295:
26:
287:
279:
148:
was therefore a considerable departure from the past. It was designed to compete in the STAé (Service
Technique de l'Aéronautique or Technical Section of Aeronautics) 1930/31 C1 (single seat Chasseur of fighter) programme.
234:
and a revised nacelle, shortened forward of the cockpit by 360 mm (14.2 in). A 33 mm (1.30 in) APX cannon was now housed in a fairing below the nacelle as an alternative to the earlier pair of
225:
The H.110 began flight testing in April 1933. Tested against its smaller and lighter competitors, it proved slower and less manoeuvrable and was returned to
Hanriot for modification. It flew in April 1934 as the
243:. With its new engine and propeller the H.115 was quicker than the earlier version, with a top speed of 390 km/h (242 mph). After more modifications over the winter of 1934-5 it returned to
222:
and a rearward leaning strut together forming a V, laterally braced with an inverted V-strut attached near the under-fuselage centre line. There was a central tailwheel on a long leg under the fin.
562:
108:
built in France in the early 1930s. It proved to be slower and less manoeuvrable than its contemporaries and failed to reach production, even as the
934:
944:
198:. Forward, the slim, square section and untapered tail booms blended into the wings at about mid-chord, the aft ends carrying a constant-chord
244:
528:
476:
555:
210:. A central, single, tall, round-tipped, wire-braced vertical tail was mounted on in it. The H.110 had a fixed, split,
939:
294:
211:
949:
548:
176:
25:
878:
853:
833:
230:, with its HS 12Xbrs engine uprated to 515 kW (691 hp), a new four-blade propeller with variable-
179:
in the short nose ahead of the open cockpit, with a variable position central cone to control the airflow.
858:
848:
586:
596:
591:
499:
129:
504:
168:
139:
97:
863:
843:
621:
203:
616:
606:
247:
in June 1935 and was officially flight tested until mid August, but failed to attract a contract.
190:. Immediately outboard they had a wider chord and beyond were double straight tapered to rounded
802:
524:
472:
362:
157:
215:
187:
172:
125:
105:
42:
183:
219:
156:
and engine in a short central nacelle. It was powered by a 485 kW (650 hp)
928:
908:
898:
893:
888:
883:
838:
828:
823:
818:
787:
757:
742:
722:
717:
712:
707:
702:
697:
692:
687:
611:
913:
903:
797:
792:
782:
777:
772:
767:
762:
752:
747:
737:
732:
727:
682:
677:
672:
667:
662:
657:
652:
647:
642:
637:
365:
160:
601:
431:
369:
266:
240:
231:
164:
142:
286:
278:
199:
145:
136:
101:
428:
236:
207:
195:
191:
571:
153:
132:
66:
113:
540:
293:
285:
277:
186:. The central 25% of their span, between the booms, had constant
544:
508:. Vol. XXVI, no. 8. 22 February 1934. p. 179.
812:
Lorraine-Hanriot 1930-33, Hanriot 1933-37 and SNCAC 1937-40
298:
Hanriot 110 3 view from l'Aerophile magazine
January 1933
265:
Uprated engine, shorter nose, four blade propeller and a
202:
slightly above them. This had rounded tips and a central
471:. Godalming, UK: Salamander Books. pp. 279–80.
372:, 480 kW (650 hp) at 4,000 m (13,120 ft)
171:. The pilot's headrest was smoothly faired into the
811:
630:
579:
523:. Warrendale, USA: SAE International. p. 178.
194:. They carried almost full-span, narrow-chord
167:behind the pilot, driving a three-blade pusher
556:
8:
467:Green, William; Swanborough, Gordon (1994).
112:after receiving a more powerful engine and
563:
549:
541:
382:Rated power (50 hr continuous, under load)
462:
460:
458:
456:
454:
452:
399:355 km/h (221 mph, 192 kn)
494:
492:
490:
488:
448:
405:600 km (370 mi, 320 nmi)
124:From 1916 until 1933, the only Hanriot
580:Pre-1916, including some Ponnier types
15:
218:mainwheel on a faired, near vertical
7:
343:24.00 m (258.3 sq ft)
331:13.50 m (44 ft 3 in)
500:"New Aircraft - The Hanriot H.110"
337:2.70 m (8 ft 10 in)
325:7.96 m (26 ft 1 in)
14:
282:H.115, showing the ventral cannon
305:Green & Swanborough p.279-80
290:H.115, showing the nose radiator
182:The wings were built around two
175:. There was a circular Chausson
152:The all-metal H.110 had an open
24:
411:7.78 min to 5,000 m (16,405 ft)
935:Single-engined pusher aircraft
1:
945:1930s French fighter aircraft
469:The Complete Book of Fighters
378:3-bladed pusher configuration
355:1,750 kg (3,858 lb)
349:1,260 kg (2,778 lb)
521:Hispano Suiza in Aeronautics
239:7.5 mm (0.295 in)
966:
212:conventional undercarriage
32:
23:
18:
631:Hanriot (Dupont) 1916-30
135:. The Hanriot H.110, a
310:General characteristics
299:
291:
283:
274:Specifications (H.110)
120:Design and development
519:Lage, Manual (2004).
297:
289:
281:
163:upright water-cooled
427:2×7.5 mm (0.293 in)
368:upright watercooled
363:Hispano-Suiza 12Xbrs
158:Hispano-Suiza 12Xbrs
98:pusher configuration
940:Twin-boom aircraft
300:
292:
284:
922:
921:
409:Time to altitude:
259:Original version.
90:
89:
957:
950:Hanriot aircraft
565:
558:
551:
542:
535:
534:
516:
510:
509:
496:
483:
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464:
419:
392:
312:
126:fighter aircraft
106:fighter aircraft
83:
54:
46:Type of aircraft
43:fighter aircraft
28:
16:
965:
964:
960:
959:
958:
956:
955:
954:
925:
924:
923:
918:
807:
626:
587:1909 monoplanes
575:
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513:
498:
497:
486:
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466:
465:
450:
445:
439:
420:
415:
388:
384:370 kW (500 hp)
308:
276:
253:
122:
96:was an unusual
81:
53:National origin
52:
47:
12:
11:
5:
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397:Maximum speed:
386:
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344:
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326:
320:
275:
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220:shock absorber
196:Frise ailerons
173:engine cowling
121:
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104:, single seat
88:
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63:
59:
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21:
20:
19:Hanriot H.110
13:
10:
9:
6:
4:
3:
2:
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951:
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530:0-7680-0997-9
526:
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507:
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501:
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491:
489:
485:
480:
478:1-85833-777-1
474:
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391:
383:
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377:
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371:
367:
364:
360:
357:
354:
353:Gross weight:
351:
348:
347:Empty weight:
345:
342:
339:
336:
333:
330:
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324:
321:
318:
315:
314:
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306:
304:
296:
288:
280:
273:
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237:Chatellerault
233:
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217:
213:
209:
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197:
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159:
155:
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138:
134:
131:
127:
119:
117:
115:
111:
110:Hanriot H.115
107:
103:
99:
95:
94:Hanriot H.110
85:
80:
79:
75:
73:First flight
72:
71:
68:
64:
62:Manufacturer
61:
60:
56:
51:
50:
44:
40:
37:
36:
31:
27:
22:
17:
873:
868:
520:
514:
503:
468:
438:
436:
432:machine guns
424:
416:
414:
408:
402:
396:
389:
387:
381:
375:
366:supercharged
358:
352:
346:
340:
334:
328:
322:
316:
309:
307:
302:
301:
245:Villacoublay
241:machine guns
227:
224:
181:
161:supercharged
151:
123:
109:
93:
91:
82:Number built
41:Single seat
390:Performance
376:Propellers:
370:V-12 engine
359:Powerplant:
267:33mm A.P.X.
165:V-12 engine
76:April 1933
929:Categories
597:1911 types
592:1910 types
443:References
341:Wing area:
214:with each
143:cantilever
116:armament.
329:Wingspan:
303:Data from
200:tailplane
169:propeller
146:monoplane
137:twin boom
128:had been
102:twin boom
574:aircraft
429:MAC 1934
417:Armament
251:Variants
208:trim tab
204:elevator
177:radiator
133:biplanes
572:Hanriot
335:Height:
323:Length:
269:cannon.
216:spatted
206:with a
154:cockpit
130:tractor
67:Hanriot
65:Avions
57:France
884:LH.161
834:LH.21S
527:
505:Flight
475:
403:Range:
140:pusher
114:cannon
33:H.110
914:H.510
909:H.230
904:H.220
899:H.190
894:H.180
889:H.170
879:H.130
874:H.115
869:H.110
864:LH.80
859:LH.70
854:LH.60
849:LH.41
844:LH.40
839:LH.30
829:LH.16
824:LH.12
819:LH.10
788:HD.40
758:HD.32
743:HD.28
738:HD.27
723:HD.24
718:HD.22
713:HD.20
708:HD.19
703:HD.18
698:HD.17
693:HD.15
688:HD.14
683:HD.12
622:D.VII
612:D.III
425:Guns:
317:Crew:
262:H.115
256:H.110
232:pitch
228:H.115
188:chord
184:spars
38:Role
803:H.46
798:H.43
793:H.41
783:H.38
778:H.36
773:H.35
768:H.34
763:H.33
753:H.31
748:H.29
733:H.26
728:H.25
678:HD.9
673:HD.8
668:HD.7
663:HD.6
658:HD.5
653:HD.4
648:HD.3
643:HD.2
638:HD.1
617:D.IV
607:D.II
525:ISBN
473:ISBN
361:1 ×
192:tips
92:The
602:D.I
319:One
931::
502:.
487:^
451:^
100:,
86:1
564:e
557:t
550:v
533:.
481:.
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