582:
117:
558:
37:
289:, 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
264:. 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
256:
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
175:
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,
238:
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
284:
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
276:. 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.
226:
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
279:
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
247:
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
252:
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
1255:
1012:
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)].
324:
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
135:
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
308:
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
1145:
910:
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].
257:
the least preliminary shaping; however, the sides featured covering strips that were parallel to the longerons, where the number of channel sections was reduced.
399:
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
143:
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
1099:
400:
156:
1260:
304:
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
1138:
1270:
191:
were presented to the air force for evaluation, and were ordered into production soon thereafter. The first mass-production version was the
128:
and its derivatives were a family of all-metal military reconnaissance aircraft developed and produced by the French aircraft manufacturer
272:, made up of channel sections, that supported 13 channel sections that ran parallel to the spars and were joined to the crosspieces using
732:
1250:
1131:
260:
The wing was constructed using similar principals to that of the fuselage; it was supported by a pair of tubular struts and the
1073:
1265:
581:
1229:
309:
978:
Cortet, Pierre (February 1998). "La série des avions d'observation A.N.F. Les
Mureaux 110 (5ème partie)".
944:
Cortet, Pierre (December 1997). "La série des avions d'observation A.N.F. Les
Mureaux 110 (3ème partie)".
927:
Cortet, Pierre (November 1997). "La série des avions d'observation A.N.F. Les
Mureaux 110 (2ème partie)".
60:
961:
Cortet, Pierre (January 1998). "La série des avions d'observation A.N.F. Les
Mureaux 110 (4ème partie)".
167:
The ANF Les
Mureaux 110 originated with a French air ministry requirement for an aircraft to replace the
1096:"The Mureaux 111 R.2 military airplane (French) : a long-distance all-metal observation monoplane"
995:
Cortet, Pierre (March 1998). "La série des avions d'observation A.N.F. Les
Mureaux 110 (6ème partie)".
485:- racing version, equipped with a supercharged Hispano-Suiza 12Ybrs piston engine. Only one was built.
1204:
1199:
657:
542:
532:
522:
510:
500:
452:
172:
1082:(in French). No. Salon 1934. 16 November – 2 December 1934. p. 65 – via Gallica BNF.
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designed specifically for aerial reconnaissance. Both the pilot and observer were seated in
152:
148:
136:
87:
268:) at intervals of roughly one meter (39.37 inches). These crosspieces constituted a Warren
1154:
129:
65:
231:, having a shorter base down and flat sides while both the top and bottom were rounded.
301:
195:
in 1933, of which 49 examples were purchased. This was supplanted in production by the
116:
222:
open cockpits; these cockpits were relatively spacious, permitting multiple styles of
1244:
1194:
1189:
1174:
1169:
369:
261:
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to equipment not just its frontline units but also to displace aircraft such as the
531:- one 113 modified to challenge world altitude record with 500 kg payload, 1x
404:
297:
281:
17:
1118:
203:
later than year. Both these series were given light bombing capability as well.
1095:
403:
on June 25, only 62 aircraft remained intact, some of which were stationed in
373:
305:
168:
1038:
1029:
Cortet, Pierre (March 1999). "Rétros du Mois" [Retros of the Month].
1021:
1004:
987:
970:
953:
936:
919:
316:, the rate of cooling being adjustable via a shutter. Both the oil tanks and
711:
235:
228:
223:
215:
212:
155:. However, all remaining aircraft were all scrapped in the aftermath of the
1123:
234:
Being largely composed of metal, the fuselage covering comprised strips of
675:
328 km/h (204 mph, 177 kn) at 3,500 m (11,500 ft)
349:
300:
was relatively wide and lacked a continuous axle. It was equipped with a
244:
140:
325:
313:
286:
36:
563:
273:
269:
253:
219:
1046:
Curnel, J.; Leyvastre (March 1974). "La lignée des A.N.F. 110 (1)".
1064:
Curnel, J.; Leyvastre (July 1974). "La lignée des A.N.F. 110 (5)".
1055:
Curnel, J.; Leyvastre (June 1974). "La lignée des A.N.F. 110 (4)".
340:
entered service initially with the Armée de l'Air's reconnaissance
580:
521:- reconnaissance bomber with revised aerodynamics (115 built), 1x
249:
115:
585:
Mureaux 111 R.2 3-view drawing from NACA Aircraft Circular No.142
1127:
473:- initial production version (Hispano-Suiza 12Ybrs) - 49 built
451:- the 110 prototypes re-engined as pre-production machines, 1x
265:
756:
499:- reconnaissance bomber with upgraded engine (119 built), 1x
893:
881:
493:- single prototype of a purpose-built night fighter version
376:
that were still in service with France's two night fighter
687:
24 minutes and 50 seconds to 8,000 m (26,000 ft)
650:
1,000 L (220 imp gal; 260 US gal)
147:. The family was in widespread usage at the start of the
461:- one specially-built aircraft to participate in 1934
320:
were deliberately placed on the opposite side of the
1162:
707:
1 × flexible 7.5 mm MAC 34 machine gun for observer
356:reserve units. It was followed into service by the
106:
101:
93:
83:
71:
59:
51:
46:
29:
509:- this version was powered by a 634-kW (850-hp)
1074:"Le Salon: Les Appareils: A.N.F. - Les Mureaux"
1256:1930s French military reconnaissance aircraft
1139:
8:
1031:Avions: Toute l'aéronautique et son histoire
1014:Avions: Toute l'aéronautique et son histoire
997:Avions: Toute l'aéronautique et son histoire
980:Avions: Toute l'aéronautique et son histoire
963:Avions: Toute l'aéronautique et son histoire
946:Avions: Toute l'aéronautique et son histoire
929:Avions: Toute l'aéronautique et son histoire
912:Avions: Toute l'aéronautique et son histoire
364:. Between 1934 and 1935, 40 of the original
1100:National Advisory Committee for Aeronautics
1146:
1132:
1124:
211:The ANF Les Mureaux 111 was an all-metal,
26:
1068:(in French). No. 57. pp. 14–15.
1059:(in French). No. 56. pp. 12–16.
1050:(in French). No. 53. pp. 20–25.
850:
848:
681:1,500 km (620 mi, 540 nmi)
151:, and thus saw intense combat during the
829:
827:
825:
823:
795:
793:
783:
781:
779:
769:
767:
765:
644:3,450 kg (7,606 lb) (overload)
419:- two examples built for evaluation, 1x
749:
479:- 40 113s converted into night fighters
441:- one example built for evaluation, 1x
1103:, 1 April 1931. NACA-AC-142, 93R19626.
541:- Prototype observation aircraft, 1x
183:Two slightly different variants, the
7:
632:34.90 m (375.7 sq ft)
620:15.40 m (50 ft 6 in)
348:, and finally replacing the ageing
1066:L'Album du fanatique de L'Aviation
1057:L'Album du fanatique de L'Aviation
1048:L'Album du fanatique de L'Aviation
733:List of Interwar military aircraft
626:3.44 m (11 ft 3 in)
614:9.98 m (32 ft 9 in)
25:
757:Curnel & Leyvastre March 1974
894:Curnel & Leyvastre July 1974
882:Curnel & Leyvastre June 1974
556:
55:Military reconnaissance aircraft
35:
1261:Single-engined tractor aircraft
1089:Jane's Encyclopedia of Aviation
593:La lignée des A.N.F Mureaux 110
1091:. London, UK: Studio Editions.
1087:Taylor, Michael J. H. (1989).
344:, followed by the observation
1:
638:1,757 kg (3,874 lb)
393:Groupes Aériens d'Observation
1271:Aircraft first flown in 1931
714:firing through ventral hatch
704:firing through propeller hub
312:installed within the engine
710:1× flexibly mounted 7.7 mm
660:, 640 kW (860 hp)
176:which was later designated
1287:
372:and used to replace those
1016:(in French) (61): 16–19.
982:(in French) (59): 19–28.
965:(in French) (58): 20–31.
948:(in French) (57): 32–36.
931:(in French) (56): 28–32.
914:(in French) (55): 19–24.
577:Specifications (115 R2B2)
354:Groupes Aériens Régionaux
34:
1251:ANF Les Mureaux aircraft
999:(in French) (60): 7–15.
717:200 kg (440 lb) of bombs
608:two (pilot and observer)
599:General characteristics
383:By the outbreak of the
285:from 20.5 to 22.9. The
586:
401:armistice with Germany
368:s were converted into
157:armistice with Germany
121:
120:ANF Les Mureaux 115 R2
41:A Mureaux 113 in 1931.
1266:Parasol-wing aircraft
1033:(in French) (72): 5.
584:
119:
817:NACA 1931, pp. 2, 4.
658:Hispano-Suiza 12Ycrs
543:Hispano-Suiza 12Ycrs
533:Hispano-Suiza 12Ybrs
523:Hispano-Suiza 12Ybrs
511:Hispano-Suiza 12Yers
501:Hispano-Suiza 12Ycrs
453:Hispano-Suiza 12Ybrs
872:NACA 1931, pp. 4-5.
863:NACA 1931, pp. 3-4.
854:NACA 1931, pp. 2-3.
808:NACA 1931, pp. 1-2.
332:Operational history
126:ANF Les Mureaux 110
47:General information
18:ANF Les Mureaux 200
702:MAC 34 machine gun
587:
443:Hispano-Suiza 12Nb
431:Hispano-Suiza 12Nb
421:Hispano-Suiza 12Nb
122:
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685:Time to altitude:
318:fire extinguisher
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16:(Redirected from
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787:NACA 1931, p. 5.
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429:- prototype, 1x
385:Second World War
199:in 1935 and the
153:Battle of France
149:Second World War
137:French Air Force
88:French Air Force
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107:First flight
94:Number built
84:Primary user
77:André Brunet
61:Manufacturer
1079:L'Aérophile
700:1 × 7.5 mm
666:Performance
654:Powerplant:
463:Bibescu Cup
374:Breguet 19s
229:trapezoidal
163:Development
1245:Categories
739:References
630:Wing area:
395:, and the
169:Breguet 19
110:April 1931
30:110 family
1119:airwar.ru
1039:1243-8650
1022:1243-8650
1005:1243-8650
988:1243-8650
971:1243-8650
954:1243-8650
937:1243-8650
920:1243-8650
744:Citations
712:Lewis gun
618:Wingspan:
590:Data from
550:Operators
350:Potez 25s
326:silencers
291:side slip
245:longerons
236:duralumin
224:parachute
216:monoplane
141:Potez 25s
1157:aircraft
722:See also
693:Armament
519:117 R2B2
503:engine.
497:115 R2B2
465:air race
455:engine.
423:engine.
411:Variants
322:firewall
310:radiator
287:ailerons
72:Designer
624:Height:
612:Length:
545:engine.
535:engine.
525:engine.
445:engine.
433:engine.
378:Groupes
352:in the
346:Groupes
342:Groupes
314:cowling
274:gussets
254:flanges
250:riveted
102:History
1220:190C.1
1215:180C.2
1210:170C.1
1037:
1020:
1003:
986:
969:
952:
935:
918:
679:Range:
564:France
561:
539:200A.3
507:115 R2
491:114 CN
483:113 GR
477:113 CN
471:113 R2
459:112 GR
449:112 R2
427:110A-2
387:, the
270:girder
262:cabane
220:tandem
207:Design
1163:Types
606:Crew:
241:spars
1205:160T
1200:140T
1035:ISSN
1018:ISSN
1001:ISSN
984:ISSN
967:ISSN
950:ISSN
933:ISSN
916:ISSN
656:1 ×
360:and
336:The
296:The
266:ribs
243:and
187:and
124:The
97:~285
52:Type
1225:200
1195:131
1190:130
1185:120
1180:110
529:119
439:111
417:110
397:117
389:115
366:113
362:115
358:117
338:113
201:117
197:115
193:113
189:111
185:110
178:111
171:in
1247::
1076:.
847:^
822:^
792:^
778:^
764:^
407:.
380:.
328:.
293:.
180:.
159:.
132:.
1175:4
1170:3
1147:e
1140:t
1133:v
1041:.
1024:.
1007:.
990:.
973:.
956:.
939:.
922:.
20:)
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