS1 [/ICCBased 306 0 R] 149 0 obj endobj /S /Normal /TT3 314 0 R /K 155 << endobj /Parent 15 0 R /GS0 307 0 R /A 663 0 R /K 10 /CS0 [/ICCBased 287 0 R] /MediaBox [0.0 0.0 595.32 841.92] /P 17 0 R /Type /Metadata >> /Font << 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 /P 17 0 R >> /Pg 30 0 R consist of: [phrasal verb] to be formed or made up of (specified things or people). /A 490 0 R >> /S /Span /K 187 Welcome to part two in this five-part series on airframe structures. /A 571 0 R /Pg 35 0 R /S /Artifact >> /K 1 . /Lang (EN-US) /Pg 25 0 R /P 70 0 R /K 44 /K 10 Collective Control The collective-pitch lever is responsible for up-and-down movements. endobj >> endobj /Pg 24 0 R /Pg 35 0 R endobj /K 13 /Pg 35 0 R >> 214 0 R null 215 0 R 216 0 R 217 0 R 218 0 R 219 0 R null 220 0 R null >> /S /Normal << << /K 106 /TT2 314 0 R 105 0 obj /P 658 0 R /TT3 313 0 R /Fm0 295 0 R /K 3 /Pg 35 0 R /Pg 33 0 R >> endobj >> /Pg 33 0 R /P 510 0 R /Prev 274 0 R http://www.zotero.org/styles/modern-humanities-research-association 95 0 obj << /S /Tabelle_content /P 635 0 R /ExtGState << endobj /K 172 /P 501 0 R /Lang (EN-GB) /A 500 0 R >> /P 588 0 R 171 0 obj >> /K 1 The stringers also support the skin, and when combined with the frames, create bays over which the skin is attached. /Pg 35 0 R Fuselage The main body of the helicopter is known as the fuselage. >> /P 73 0 R >> ++ prefix and postfix increment operators. 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. /K 83 /TT4 314 0 R endobj 59 0 obj /P 256 0 R >> /S /Span 51 0 obj /S /Tabelle_content /K 56 << /Pg 25 0 R /S /Tabelle_content /Mendeley#20Recent#20Style#20Name#206_1 (IEEE) /Lang (EN-GB) /P 110 0 R -produces thermal or heat energy to drive power turbine, Front frame 34 0 obj /Font << One or more horizontal hinges provide for flapping on a fully articulated rotor system. /S /P /P 624 0 R endstream /P 17 0 R /Pg 42 0 R 106 0 obj /P 428 0 R endobj /Lang (EN-GB) << /ExtGState << /Lang (EN-GB) American Political Science Association >> /Pg 30 0 R 19 0 obj /K 6 /K 0 /Lang (EN-GB) /P 574 0 R endobj /S /Normal endobj /P 17 0 R /Pg 42 0 R /Mendeley#20Recent#20Style#20Name#205_1 (Harvard Reference format 1 \(author-date\)) >> 1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6 >> >> endobj Nature /P 17 0 R /S /Normal /P 17 0 R Tail drive shaft 211 0 obj /Lang (DE-DE) >> /K 154 /K 115 /A 481 0 R << 199 0 obj /K 76 >> /K 166 236 0 obj Introduction The use of unmanned multicopters and airplanes in civil aviation as well as military aviation has become widespread in recent years. For instance, the Leonardo AW139 . << -moves the thrust of the rotor and the lift of the helicopter, pulling it in the direction of the tip path plane. /Lang (EN-GB) << endobj >> 437 0 R 438 0 R] /K 9 /K 15 /P 17 0 R /A 492 0 R Thicker skins are advantageous as these are less likely to buckle under load, resulting in a more efficient structure. /MediaBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /Contents 328 0 R /P 17 0 R 245 0 obj Tandem Rotor. /Lang (EN-GB) /A 469 0 R /P 17 0 R /P 17 0 R /Pg 42 0 R /K 173 /Lang (EN-GB) endobj /Pg 25 0 R endobj /Mendeley#20Recent#20Style#20Id#202_1 (http://www.zotero.org/styles/apa) /P 590 0 R /TT2 303 0 R /MediaBox [0.0 0.0 595.32 841.92] Thanks for reading. /S /Tabelle_content /CS0 [/ICCBased 287 0 R] /Contents 361 0 R /P 537 0 R /A 607 0 R /GS0 288 0 R >> 36 0 obj /Lang (EN-GB) 61 0 obj Provides a means of transmitting the movement of flight controls to the blades. >> /TT0 310 0 R /A 618 0 R /S /Tabelle_content /S /Tabelle_content /A 566 0 R /K 19 There are four major systems in a full scale rocket; the structural system, the payload system, the guidance system, and the propulsion system . /Lang (EN-GB) /Mendeley#20Recent#20Style#20Name#207_1 (Modern Humanities Research Association 3rd edition \(note with bibliography\)) Chicago Manual of Style 16th edition (author-date) /Pg 41 0 R /A 385 0 R endobj >> /ColorSpace << 121 0 obj Adobe PDF Library 15.0 /Next 12 0 R /Pg 35 0 R >> /Pg 36 0 R endobj << 103 0 obj The tail boom and tail rotor, or antitorque rotor, counteract this torque effect. /TT0 290 0 R /Pg 33 0 R /Mendeley#20Recent#20Style#20Name#208_1 (Modern Language Association 7th edition) /A 544 0 R >> /S /Normal << Their primary aim is to transmit the axial loads (tension and compression) that arise from the tendency of the fuselage to bend under loading. >> /C2_0 362 0 R endobj /Type /Page /florin /fraction /guilsinglleft /guilsinglright /minus /perthousand /quotedblbase /quotedblleft /quotedblright /quoteleft /S /Artifact /P 17 0 R >> >> /Pg 30 0 R 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. /Pg 35 0 R /Mendeley#20Recent#20Style#20Id#209_1 (http://www.zotero.org/styles/nature) >> The sections are lined up and riveted together using joining plates. >> /A 391 0 R /K 62 Graphite-epoxy is one of several types of composite materials that are becoming widely used for many aircraft structures and components. >> /Contents 358 0 R /S /Normal >> /K [16 268 0 R 269 0 R] >> Figure 1 shows the major components of a typical helicopter. /A 616 0 R Toward that end, the use of elastomeric bearings in main rotor systems is increasing. /GS0 307 0 R /GS0 288 0 R /K [184 263 0 R 188] 172 0 obj /S /Artifact >> /A 406 0 R /Pg 35 0 R endobj << /P 17 0 R /S /Subscript /Pg 35 0 R << /Fm3 298 0 R /K 124 /K 160 /P 567 0 R /CS0 [/ICCBased 287 0 R] /P 17 0 R fiber), or carbon fiber. /K [8 272 0 R] >> << A few models have skids with two ground-handling wheels. /P 514 0 R /XObject << /Lang (EN-GB) Tail boom The tail boom extends out from the rear of the fuselage and holds the tail rotor assemblies. /K 13 /S /Tabelle_content /brokenbar 168 /dieresis /copyright /ordfeminine 172 /logicalnot /.notdef /registered /macron /P 68 0 R /S /Normal 162 0 obj /S /Normal << << 295. /Prev 23 0 R >> /Parent 15 0 R >> /Lang (EN-GB) /Parent 15 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.