26:
213:
220:
The helicopter was completed by the end of 1949. During the first flight trial on 14 January 1950, it was overturned by a wind gust and had to be repaired. The test pilot was Bronisław Żurakowski, who taught himself to fly a helicopter. The helicopter first flew on 4 April 1950, restrained on tethers
243:
In 1956, the helicopter was repaired and used for training flights. On 28 June 1957 a tail rotor gear (originally from a motorcycle) broke and it could not be replaced, consequently, the helicopter never flew again, being written off on 28 October 1960. During 1956–1957 it had completed 185 flights,
224:
During 1950–1953, it underwent a test program and was often modified. At first it had elastic rotor blades. In 1950, it was fitted with rigid blades and an efficient simple custom-designed resonant vibration eliminator, similar to later
122:, constructed in 1950. Developed by the Main Aviation Institute (Warsaw), the only constructed GIL saw service until 1960 when it was irreparably damaged and subsequently decommissioned. The prototype aircraft currently resides at the
240:). On 16 November 1953, the helicopter was damaged when the main rotor was bent by the wind and cut off the tail boom, thus ending the test program. By then, the prototype had completed 169 flights, in 20 hours 21 minutes in total.
196:
Initially, the helicopter had no name. It only received the registration letters SP-GIL, from the institute abbreviation, and hence it soon became known as GIL or Gil (
147:
178:
229:
designs. During tests, it crashed or was damaged without casualties at least seven times, for different reasons, and was repaired each time.
380:
564:
468:
584:
574:
142:, from an initiative of Zbigniew Brzoska. It was a difficult task, because Polish aviation industry was entirely destroyed during
579:
569:
236:
airfield (it was the first public presentation of a helicopter in Poland and one of first presentations in the
157:
Despite severe material shortages, work on experimental design started in 1948, and the main designer became
169:
rotor type, with two auxiliary blades. A fuselage structure, tail boom, auxiliary rotor and tricycle
158:
248:
123:
52:
31:
549:
464:
314:
4-cylinder air-cooled in-line piston engine, 78 kW (105 hp) vertically mounted
174:
162:
8:
390:
385:
232:
On 20 July 1952, the BŻ-1 GIL was first displayed to the public, during an air show at
201:
204:
in Polish). Later it was also given the designation BŻ-1, from Żurakowski's initials.
226:
102:
166:
181:. The design utilized some components left by the Germans, like a piston engine
558:
368:
311:
237:
182:
170:
151:
143:
190:
119:
186:
252:
233:
25:
150:
was the only person in a team, who had ever seen a helicopter (
139:
115:
221:
by two men (Fiszdon and Chyliński) for a measure of safety.
165:), who designed a rotor and control system. It used simpler
530:Żurakowski, Bronisław. "SP-GIL - wspomnienia konstruktora"
212:
134:
The helicopter was designed at the research institute
519:
Witkowski, Ryszard. "Powrót GILa i jego dalsze losy"
375:
Aircraft of comparable role, configuration, and era
185:(re-configured for vertical use), rear gear from a
465:"Polish Aviation Museum Cracow:Helicopter: SP-GIL"
247:Currently, the sole BŻ-1 GIL is preserved in the
556:
177:. A power unit and final drive were designed by
266:Lotnictwo : Powrót GILa i jego dalsze losy
509:. London: Fredrick Warne & Co. Ltd., 1958.
507:The Observer's Book of Aircraft, 1958 edition
129:
211:
427:
425:
423:
421:
419:
417:
415:
413:
341:140 km/h (87 mph, 76 kn)
146:. In addition, the institute principal
557:
514:Helicopters and Autogyros of the World
494:Glass, Andrzej. "Śmigłowiec BŻ-1 GIL"
450:
448:
446:
207:
505:Green, William and Gerald Pollinger.
410:
193:glider's jettisonable landing gear.
443:
13:
565:1950s Polish experimental aircraft
457:
320:8.8 m (28 ft 10 in)
286:8.5 m (27 ft 11 in)
14:
596:
585:Single-engined piston helicopters
543:
326:60.8 m (654 sq ft)
258:
24:
575:Aircraft manufactured in Poland
471:from the original on 2011-07-24
292:3 m (9 ft 10 in)
502:, 2(47)/2005. ISSN 1732-5323.
434:
353:4.5 m/s (890 ft/min)
1:
538:, 2(47)/2005. ISSN 1732-5323.
527:, 2(47)/2005. ISSN 1732-5323.
398:
189:motorcycle and wheels from a
138:- Main Aviation Institute in
580:Aircraft first flown in 1950
347:2,000 m (6,600 ft)
7:
357:
304:610 kg (1,345 lb)
298:510 kg (1,124 lb)
244:for a total of 12.5 hours.
10:
601:
454:Witkowski 2005, pp. 49–51.
440:Żurakowski 2005, pp.45–49.
136:Główny Instytut Lotnictwa
98:
90:
85:
77:
69:
61:
57:Główny Instytut Lotnictwa
51:
43:
38:
23:
18:
570:1950s Polish helicopters
516:. London: Cassell, 1958.
271:General characteristics
161:(brother of test pilot
431:Glass 2005, pp. 44–45.
249:Polish Aviation Museum
217:
130:Design and development
124:Polish Aviation Museum
32:Polish Aviation Museum
215:
318:Main rotor diameter:
159:Bronisław Żurakowski
391:Vought-Sikorsky 300
386:Gazda Helicospeeder
363:Related development
208:Operational history
39:General information
512:Lambermont, Paul.
218:
175:Tadeusz Chyliński
173:were designed by
163:Janusz Żurakowski
148:Władysław Fiszdon
108:
107:
592:
533:
522:
497:
481:
479:
477:
476:
461:
455:
452:
441:
438:
432:
429:
345:Service ceiling:
334:
324:Main rotor area:
273:
179:Zbigniew Brzoska
30:BŻ-1 Gil at the
28:
16:
15:
600:
599:
595:
594:
593:
591:
590:
589:
555:
554:
546:
541:
531:
520:
495:
485:
484:
474:
472:
463:
462:
458:
453:
444:
439:
435:
430:
411:
401:
360:
330:
269:
261:
210:
132:
34:
12:
11:
5:
598:
588:
587:
582:
577:
572:
567:
553:
552:
545:
544:External links
542:
540:
539:
528:
517:
510:
503:
491:
490:
489:
483:
482:
456:
442:
433:
408:
407:
406:
405:
400:
397:
394:
393:
388:
383:
372:
371:
359:
356:
355:
354:
351:Rate of climb:
348:
342:
339:Maximum speed:
328:
327:
321:
315:
305:
299:
293:
287:
281:
260:
259:Specifications
257:
209:
206:
131:
128:
114:was the first
106:
105:
100:
96:
95:
92:
88:
87:
83:
82:
79:
75:
74:
71:
67:
66:
63:
59:
58:
55:
49:
48:
45:
41:
40:
36:
35:
29:
21:
20:
9:
6:
4:
3:
2:
597:
586:
583:
581:
578:
576:
573:
571:
568:
566:
563:
562:
560:
551:
548:
547:
537:
529:
526:
518:
515:
511:
508:
504:
501:
493:
492:
487:
486:
470:
466:
460:
451:
449:
447:
437:
428:
426:
424:
422:
420:
418:
416:
414:
409:
403:
402:
396:
392:
389:
387:
384:
382:
379:
378:
377:
376:
370:
367:
366:
365:
364:
352:
349:
346:
343:
340:
337:
336:
335:
333:
325:
322:
319:
316:
313:
309:
306:
303:
302:Gross weight:
300:
297:
296:Empty weight:
294:
291:
288:
285:
282:
279:
276:
275:
274:
272:
267:
265:
256:
254:
250:
245:
241:
239:
235:
230:
228:
222:
214:
205:
203:
199:
194:
192:
188:
184:
180:
176:
172:
171:undercarriage
168:
164:
160:
155:
154:in England).
153:
149:
145:
141:
137:
127:
125:
121:
118:experimental
117:
113:
104:
101:
97:
93:
89:
84:
80:
76:
72:
68:
64:
60:
56:
54:
50:
46:
42:
37:
33:
27:
22:
17:
535:
524:
513:
506:
499:
488:Bibliography
473:. Retrieved
459:
436:
395:
374:
373:
362:
361:
350:
344:
338:
331:
329:
323:
317:
312:Hirth HM 504
307:
301:
295:
289:
283:
277:
270:
268:
263:
262:
246:
242:
238:Eastern Bloc
231:
223:
219:
197:
195:
183:Hirth HM 504
156:
152:Sikorsky R-4
144:World War II
135:
133:
111:
109:
94:4 April 1950
91:First flight
78:Number built
70:Primary user
65:Experimental
53:Manufacturer
532:(in Polish)
521:(in Polish)
496:(in Polish)
332:Performance
308:Powerplant:
191:DFS Kranich
559:Categories
475:2010-06-25
399:References
381:Aero XE-II
120:helicopter
47:Helicopter
19:BŻ-1 "GIL"
536:Lotnictwo
525:Lotnictwo
500:Lotnictwo
264:Data from
202:bullfinch
550:BŻ-1 Gil
480:backup:
469:Archived
369:BŻ-4 Żuk
358:See also
227:Sikorsky
216:BŻ-1 GIL
200:means a
112:BŻ-1 GIL
290:Height:
284:Length:
187:Zündapp
99:Retired
86:History
253:Kraków
234:Okęcie
167:Hiller
140:Warsaw
116:Polish
73:Poland
62:Status
404:Notes
278:Crew:
310:1 ×
110:The
103:1960
44:Type
534:.
498:.
251:in
198:gil
561::
523:.
467:.
445:^
412:^
255:.
126:.
478:.
280:1
81:1
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.