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Potez 37

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in April 1931, with all prototypes bar the Breguet gathered together. The selection process was unusually long and, while it continued, a second Potez 37 was completed and began testing. It had been fitted with a new radiator and preliminary flights suggested it was faster. In April 1932, after a
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The date of the first flight of the Potez 37 is not known but test flights, flown by Lemoine, were under way by June 1930. Lemoine and Duroyon continued development flying until at least the end of July. They reported agreeable and straightforward handling characteristics.
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The Potez 37 had fixed, conventional landing gear, with mainwheels, equipped with brakes, placed 3.0 m (9 ft 10 in) apart at the ends of half-axles and drag struts hinged to the fuselage. The wheels had near-vertical
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and tips. There was a rounded cut-out in the centre-section's trailing edge to assist the pilot's upward view. Generous ailerons filled much of the trailing edges outboard. Structurally each outer panel was built around two steel
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mounting and small side-windows. Immediately aft the girder cross-section was reduced rapidly, then joined to the final part of the fuselage, an unusual truncated dural cone strengthened internally with longerons and frames.
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The French R.2 specification of 1928 called for an all-metal two seat reconnaissance aircraft, fast and with a rapid climb rate and large radius of action. It led to prototypes from eight manufacturers, the
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The fuselage was in three parts. The forward part mounted the Hispano-Suiza V-12 engine within a close-fitting, sheet metal cowling that followed the cylinder banks and with a curved, transverse
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mounted on the forward wing struts at a point reinforced by extra struts to the upper fuselage and to the base of the rear wing strut. There was a small, sprung tailskid.
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Les Ailles gives the airfoil as Clark VH, which exists, but also notes the same airfoil was used on the Potez 39. This had the much more widely used Clark YH.
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and with two outer panels, each mounted at about half-span on a parallel pair of struts from the lower fuselage. Like all the struts, these were enclosed in
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under its rear. Behind the engine the fuselage structure was a conventional rectangular section girder frame bearing wing struts and
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Bernard, Martin; Sparrow, Dave; Espérou, Bernard (September 2012). "F-1922 – The French Civil Register from 1922".
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Aircraft circulars Of the National Advisory Committee for Aeronautics no.152 – Potez 37R2 military airplane
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in September 1933. Starting on 9 September the eight prototypes, led by Jonchay in the Potez, flew from
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government contract. It flew in mid-1930 but did not win the competition, so only two were completed.
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was mounted just above the fuselage on the fin; supported on inverted V-struts from below, its
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wing aircraft. Its wing was in three parts, with a small centre-section attached to the upper
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year of contest, the ANF-Mureax 111 was declared winner so no more Potez 37s were built.
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From 1930 to 1938 French military prototypes appeared on the Civil Register in the
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One at least was still flying about eighteen months later and took part in the 3rd
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and dural covered; the leading edges were readily removable.
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Potez 37 3-view drawing from NACA aircraft Circular No.152
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The tail unit was conventional, with a blunted triangular
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264 km/h (164 mph, 143 kn) at ground level
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In plan the wings had straight, unswept 721:"Le Tour de France des Avions Prototypes" 562: 560: 558: 556: 554: 510: 479: 390:340 kg (750 lb) including oil 677:"D'aérodrome en aérodrome – A Meaulte" 659:"D'aérodrome en aérodrome – A Meaulte" 623:"D'aérodrome en aérodrome – A Meaulte" 431:7,500 m (24,600 ft) absolute 18: 437:8 min to 3,000 m (9,800 ft) 7: 345:10.285 m (33 ft 9 in) 351:14.20 m (46 ft 7 in) 567:Frachet, André (4 December 1930). 357:3.50 m (11 ft 6 in) 14: 239:could be adjusted in flight. The 174:but were mildly curved over the 27: 363:35 m (380 sq ft) 158:on two outward-leaning, N-form 294:group. The first Potez 37 was 1: 727:(639): 14. 14 September 1933. 665:(535): 12. 17 September 1931. 569:"L'avion Henry Potez 37-R. 2" 384:2,536 kg (5,591 lb) 378:1,574 kg (3,470 lb) 281:Tour de France du Prototypes 683:(541): 12. 29 October 1931. 593:(147): 279–80. August 1931. 404:, 510 kW (680 hp) 94:was a two-seat, long range 1133: 701:. 14 April 1932. p. 3 647:(514): 18. 23 March 1931. 468:. Washington: NACA. 1931. 26: 21: 629:(476): 12. 31 July 1930. 611:(471): 12. 26 June 1930. 525:(147): 275. August 1931. 449:205 m (673 ft) 443:190 m (620 ft) 224:mounting a curved, deep 129:Nieuport-Delage Ni-D 580 500:Aviafrance Potez 37-R.2 330:General characteristics 325:Les Ailes December 1930 98:built to compete for a 96:reconnaissance aircraft 40:Reconnaissance aircraft 547:(V): 145. 15 May 1931. 319: 65:Aéroplanes Henry Potez 1107:Parasol-wing aircraft 317: 780:Potez and Potez-CAMS 740:Air Britain Archive 204:and containing two 150:The Potez 37 was a 398:Hispano-Suiza 12Nb 320: 237:angle of incidence 141:Hispano-Suiza 12Nb 1094: 1093: 435:Time to altitude: 88: 87: 1124: 773: 766: 759: 750: 744: 743: 735: 729: 728: 717: 711: 710: 708: 706: 699:Le Petit Parisen 691: 685: 684: 673: 667: 666: 655: 649: 648: 637: 631: 630: 619: 613: 612: 601: 595: 594: 583: 577: 576: 564: 549: 548: 533: 527: 526: 515: 487: 484: 469: 467: 429:Service ceiling: 418: 332: 81: 51: 43:Type of aircraft 31: 19: 1132: 1131: 1127: 1126: 1125: 1123: 1122: 1121: 1097: 1096: 1095: 1090: 1064: 783: 777: 747: 737: 736: 732: 719: 718: 714: 704: 702: 693: 692: 688: 675: 674: 670: 657: 656: 652: 639: 638: 634: 621: 620: 616: 603: 602: 598: 587:"Potez 37 R. 2" 585: 584: 580: 566: 565: 552: 535: 534: 530: 517: 516: 512: 508: 496: 491: 490: 485: 481: 476: 465: 459: 456: 454:Further reading 414: 328: 312: 298:and the second 261: 253:shock absorbers 243:were narrow in 125:Les Mureaux 111 108: 79: 50:National origin 49: 44: 17: 12: 11: 5: 1130: 1128: 1120: 1119: 1114: 1112:Potez aircraft 1109: 1099: 1098: 1092: 1091: 1089: 1088: 1083: 1078: 1072: 1070: 1066: 1065: 1063: 1062: 1057: 1052: 1047: 1042: 1037: 1032: 1027: 1022: 1017: 1012: 1007: 1002: 997: 992: 987: 982: 977: 972: 967: 962: 957: 952: 947: 942: 937: 932: 927: 922: 917: 912: 907: 902: 897: 892: 887: 882: 877: 872: 867: 862: 857: 852: 847: 842: 837: 832: 827: 822: 817: 812: 807: 802: 797: 791: 789: 785: 784: 778: 776: 775: 768: 761: 753: 746: 745: 730: 712: 686: 668: 650: 632: 614: 596: 591:L'Aéronautique 578: 550: 528: 523:L'Aéronautique 509: 507: 504: 503: 502: 495: 494:External links 492: 489: 488: 478: 477: 475: 472: 471: 470: 455: 452: 451: 450: 444: 438: 432: 426: 423:Maximum speed: 412: 411: 405: 391: 388:Fuel capacity: 385: 379: 373: 364: 358: 352: 346: 340: 311: 310:Specifications 308: 260: 257: 176:trailing edges 133:Weymann WEL-80 107: 104: 86: 85: 82: 76: 75: 72: 68: 67: 62: 58: 57: 52: 46: 45: 42: 37: 33: 32: 24: 23: 15: 13: 10: 9: 6: 4: 3: 2: 1129: 1118: 1115: 1113: 1110: 1108: 1105: 1104: 1102: 1087: 1084: 1082: 1079: 1077: 1074: 1073: 1071: 1067: 1061: 1058: 1056: 1053: 1051: 1048: 1046: 1043: 1041: 1038: 1036: 1033: 1031: 1028: 1026: 1023: 1021: 1018: 1016: 1013: 1011: 1008: 1006: 1003: 1001: 998: 996: 993: 991: 988: 986: 983: 981: 978: 976: 973: 971: 968: 966: 963: 961: 958: 956: 953: 951: 948: 946: 943: 941: 938: 936: 933: 931: 928: 926: 923: 921: 918: 916: 913: 911: 908: 906: 903: 901: 898: 896: 893: 891: 888: 886: 883: 881: 878: 876: 873: 871: 868: 866: 863: 861: 858: 856: 853: 851: 848: 846: 843: 841: 838: 836: 833: 831: 828: 826: 823: 821: 818: 816: 813: 811: 808: 806: 803: 801: 798: 796: 793: 792: 790: 786: 781: 774: 769: 767: 762: 760: 755: 754: 751: 741: 734: 731: 726: 722: 716: 713: 700: 696: 690: 687: 682: 678: 672: 669: 664: 660: 654: 651: 646: 642: 636: 633: 628: 624: 618: 615: 610: 606: 600: 597: 592: 588: 582: 579: 574: 570: 563: 561: 559: 557: 555: 551: 546: 542: 538: 532: 529: 524: 520: 514: 511: 505: 501: 498: 497: 493: 483: 480: 473: 464: 463: 458: 457: 453: 448: 445: 442: 441:Take-off run: 439: 436: 433: 430: 427: 424: 421: 420: 419: 417: 409: 406: 403: 400:water-cooled 399: 395: 392: 389: 386: 383: 382:Gross weight: 380: 377: 376:Empty weight: 374: 371: 369: 365: 362: 359: 356: 353: 350: 347: 344: 341: 338: 335: 334: 333: 331: 326: 324: 316: 309: 307: 305: 301: 297: 293: 288: 286: 282: 277: 274: 270: 267:The S.T.I.Aé 265: 258: 256: 254: 248: 246: 242: 238: 234: 231: 227: 223: 218: 215: 211: 207: 203: 202:undercarriage 199: 196: 191: 189: 186: 182: 177: 173: 172:leading edges 169: 165: 161: 160:cabane struts 157: 153: 148: 146: 143:water-cooled 142: 138: 134: 130: 126: 122: 121:Latécoère 490 118: 114: 105: 103: 101: 97: 93: 83: 78: 77: 73: 71:First flight 70: 69: 66: 63: 61:Manufacturer 60: 59: 56: 53: 48: 47: 41: 38: 35: 34: 30: 25: 20: 914: 739: 733: 724: 715: 703:. Retrieved 698: 689: 680: 671: 662: 653: 644: 635: 626: 617: 608: 599: 590: 581: 572: 544: 540: 531: 522: 513: 482: 461: 447:Landing run: 446: 440: 434: 428: 422: 415: 413: 407: 393: 387: 381: 375: 366: 360: 354: 348: 342: 336: 329: 327: 322: 321: 303: 299: 295: 291: 289: 280: 278: 273:Villacoublay 268: 266: 262: 249: 230:aspect ratio 219: 192: 149: 131:, Potez 37, 109: 91: 89: 80:Number built 742:: 2012/136. 541:L'Aérophile 416:Performance 408:Propellers: 394:Powerplant: 259:Development 214:machine gun 145:V-12 engine 137:Wibault 260 1101:Categories 1069:Potez-CAMS 575:(494): 11. 506:References 361:Wing area: 117:Breguet 33 725:Les Ailes 681:Les Ailes 663:Les Ailes 645:Les Ailes 627:Les Ailes 609:Les Ailes 573:Les Ailes 349:Wingspan: 323:Data from 304:Potez 371 241:elevators 233:tailplane 228:. A high 113:Amiot 130 74:mid-1930 22:Potez 37 782:aircraft 410:2-bladed 372:Clark YH 210:cockpits 198:radiator 168:fairings 166:section 156:fuselage 135:and the 92:Potez 37 705:18 June 368:Airfoil 355:Height: 343:Length: 195:Lamblin 164:airfoil 152:parasol 300:F-AKFT 296:F-AKFS 292:F-AKxx 226:rudder 206:tandem 106:Design 100:French 55:France 835:XVIII 788:Potez 474:Notes 466:(PDF) 337:Crew: 245:chord 208:open 185:dural 183:with 181:spars 36:Role 845:XXII 830:XVII 800:VIII 707:2016 402:V-12 396:1 × 285:Orly 188:ribs 90:The 1086:161 1081:160 1076:141 1040:230 1035:220 1025:662 1020:661 970:506 965:501 840:XIX 820:XII 795:VII 339:Two 222:fin 115:, 1103:: 1060:94 1055:91 1050:84 1045:75 1030:67 1015:65 1010:63 1005:62 1000:60 995:58 990:56 985:54 980:53 975:51 960:50 955:49 950:45 945:43 940:42 935:41 930:40 925:39 920:38 915:37 910:36 905:35 900:34 895:33 890:32 885:31 880:29 875:28 870:27 865:26 860:25 855:24 850:23 825:XV 815:XI 805:IX 723:. 697:. 679:. 661:. 643:. 625:. 607:. 589:. 571:. 553:^ 545:39 543:. 539:. 521:. 306:. 147:. 127:, 123:, 119:, 84:2 810:X 772:e 765:t 758:v 709:. 370::

Index


Reconnaissance aircraft
France
Aéroplanes Henry Potez
reconnaissance aircraft
French
Amiot 130
Breguet 33
Latécoère 490
Les Mureaux 111
Nieuport-Delage Ni-D 580
Weymann WEL-80
Wibault 260
Hispano-Suiza 12Nb
V-12 engine
parasol
fuselage
cabane struts
airfoil
fairings
leading edges
trailing edges
spars
dural
ribs
Lamblin
radiator
undercarriage
tandem
cockpits

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