Knowledge (XXG)

Krueger flap

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leading edge, so the stowed panels are nominally flat, albeit twisted a small amount along the leading edge of the wing. Using two sets of identical linkages per flap, the fiberglass panel is deployed and bent to an optimal aerodynamic shape for low speed flight, while a separate aluminum folding nose that is stowed inside the wing is deployed tangent to the fiberglass panel.
102:. Conversely, slats extend forwards from the upper surface of the leading edge. Also, when deployed, Krueger flaps result in a much more pronounced blunt leading edge on the wing, helping to achieve better low-speed handling. This allows smaller-radius wing leading edges, better optimized for cruise. Leading edge Krueger flaps enhance wing's low speed 204: 133:
Invented by James B. Cole and Richard H. Weiland of Boeing in the mid-1960s, the "VCK" (Variable Camber Krueger) flaps deployed from the lower leading edge of the wing similar to rigid panel Krueger flaps. The high speed lower wing in that region of the wing is a straight line normal to the wing
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vertical tail. The left wing was modified to include a 6.7 m-span glove section supporting a variable-camber Krueger flap to be deployed during landing, protruding just ahead of the leading edge. Although Krueger flaps had been tried before as insect-mitigation screens, previous designs caused
192: 230:(NLF) on an aircraft wing can reduce fuel burn by as much as 15%, but even small contaminants from insect remains could trip the flow from laminar to turbulent, destroying the performance benefit. The test flights were supported by the European airline group 90:(in those cases where there is a gap or slot between the flap trailing edge and wing leading edge), they are deployed differently. Krueger flaps, hinged at their foremost position, hinge forwards from the under surface of the wing, increasing the 184:
using a fixed flap and a skid on the after-body. After the Boeing test flight on the B-707 prototype on 15 July 1954, Krueger flaps were first used in production for the Boeing 727 which made its maiden flight on 9 February 1963.
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used Krueger flaps on the wing leading edge. Several modern aircraft use Krueger flaps between the fuselage and closest engine, but use
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additional drag. The newer design is variable-camber and retracts as seamlessly as possible into the lower wing surface. Increasing
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in 1943 and evaluated in the wind tunnels in Göttingen, Germany. One of the earliest civil applications was the
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with an extreme attitude take-off with the tail dragging on the runway, a scenario that had caused two
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also used a mix of inboard Krueger flaps and outboard slats, although it had no engine between them.
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wing was redesigned with optimized VCK flap panels that were similar to the original 747.
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material and were designed to be intentionally distorted into a much more efficient
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Aircraft Flight Instruments and Guidance Systems: Principles, Operations and ...
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as part of the agency’s Environmentally Responsible Aviation (ERA) program.
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While the aerodynamic effect of Krueger flaps may be similar to that of
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X-Planes of Europe II, Tony Buttler Hikoki Puplication 2015. Page 193.
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J. B. Cole (Dec 17, 1966), Design of the Variable Camber Flap
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conducted a series of test flights in 2015 with a modified
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accidents. A preliminary flight test had been made on the
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fighter which flew in 1955. The flap was added to prevent
42:, are lift enhancement devices that may be fitted to the 221:, incorporating new wing-leading-edge sections and an 1379: 1358: 1291: 1187: 1022: 888: 725: 541: 460:"757 EcoDemo Focuses On Laminar And Active Flow" 515: 144:Another airplane that used VCK flaps was the 8: 522: 508: 500: 168:claimed the first use of the flap in its 18: 264: 187: 488:, London: Universal Books Ltd., 1990. 7: 1488:German inventions of the Nazi period 425:Hitchens, Frank (25 November 2015). 365:Niels KluĂźmann; Arnim Malik (2012). 118:The Krueger flaps developed for the 70:outboard of the closest engine. The 14: 275:Ace the Technical Pilot Interview 428:The Encyclopedia of Aerodynamics 202: 190: 23:Krueger flaps deployed from the 305:Wyatt, David (21 August 2014). 1432:In-flight entertainment system 1129:Horizontal situation indicator 462:. Aviation Week. 23 March 2015 156:KrĂĽger flaps were invented by 31:(top left and right in photo). 1: 1412:Environmental control system 278:. McGraw-Hill Professional. 164:, whereas the Swiss company 114:Variable Camber Krueger Flap 371:. Springer. pp. 193–. 234:and conducted jointly with 182:Boeing 367-80 (the Dash 80) 1514: 1089:Course deviation indicator 780:Electro-hydraulic actuator 1320:Conventional landing gear 106:production especially on 1483:Aircraft wing components 1104:Flight management system 272:Gary V. Bristow (2002). 98:. It produces a nose-up 1407:Emergency oxygen system 1169:Turn and slip indicator 964:Leading-edge droop flap 934:Drag-reducing aerospike 909:Adaptive compliant wing 904:Active Aeroelastic Wing 130:section on deployment. 1447:Passenger service unit 1248:Self-sealing fuel tank 1144:Multi-function display 197:Krueger flap operation 122:were constructed from 32: 1427:Ice protection system 1345:Tricycle landing gear 1335:Landing gear extender 552:Aft pressure bulkhead 368:Lexikon Der Luftfahrt 346:U.S. Patent 3,504,870 22: 1473:Aircraft wing design 1392:Auxiliary power unit 800:Flight control modes 337:Taylor 1990, p. 114. 228:natural laminar flow 1371:Escape crew capsule 1278:War emergency power 1149:Pitot–static system 994:Variable-sweep wing 702:Vertical stabilizer 96:coefficient of lift 1079:Attitude indicator 1059:Airspeed indicator 1054:Aircraft periscope 486:The Lore of Flight 484:Taylor, John W.R. 248:Flap (aeronautics) 178:de Havilland Comet 33: 16:Aerodynamic device 1478:Aircraft 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Retrieved 454: 442:. Retrieved 427: 420: 403: 387: 367: 360: 351: 342: 333: 321:. Retrieved 307: 300: 289:. Retrieved 274: 267: 213: 155: 146:Boeing YC-14 143: 139:Boeing 747-8 136: 132: 117: 110:aircraft. 94:and maximum 81: 44:leading edge 40:KrĂĽger flaps 39: 35: 34: 25:leading edge 1350:Tundra tire 1233:Intake ramp 1164:Transponder 949:Gurney flap 890:Aerodynamic 805:Fly-by-wire 687:Triple tail 92:wing camber 56:droop flaps 1467:Categories 1340:Oleo strut 1228:Inlet cone 1223:Gascolator 1189:Propulsion 1179:Yaw string 1174:Variometer 1030:instrument 1009:Wing fence 944:Gouge flap 919:Blown flap 875:Yaw damper 850:Stabilator 835:Side-stick 770:Dive brake 657:Stabilizer 632:Lift strut 622:Jury strut 291:2009-02-16 259:References 219:Boeing 757 174:wing stall 162:Boeing 707 124:fiberglass 120:Boeing 747 108:swept wing 72:Boeing 727 64:Boeing 747 60:Boeing 707 29:Boeing 747 1315:Autobrake 1243:NACA duct 1218:Fuel tank 1208:Drop tank 1191:controls, 1074:Astrodome 1064:Altimeter 929:Dog-tooth 894:high-lift 845:Spoileron 830:Servo tab 810:Gust lock 765:Deceleron 750:Autopilot 707:Wing root 692:Twin tail 677:Tailplane 612:Hardpoint 582:Empennage 545:structure 78:Operation 50:. 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Index


leading edge
Boeing 747
leading edge
wing
slats
droop flaps
Boeing 707
Boeing 747
slats
Boeing 727
slats
slots
wing camber
coefficient of lift
pitching moment
lift
swept wing
Boeing 747
fiberglass
aerofoil
Boeing 747-8
Boeing YC-14
Werner KrĂĽger
Boeing 707
FFA
FFA P-16
wing stall
de Havilland Comet
Boeing 367-80 (the Dash 80)

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