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ANF Les Mureaux 113

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571: 106: 547: 26: 278:, which were relatively narrow and unbalanced, were set into the wing and had differential control in order to reduce the force needed to actuate them. The travel of the depressed aileron was less than that of the elevated aileron, which resulted in a gentler manoeuvre and diminishing the likeliness of a 253:. The internal structure featured two duralumin spars complete with a lightened web of sheet metal of 0 to 20 mm (0.4 to 0.8 in.) thick. These spars were of equal thickness to that of the wing with channel sections parallel to them, that were held in position by box crosspieces (instead of conventional 245:
or angle sections in the other. The latter sections were continuous and only flattened to accommodate the passage of the channel sections that ran parallel to the spars. On both the top and bottom of the fuselage, the strips were placed transversely, which facilitated the use of a rounded form with
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service in the "R2" two-seat reconnaissance role. ANF Les Mureaux opted to produce a clean-sheet response to this requirement. It was during this design work that the firm developed a new technique for metal construction, it was promptly incorporated into the new long distance observation aircraft,
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that had a typical width of 20 to 30 cm (7.87 to ll.81 inches); these could be given flanged edges as to permit their riveting together to form sheets. Occasionally, an alternative joining arrangement that used narrow angle pieces was harnessed instead. The structure of the aircraft consisted both
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was attached by screws inclined at 45-degrees with their heads covered by compact sliding plates. The wing's interior could be easily inspected by removing the leading edge. The wing tips were rounded and relatively thin. To diminish fatigue while in a dive, the fineness of the wing was increased
265:. The covering strips were placed at right angles to the spars and were riveted to their flanges and to the channel sections, but not to the box crosspieces, to obtain torsional rigidity. The spars were braced against each other via a series of tubes present the plane of each flange. 215:
to be equipped by the pilot. While the pilot was provided with an adjustable seat, the observer's seat was entirely removable. To optimise for both crew visibility and aerodynamic characteristics, the selected cross section for the aircraft's fuselage was
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The wing's covering comprised strips of sheet metal placed perpendicular to the spars and distributed across three zones, which were joined at the spar flanges. This covering had no other projections than the rivet heads, while the
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as the principal members, which were supported by an array of secondary spars and a channel section frame that were typically placed generally placed perpendicular to the covering strips to which they were
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to, changing them to closed sections best adapted to withstand local stresses. The rigidity of the covering was thus insured by the channel sections in one direction and either the strip
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Cortet, Pierre (April 1998). "La série des avions d'observation A.N.F. Les Mureaux 110 (photoscape)" [The A.N.F. Mureaux 110 Series of Observation Aircraft (Photospread)].
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from the engine; the fuel tank was also in a protected position within the fuselage, using two pumps to convey fuel to the engine. To reduce engine noise, it was equipped with a
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It was designed in response to a requirement issued by the French air ministry. Introduced to service during the 1930s, in excess of two hundred aircraft were procured for the
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shock absorber. To facilitate the installation of various powerplants, a removal support was present in the engine bay. Cooling for the engine was provided by a water-cooled
1134: 899:
Cortet, Pierre (October 1997). "La série des avions d'observation A.N.F. Les Mureaux 110 (1ère partie)" [The A.N.F. Mureaux 110 Series of Observation Aircraft].
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the least preliminary shaping; however, the sides featured covering strips that were parallel to the longerons, where the number of channel sections was reduced.
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nine more. By April 1940, 11 aircraft had been lost in action, leaving 228 on strength at the beginning of the Blitzkrieg in May. By the time of the French
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from reserve units as well. Multiple variants were operated by the service, perhaps most noteworthy was the conversion of 40 aircraft to serve as dedicated
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that had a stroke of 12 cm (4.72 in.) along with brakes. A shoe-type tail skid was fitted to the underside of the fuselage, it was mounted on an
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were presented to the air force for evaluation, and were ordered into production soon thereafter. The first mass-production version was the
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and its derivatives were a family of all-metal military reconnaissance aircraft developed and produced by the French aircraft manufacturer
261:, made up of channel sections, that supported 13 channel sections that ran parallel to the spars and were joined to the crosspieces using 721: 1239: 1120: 249:
The wing was constructed using similar principals to that of the fuselage; it was supported by a pair of tubular struts and the
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Cortet, Pierre (February 1998). "La série des avions d'observation A.N.F. Les Mureaux 110 (5ème partie)".
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Cortet, Pierre (December 1997). "La série des avions d'observation A.N.F. Les Mureaux 110 (3ème partie)".
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Cortet, Pierre (November 1997). "La série des avions d'observation A.N.F. Les Mureaux 110 (2ème partie)".
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Cortet, Pierre (January 1998). "La série des avions d'observation A.N.F. Les Mureaux 110 (4ème partie)".
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The ANF Les Mureaux 110 originated with a French air ministry requirement for an aircraft to replace the
1085:"The Mureaux 111 R.2 military airplane (French) : a long-distance all-metal observation monoplane" 984:
Cortet, Pierre (March 1998). "La série des avions d'observation A.N.F. Les Mureaux 110 (6ème partie)".
474:- racing version, equipped with a supercharged Hispano-Suiza 12Ybrs piston engine. Only one was built. 1193: 1188: 646: 531: 521: 511: 499: 489: 441: 161: 1071:(in French). No. Salon 1934. 16 November – 2 December 1934. p. 65 – via Gallica BNF. 1208: 1203: 1198: 1173: 279: 65: 690: 451: 431: 419: 409: 229: 1102: 1067: 1023: 1006: 989: 972: 955: 938: 921: 904: 310: 306: 559: 373: 207:
designed specifically for aerial reconnaissance. Both the pilot and observer were seated in
141: 137: 125: 76: 257:) at intervals of roughly one meter (39.37 inches). These crosspieces constituted a Warren 1143: 118: 54: 220:, having a shorter base down and flat sides while both the top and bottom were rounded. 290: 184:
in 1933, of which 49 examples were purchased. This was supplanted in production by the
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open cockpits; these cockpits were relatively spacious, permitting multiple styles of
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to equipment not just its frontline units but also to displace aircraft such as the
520:- one 113 modified to challenge world altitude record with 500 kg payload, 1x 393: 286: 270: 1107: 192:
later than year. Both these series were given light bombing capability as well.
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on June 25, only 62 aircraft remained intact, some of which were stationed in
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Cortet, Pierre (March 1999). "Rétros du Mois" [Retros of the Month].
1010: 993: 976: 959: 942: 925: 908: 305:, the rate of cooling being adjustable via a shutter. Both the oil tanks and 700: 224: 217: 212: 204: 201: 144:. However, all remaining aircraft were all scrapped in the aftermath of the 1112: 223:
Being largely composed of metal, the fuselage covering comprised strips of
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328 km/h (204 mph, 177 kn) at 3,500 m (11,500 ft)
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was relatively wide and lacked a continuous axle. It was equipped with a
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Curnel, J.; Leyvastre (March 1974). "La lignée des A.N.F. 110 (1)".
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Curnel, J.; Leyvastre (July 1974). "La lignée des A.N.F. 110 (5)".
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Curnel, J.; Leyvastre (June 1974). "La lignée des A.N.F. 110 (4)".
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entered service initially with the Armée de l'Air's reconnaissance
569: 510:- reconnaissance bomber with revised aerodynamics (115 built), 1x 238: 104: 574:
Mureaux 111 R.2 3-view drawing from NACA Aircraft Circular No.142
1116: 462:- initial production version (Hispano-Suiza 12Ybrs) - 49 built 440:- the 110 prototypes re-engined as pre-production machines, 1x 254: 745: 488:- reconnaissance bomber with upgraded engine (119 built), 1x 882: 870: 482:- single prototype of a purpose-built night fighter version 365:
that were still in service with France's two night fighter
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24 minutes and 50 seconds to 8,000 m (26,000 ft)
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1,000 L (220 imp gal; 260 US gal)
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were deliberately placed on the opposite side of the
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1 × flexible 7.5 mm MAC 34 machine gun for observer
345:reserve units. It was followed into service by the 95: 90: 82: 72: 60: 48: 40: 35: 18: 498:- this version was powered by a 634-kW (850-hp) 1063:"Le Salon: Les Appareils: A.N.F. - Les Mureaux" 1245:1930s French military reconnaissance aircraft 1128: 8: 1020:Avions: Toute l'aéronautique et son histoire 1003:Avions: Toute l'aéronautique et son histoire 986:Avions: Toute l'aéronautique et son histoire 969:Avions: Toute l'aéronautique et son histoire 952:Avions: Toute l'aéronautique et son histoire 935:Avions: Toute l'aéronautique et son histoire 918:Avions: Toute l'aéronautique et son histoire 901:Avions: Toute l'aéronautique et son histoire 353:. Between 1934 and 1935, 40 of the original 1089:National Advisory Committee for Aeronautics 1135: 1121: 1113: 200:The ANF Les Mureaux 111 was an all-metal, 15: 1057:(in French). No. 57. pp. 14–15. 1048:(in French). No. 56. pp. 12–16. 1039:(in French). No. 53. pp. 20–25. 839: 837: 670:1,500 km (620 mi, 540 nmi) 140:, and thus saw intense combat during the 818: 816: 814: 812: 784: 782: 772: 770: 768: 758: 756: 754: 633:3,450 kg (7,606 lb) (overload) 408:- two examples built for evaluation, 1x 738: 468:- 40 113s converted into night fighters 430:- one example built for evaluation, 1x 1092:, 1 April 1931. NACA-AC-142, 93R19626. 530:- Prototype observation aircraft, 1x 172:Two slightly different variants, the 7: 621:34.90 m (375.7 sq ft) 609:15.40 m (50 ft 6 in) 337:, and finally replacing the ageing 1055:L'Album du fanatique de L'Aviation 1046:L'Album du fanatique de L'Aviation 1037:L'Album du fanatique de L'Aviation 722:List of Interwar military aircraft 615:3.44 m (11 ft 3 in) 603:9.98 m (32 ft 9 in) 14: 746:Curnel & Leyvastre March 1974 883:Curnel & Leyvastre July 1974 871:Curnel & Leyvastre June 1974 545: 44:Military reconnaissance aircraft 24: 1250:Single-engined tractor aircraft 1078:Jane's Encyclopedia of Aviation 582:La lignée des A.N.F Mureaux 110 1080:. London, UK: Studio Editions. 1076:Taylor, Michael J. H. (1989). 333:, followed by the observation 1: 627:1,757 kg (3,874 lb) 382:Groupes Aériens d'Observation 1260:Aircraft first flown in 1931 703:firing through ventral hatch 693:firing through propeller hub 301:installed within the engine 699:1× flexibly mounted 7.7 mm 649:, 640 kW (860 hp) 165:which was later designated 1276: 361:and used to replace those 1005:(in French) (61): 16–19. 971:(in French) (59): 19–28. 954:(in French) (58): 20–31. 937:(in French) (57): 32–36. 920:(in French) (56): 28–32. 903:(in French) (55): 19–24. 566:Specifications (115 R2B2) 343:Groupes Aériens Régionaux 23: 1240:ANF Les Mureaux aircraft 988:(in French) (60): 7–15. 706:200 kg (440 lb) of bombs 597:two (pilot and observer) 588:General characteristics 372:By the outbreak of the 274:from 20.5 to 22.9. The 575: 390:armistice with Germany 357:s were converted into 146:armistice with Germany 110: 109:ANF Les Mureaux 115 R2 30:A Mureaux 113 in 1931. 1255:Parasol-wing aircraft 1022:(in French) (72): 5. 573: 108: 806:NACA 1931, pp. 2, 4. 647:Hispano-Suiza 12Ycrs 532:Hispano-Suiza 12Ycrs 522:Hispano-Suiza 12Ybrs 512:Hispano-Suiza 12Ybrs 500:Hispano-Suiza 12Yers 490:Hispano-Suiza 12Ycrs 442:Hispano-Suiza 12Ybrs 861:NACA 1931, pp. 4-5. 852:NACA 1931, pp. 3-4. 843:NACA 1931, pp. 2-3. 797:NACA 1931, pp. 1-2. 321:Operational history 115:ANF Les Mureaux 110 36:General information 691:MAC 34 machine gun 576: 432:Hispano-Suiza 12Nb 420:Hispano-Suiza 12Nb 410:Hispano-Suiza 12Nb 111: 1227: 1226: 674:Time to altitude: 307:fire extinguisher 103: 102: 1267: 1137: 1130: 1123: 1114: 1081: 1072: 1058: 1049: 1040: 1031: 1014: 997: 980: 963: 946: 929: 912: 886: 885:, pp. 14–15 880: 874: 868: 862: 859: 853: 850: 844: 841: 832: 831:NACA 1931, p. 2. 829: 823: 822:NACA 1931, p. 3. 820: 807: 804: 798: 795: 789: 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400:Variants 311:firewall 299:radiator 276:ailerons 61:Designer 613:Height: 601:Length: 534:engine. 524:engine. 514:engine. 434:engine. 422:engine. 367:Groupes 341:in the 335:Groupes 331:Groupes 303:cowling 263:gussets 243:flanges 239:riveted 91:History 1209:190C.1 1204:180C.2 1199:170C.1 1026:  1009:  992:  975:  958:  941:  924:  907:  668:Range: 553:France 550:  528:200A.3 496:115 R2 480:114 CN 472:113 GR 466:113 CN 460:113 R2 448:112 GR 438:112 R2 416:110A-2 376:, the 259:girder 251:cabane 209:tandem 196:Design 1152:Types 595:Crew: 230:spars 1194:160T 1189:140T 1024:ISSN 1007:ISSN 990:ISSN 973:ISSN 956:ISSN 939:ISSN 922:ISSN 905:ISSN 645:1 × 349:and 325:The 285:The 255:ribs 232:and 176:and 113:The 86:~285 41:Type 1214:200 1184:131 1179:130 1174:120 1169:110 518:119 428:111 406:110 386:117 378:115 355:113 351:115 347:117 327:113 190:117 186:115 182:113 178:111 174:110 167:111 160:in 1236:: 1065:. 836:^ 811:^ 781:^ 767:^ 753:^ 396:. 369:. 317:. 282:. 169:. 148:. 121:. 1164:4 1159:3 1136:e 1129:t 1122:v 1030:. 1013:. 996:. 979:. 962:. 945:. 928:. 911:.

Index


Manufacturer
ANF Les Mureaux
André Brunet
French Air Force

ANF Les Mureaux
French Air Force
Potez 25s
night fighters
Second World War
Battle of France
armistice with Germany
Breguet 19
Armée de l'Air
parasol-wing
monoplane
tandem
parachute
trapezoidal
duralumin
spars
longerons
riveted
flanges
cabane
ribs
girder
gussets
leading edge

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