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/A 413 0 R Smith, Michael Abbott, LP4 Valves/Valve Operators (Obj. /S /Span /Parent 13 0 R /Lang (EN-GB) /TT1 289 0 R /Pg 35 0 R /Lang (EN-GB) /A 609 0 R /Pg 35 0 R /S /Normal /S /Normal /MediaBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) /K 66 /Pg 35 0 R << 14 0 obj "The Tempo project deals with using new fuselage structures and assembly tasks to reduce the time and cost of current states of production," says Brieskorn. This action to the left causes an opposite reaction to the right, which is the direction needed to counter the main rotor torque. /Lang /MarkInfo << /S /Tabelle_content 207 0 obj endobj >> /S /Normal /S /Artifact /P 640 0 R 137 0 obj 191 0 obj /Pg 35 0 R >> /K 17 0 R Helicopter fuselages vary widely from those with a truss frame, two seats, no doors, and a monocoque shell flight compartment to those with fully enclosed airplane-style cabins as found on larger twin-engine helicopters. 173 0 obj 195 0 obj >> 185 0 obj << << /K [8 264 0 R] /K 156 /P 17 0 R /Pg 35 0 R endobj /Resources << >> endobj /Pg 25 0 R /K 183 "Integral frames made of CFRP may replace differential constructions, due to higher stiffness, and . /ExtGState << /Pg 30 0 R >> endobj endobj Lift and control are relatively independent of what? /TT1 291 0 R /K 61 /S /P /Pg 35 0 R /P 572 0 R /P 604 0 R endobj /K 131 /GS0 288 0 R /Sh5 353 0 R >> 50 0 obj /S /Normal /TT0 290 0 R /Parent 15 0 R from China. Large bending loads are introduced from the wing and tail sections, as well as a torsional load from the pitching moment of the wing. 266 0 R null 107 0 R 267 0 R null 108 0 R 109 0 R 268 0 R null 269 0 R /Sh13 343 0 R << /ColorSpace << /Pg 30 0 R endobj /Sh5 323 0 R /S /Normal /K 134 /ProcSet [/PDF /Text /ImageC] >> >> /P 651 0 R endobj /ColorSpace << >> /K 44 /Pg 42 0 R /S /Subscript One or more horizontal hinges provide for flapping on a fully articulated rotor system. /Lang (EN-GB) /K 15 << << << Figure 1 shows the major components of a typical helicopter. /Pg 35 0 R /K 70 /Pg 42 0 R /P 17 0 R /P 106 0 R << /Title (3. /S /Artifact /GS0 307 0 R << >> Position the helicopter and drill holes for the front mounting bracket. 52 0 obj /Font << /P 565 0 R /K 13 According to Wikipedia, the semi-monocoqne fuselage structure is preferred when constructing an all-aluminum fuselage. 62 0 obj /ProcSet [/PDF /Text] /A 454 0 R 230 0 obj 114 0 R 115 0 R 116 0 R 117 0 R 118 0 R] /Contents 302 0 R /P 17 0 R >> /Lang (EN-GB) /S /Tabelle_content /K 90 277 0 obj /Pg 35 0 R /D [41 0 R /XYZ 104 373 0.0] 263 0 obj /Pg 35 0 R /Lang (EN-GB) /Font << /S /Sect /Tabs /S 13 0 obj /Fm4 299 0 R /P 17 0 R /Pg 35 0 R /S /Artifact Changing the angle of attack of the rotating blades increases or decreases lift, respectively raising or lowering the helicopter. << /Contents 305 0 R 3218 Kalle Saastamoinen et al. >> /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] 41 0 obj / Procedia Computer Science 176 (2020) 3217-3224 2 Author name / Procedia Computer Science 00 (2020) 000-000 1. 18 0 obj /S /Tabelle_content 117 0 obj /Lang (EN-GB) << /S /Normal /A 404 0 R /K 24 << /Sh7 355 0 R The fuselage has also elements perpendicular to the skin that support it and help keep its shape. /S /Author << >> >> >> /Lang (EN-GB) /CropBox [0.0 0.0 595.32 841.92] /S /Table << /Kids [24 0 R 25 0 R 26 0 R 27 0 R] << /Parent 16 0 R 3 0 obj >> /S /Tabelle_content /K 3 /P 540 0 R /Lang (EN-GB) /Font << /GS0 288 0 R 268 0 obj endobj /Fm0 295 0 R /S /Tabelle_content /A 481 0 R /ColorSpace << 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. /Resources << /K 6 -through the use of a freewheeling unit, located w/in main gearbox assembly, Stops rotation of rotor head << /XObject << /A 557 0 R /Pg 35 0 R /Sh12 319 0 R endobj The result is a simpler rotor mast with lower maintenance due to fewer moving parts. << /S /Subscript /TT1 313 0 R /Lang (EN-GB) /CS0 [/ICCBased 287 0 R] /A 381 0 R /Sh14 344 0 R /K 138 endobj 131 0 obj /S /Tabelle_content /Type /Page 199 0 obj 220 0 obj /Prev 274 0 R endobj Contact Us | Privacy Policy | Terms of Use, The airframe, or fundamental structure, of a helicopter can be made of either metal, wood, or composite materials, or some combination of the two. In some models, the tail boom is nothing more than an aluminum frame. /Endnote /Note endobj /Pg 35 0 R /A 416 0 R /S /Tabelle_content endobj << 3 Wing Contents Providing lift is the main function of the wings of an aircraft. /Lang (EN-GB) /Pg 35 0 R /Marked true /S /P /P 519 0 R /Type /Page << /Sh6 354 0 R >> /Contents 375 0 R >> << /P 17 0 R /P 17 0 R 181 0 obj /ProcSet [/PDF /Text /ImageC] /Pg 35 0 R >> /P 432 0 R /S /Tabelle_content /Adieresis /Aring /AE /Ccedilla /Egrave /Eacute /Ecircumflex /Edieresis /Igrave /Iacute >> /Pg 30 0 R /P 17 0 R /S /P << /A 412 0 R 11 [null null 135 0 R null null null 136 0 R null null 137 0 R /Count 6 Introduction The use of unmanned multicopters and airplanes in civil aviation as well as military aviation has become widespread in recent years. 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 /Differences [24 /breve /caron /circumflex /dotaccent /hungarumlaut /ogonek /ring /tilde 39 null null 138 0 R null null 139 0 R null null 140 0 R null 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. /Pg 35 0 R /S /Subscript /ColorSpace << /Mendeley#20Document_1 (True) -on helicopters using 2 engines, the main trans. /S /Normal << >> /Parent 15 0 R << /K 101 endobj >> /Pg 35 0 R << endobj >> >> endobj << << 85 0 obj << /Lang (EN-GB) << /S /Tabelle_content endobj endobj The relative windspeed is greater on an advancing blade than it is on a retreating blade. /ProcSet [/PDF /Text /ImageC] /Parent 16 0 R /Font << /A 529 0 R /Lang (EN-GB) /A 654 0 R << /Lang (EN-GB) 56 0 obj endobj /Parent 4 0 R /TT0 290 0 R << /Lang (EN-GB) endobj endobj /Lang (EN-GB) /S /Normal << << /Im0 368 0 R /Parent 5 0 R << /Contents 364 0 R /S /Tabelle_content /Count 0 187 0 obj /Prev 23 0 R /P 666 0 R /Lang (EN-GB) << >> 170 0 obj endobj gearbox has provisions for operating in the event of a single failure endobj 112 0 obj If you enjoyed this post or found it useful as a study aid, then please introduce your colleagues and friends to AeroToolbox.com and share this on your favourite social media platform. /Sh3 321 0 R One of the helicopters came down and major components/assemblies were recovered . endobj >> /Mendeley#20Unique#20User#20Id_1 (1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6) stream /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 /P 521 0 R /Fm1 296 0 R IEEE 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. /Lang (EN-GB) << /P 550 0 R /S /Normal /Parent 13 0 R /P 70 0 R endobj /P 422 0 R /Lang (EN-GB) The rotor consists of a mast, hub, and rotor blades. /P 559 0 R /CS1 [/ICCBased 306 0 R] /Lang (EN-US) /K [1 265 0 R] /S /Normal /Lang (EN-GB) The fuselage also houses the engine, the transmission, avionics, flight controls, and the powerplant. >> /A 487 0 R /TT1 333 0 R /S /Artifact /S /P >> /A 385 0 R endobj 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) /P 433 0 R /Lang (EN-GB) /K 96 135 0 obj /K 1 Other important ight subsystems, illustrated in Figure 1.1, are the horizontal tail, the vertical tail, and the engines. /Pg 41 0 R areas are at the fuselage upper part and at the joints of the fuselage frames to the wing spars. /S /P /P 426 0 R /K 6 Maybe I wasn't clear. /S /Tabelle_content /Contents 337 0 R >> 239 0 obj /K 9 /Pg 42 0 R 255 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 /Mendeley#20Recent#20Style#20Id#208_1 (http://www.zotero.org/styles/modern-language-association) << /Fm1 296 0 R << The tail boom and tail rotor, or antitorque rotor, counteract this torque effect. /StructParents 19 /Pg 25 0 R << The loading consists of Internal pressure applied by the fuel. /P 517 0 R >> /P 17 0 R /P 613 0 R /Mendeley#20Recent#20Style#20Name#203_1 (American Sociological Association) 31 0 obj /P 597 0 R /ProcSet [/PDF /Text] /MediaBox [0.0 0.0 595.32 841.92] >> >> >> 121 0 obj >> >> /First 11 0 R /Lang (EN-GB) /Pg 33 0 R /S /Subscript /Fm2 297 0 R -used to tilt the tip path plane of the main rotor >> /P 624 0 R >> endobj >> /S /Artifact << 73 0 R] /S /Artifact /StructParents 18 >> /StructParents 9 295. /CropBox [0.0 0.0 595.32 841.92] 262 0 obj $\begingroup$ @mins No, that's not even close. /S /Tabelle_content /Font << 158 0 obj /Fm2 297 0 R /K 174 68 0 R 123 0 R 68 0 R 124 0 R 70 0 R 125 0 R 70 0 R 126 0 R] /P 436 0 R /Pg 24 0 R /P 17 0 R << The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. /D [24 0 R /XYZ 104 737 0.0] /Mendeley#20Recent#20Style#20Id#200_1 (http://www.zotero.org/styles/american-medical-association) /Fm3 298 0 R >> >> /Font << >> << << /A 414 0 R /Lang (EN-GB) 249 0 obj >> /Count 0 endobj /ExtGState << /Pg 35 0 R /TT1 289 0 R As such, many hinges and bearings can be eliminated from the tradition main rotor system. /P 81 0 R /Pg 42 0 R /Bibliography /BibEntry << /K 0 BIGTREETECH BTT SKR PICO V1.0 Motherboard On Board TMC2209 UART MURATA Capacitor for Raspberry Pi VORON /Pg 35 0 R << << /A 659 0 R /P 635 0 R >> /Type /Pages /P 567 0 R Quick delivery of your "Antonov An-30. /A 446 0 R >> /Fm3 298 0 R endobj /Resources << 69 0 obj /CS0 [/ICCBased 287 0 R] /P 70 0 R /Pg 26 0 R /P 534 0 R << /Pg 33 0 R Typically, a composite component consists of many layers of fiber-impregnated resins . They are typically spaced approximately 20 inches apart and define the aerodynamic shape. /S /Normal /A 605 0 R << /TT3 291 0 R << /Type /Page /P 17 0 R %PDF-1.3 141 0 R null 142 0 R null 143 0 R 144 0 R 145 0 R 146 0 R 147 0 R null /K 130 >> /Pg 30 0 R /StructParents 0 /Pg 35 0 R All these load cases, and the interaction between cases must be considered to arrive at a final design. 37 0 obj /TT0 290 0 R << /Length 7746 5. /TT3 313 0 R They also do not require regular lubrication, which reduces maintenance. /Pg 35 0 R /K 110 << /Pg 33 0 R /A 408 0 R /K 11 /K 116 /P 6 0 R /S /Artifact gearbox /Pg 35 0 R 261 0 obj /S /Normal 90 0 obj /Resources << << /Lang (EN-US) /Sh1 316 0 R >> /Font << >> /A 273 0 R endobj >> >> A NOTAR antitorque system has no visible rotor mounted on the tail boom. /Rotate 0 /Lang (DE-DE) /S /Artifact endobj >> /Pg 33 0 R 102 0 obj << /CropBox [0.0 0.0 595.32 841.92] /A 593 0 R endobj 106 0 obj /Pg 41 0 R /S /Normal /S /Normal /S /Normal /Lang (EN-GB) << Thicker skins are advantageous as these are less likely to buckle under load, resulting in a more efficient structure. /TT1 311 0 R << /Prev 21 0 R /Lang (EN-GB) The fuselage (/ f ju z l /; from the French fusel "spindle-shaped") is an aircraft's main body section. /P 17 0 R /Lang (EN-GB) endobj /A 620 0 R endobj /Lang (EN-GB) /Lang (EN-GB) /Pg 35 0 R << /Strikeout /Span /P 17 0 R endobj << endobj /CS1 [/ICCBased 306 0 R] 101 0 obj 200 0 obj What happens to the inflow of air during forward flight? /S /P Most have the pilot seated on the right side, although there are some with the pilot seated on the left side or center. /P 17 0 R /P 543 0 R >> Helicopters come in a variety of sizes and shapes, but most share the same major components [10- 13] (Figure 1). >> /A 459 0 R endobj /Lang (EN-GB) 217 0 obj /Rotate 0 /Font << endobj << /K 128 nafems /ProcSet [/PDF /Text] /K 157 /Sh19 349 0 R << Large frames are required at the wing-fuselage and tail-fuselage interface to transmit the loads generated by these lifting surfaces into the fuselage. /S /Tabelle_content >> >> >> /Lang (EN-GB) /P 17 0 R /K 48 endobj /P 49 0 R /K 150 203 0 obj endobj /Prev 11 0 R 86 0 obj /A 476 0 R Frames also provide a means to introduce point loads into the fuselage. >> /K 19 /P 655 0 R >> The large rotating mass of the main rotor blades of a helicopter produce torque. >> /S /Tabelle_content >> << 0 endobj /Helv 9 0 R endobj >> /P 673 0 R /Lang (EN-GB) /K 51 /Lang (EN-GB) /Lang (EN-GB) /Fm3 298 0 R /S /Tabelle_content /Type /Page /Producer (Adobe PDF Library 15.0) endobj /K 49 /S /Tabelle_content 50 0 R 51 0 R 52 0 R 121 0 R] /S /Span Water lines (WL) designate location in the height of the aircraft, from ground up. 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. << >> endobj >> /Pg 35 0 R /TT1 312 0 R It's also one of the most complex in terms of its construction and operation. /P 438 0 R /CropBox [0.0 0.0 595.32 841.92] << /S /Normal 46 0 obj /Resources << endobj endobj /S /Subscript The load-bearing skins are attached to the stringers and frames of an aluminium aircraft through rivets. endobj application/pdf /S /P 1. /S /Tabelle_content >> /S /formula /K 18 /Lang (EN-GB) /Pg 42 0 R endobj endobj Single Rotor. /S /Tabelle_content -allows blades to flap up, down, lead, and lag, -Air cushion formed when hovering close to the ground /K [12 267 0 R] >> /Pg 35 0 R >> >> >> /Sh0 338 0 R /A 573 0 R /P 17 0 R /S /Tabelle_content << >> >> /K 5 /K 40 >> Frames are transverse elements that define the cross-section of the fuselage. endobj /K 20 /Parent 14 0 R /TT1 289 0 R /Contents 304 0 R 1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6 << >> 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 8 0 obj 224 0 obj The internal wing structure, consisting of spars, ribs and stringers, and the external wing, which is the skin. /Lang (EN-GB) /Parent 15 0 R /A 387 0 R http://www.zotero.org/styles/ieee >> /Fm1 296 0 R /TT0 310 0 R /S /Tabelle_content /P 501 0 R /Pg 35 0 R /S /Span >> Top customer satisfaction 4,2/5. /CS1 [/ICCBased 306 0 R] 179 0 obj endobj /TT0 289 0 R endobj /A 602 0 R endobj 125 0 obj /Pg 35 0 R >> Free shipping for many products! 250 0 obj /Outlines 4 0 R /P 610 0 R /Pg 35 0 R << >> 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. endobj >> << /Fm2 297 0 R /S /Tabelle_content /XObject << /Pg 35 0 R Compressor >> , " "" ( " ""), 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. /Shading << /ParentTree 18 0 R /P 17 0 R /Contents 369 0 R endobj /Pg 35 0 R /K 5 /P 109 0 R /Type /Page Modern Humanities Research Association 3rd edition (note with bibliography) /Pg 43 0 R The latter two are still in use. /K 33 << /S /Subscript /S /Artifact >> The constructor should then initialize the integer member of the class to represent the day specified by the month and day of month parameters. 209 0 obj << /Pg 24 0 R /Sh10 340 0 R /Count 4 /P 646 0 R << /Fm4 299 0 R of the year, the new value of the object will represent the first day of the year. Define the SHGC (solar heat gain coefficient), and explain how it differs from the SC (shading coefficient). /S /Subscript /TT1 313 0 R >> /K [21 270 0 R] << /P 73 0 R Landing loads introduced into the fuselage can be particularly severe if the landing is executed poorly. << /A 536 0 R Normally, it supports the tail rotor assembly, although some tail rotors are mounted on the tail cone of the boom. ciusss sud ouest; city of kent wa noise ordinance hours; what is the main idea of the albertosaurus mystery; mackenzie bezos new husband age >> /MediaBox [0.0 0.0 595.32 841.92] >> Nature /Resources << Helicopter cabins have a variety of seating arrangements. << 139 0 obj /Sh1 339 0 R >> /S /Subscript /K 19 Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment 198 0 obj /Superscript /Span endobj >> /ExtGState << /Annotation /Span /K 415 0 R >> /ExtGState << /A 629 0 R /P 17 0 R 1. iis express not working with ip address. endstream 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 115 0 obj /P 595 0 R 17 0 obj /ColorSpace << >> /K 38 /Pg 35 0 R /Pg 35 0 R 138 0 obj 192 0 obj 97 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] A few models have skids with two ground-handling wheels. >> << << >> << /Fm1 296 0 R /Tabs /S /K 132 /Pg 35 0 R /K 2 endobj >> /Parent 14 0 R Foot pedals A pair of foot pedals controls the tail rotor. /K 12 /TT3 336 0 R endobj << /CS0 [/ICCBased 287 0 R] << >> /P 530 0 R /P 570 0 R >> << /S /Tabelle_content /K 0 /A 396 0 R /K 148 /ExtGState << 177 0 R null 178 0 R null 179 0 R 180 0 R 181 0 R 182 0 R 183 0 R null /Pg 35 0 R /TT4 314 0 R << >> endobj >> << /Lang (EN-GB) Lugs are the most widely used connecting elements in aircraft. << 164 0 obj /P 17 0 R >> 107 0 obj For instance, 53 percent of the aircraft consists of carbon-fiber composite parts. -- prefix and postfix decrement operators. /TT2 312 0 R /Next 12 0 R If you missed part one, then perhaps go back and read this before continuing as this provides an overview on structural loading and design. Airframe design encompasses engineering, aerodynamics, materials technology, and manufacturing methods to achieve favorable balances of performance, reliability, and cost. 14 132 0 R 16 133 0 R 18 134 0 R 20] /dotlessi /lslash /oe /scaron /zcaron 160 /Euro 164 /currency 166 Fuselage The main body of the helicopter is known as the fuselage. /Font << /P 667 0 R uuid:ce5ad891-f06f-4f16-9f52-42c508d454cd /K 4 endobj >> -moves the thrust of the rotor and the lift of the helicopter, pulling it in the direction of the tip path plane. /P 73 0 R /CropBox [0.0 0.0 595.32 841.92] 84 0 obj /S /Tabelle_content endobj These external pressure loads combine with internal pressure loads if the aircraft is pressurized. << 47 0 obj << Piper PA-18 Super Cub with a Space Frame Fuselage. 243 0 obj 57 0 obj /Font << /S /P /A 383 0 R endobj endobj /P 525 0 R 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. >> /S /Normal /formula /P /MediaBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) 72 0 obj Panels were made with the same geometrical shape and dimensions but . << /S /P The structural system, or frame, is similar to the fuselage of an airplane. /MediaBox [0.0 0.0 595.32 841.92] 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. With this hinge, when one blade flaps up, the other flaps down. /Lang (EN-GB) /P 17 0 R endobj 122 0 obj /MediaBox [0.0 0.0 595.32 841.92] /P 17 0 R /Lang (EN-GB) /Lang (EN-US) /S /P endobj /S /Tabelle_content /Parent 4 0 R >> . endobj << /P 561 0 R endobj /Resources << /MediaBox [0.0 0.0 595.32 841.92] >> >> /Tabs /S /Pg 35 0 R /Pg 35 0 R 12 0 obj /P 17 0 R /Sh2 320 0 R >> /A 400 0 R << << /P 17 0 R /GS0 307 0 R /A 638 0 R endobj >> /K 12 20 0 obj endstream endobj startxref /Lang (EN-GB) /Pg 35 0 R Thin sheets of the material can be stacked in various ways to meet specific strength or . /Sh3 351 0 R /A 677 0 R >> endobj 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. endobj /K 5 /ExtGState << /S /Subscript /A 652 0 R /BaseFont /ZapfDingbats >> 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. 257 0 obj /CS0 [/ICCBased 287 0 R] 30 0 obj /P 17 0 R /Lang (EN-GB) >> /Lang (EN-GB) /Fm4 299 0 R /Lang (EN-GB) endobj >> >> /P 630 0 R endobj 61 0 obj /Fm3 298 0 R /P 96 0 R /Pg 43 0 R /Contents 328 0 R /P 431 0 R /Lang (EN-GB) >> /S /Normal [Figure 5]. /Pg 41 0 R 141 0 obj /ProcSet [/PDF /Text] >> >> /P 590 0 R >> /S /Tabelle_content /A 402 0 R /Pg 25 0 R endobj endobj /Pg 35 0 R >> /S /GoTo 232 0 obj Helicopter cabins have a variety of seating arrangements. << /Lang (EN-US) /S /Span << 221 0 obj >> /CS0 [/ICCBased 287 0 R]