Polikarpov UTI-4 typ 15

Polikarpov UTI-4 Type 15 / Поликарпов УТИ-4 тип 15
     
Název:
Name:
Polikarpov UTI-4 typ 15 Polikarpov UTI-4 Type 15
Originální název:
Original Name:
Поликарпов УТИ-4 тип 15
Kategorie:
Category:
cvičný letoun trainer aeroplane
Výrobce:
Producer:
DD.MM.1937-DD.MM.1941 Gorkovský letecký závod č. 21 Ordžonikidzeho, Gorkij /
DD.MM.1940-DD.MM.1941 Novosibirský letecký závod č. 153 V. P. Čkalova, Novosibirsk /
DD.03.1941-DD.MM.1941 Rostovský letecký závod č. 458, Rostov na Donu /
DD.MM.1941-DD.01.1942 Bakuský letecký závod č. 458, Baku /
Období výroby:
Production Period:
DD.MM.1937-DD.01.1942
Vyrobeno kusů:
Number of Produced:
1660 nově postavených letounů
cca 150 další přestavěných stíhačak po opravách
První vzlet:
Maiden Flight:
DD.10.1935
Osádka:
Crew:
2
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept:
klasické conventional
Podvozek:
Undercarriage:
pevný fixed
Přistávací zařízení:
Landing Gear:
kola/lyže wheels/ski
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
1156 kg 2549 lb
Vzletová hmotnost:
Take-off Weight:
1458 kg 3214 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
9,004 m 29ft 6,5in
Délka:
Length:
5,985 m 19ft 7,66in
Výška:
Height:
3,520 m 11ft 6,5in
Plocha křídla:
Wing Area:
14,45 m2 155.54 ft2
Plošné zatížení:
Wing Loading:
100,9 kg/m2 20.67 lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
1
Typ:
Type:
Švecov M-25V vzduchem chlazený hvězdicový devítiválec o vzletovém výkonu 570 kW (775 k) a nominální výkon 551,62 kW (750 k) v h= 2 900 m.
Vrtule AV-1 dvoulistá kovová s nastavitelným úhlem náběhu o průměru 2 800 mm.
Shvetcov M-25V nine-cylinder air-cooled radial engine, rated at 765 hp for take-off and nominal power 740 hp at 9,514 ft,
driving a two-blade metal variable-pitch propeller Type AV-1 of 9ft 2 1/4in diameter.
Objem palivových nádrží:
Fuel Tank Capacity:
145 l 32 UK gallons (38.3 US gallons)
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
450 km/h v 2800 m 279.6 mph in 9186 ft
Cestovní rychlost:
Cruise Speed:
? km/h v ? m ? mph in ? ft
Rychlost stoupání:
Climb Rate:
14,8 m/s 2913.4 ft/min
Čas výstupu na výšku:
Time to Climb to:
6,39 min do 5000 m 6,39 min to 16404 ft
Operační dostup:
Service Ceiling:
8960 m 29396 ft
Dolet:
Range:
365 km 226.8 mi
Maximální dolet:
Maximum Range:
? km ? mi
Výzbroj:
Armament:
bez výzbroje without weapons
Uživatelské státy:
User States:








Poznámka:
Note:
Část letounů byla vyrobena v jednomístné bitevní verzi, tyto stroje byly nasazeny bojích u Baku. Part of the aircraft produced in 1939 had a fixed landing gear.
The existence of a assault variants is not demonstrated.
Zdroje:
Sources:
Yefim Gordon and Keith Dexter. Polikarpov's I-16 Fighter, Its Forerunners and Progeny, Red Star, Vol.3., Earl Shilton, Leicester, UK, Midland Publishing Ltd., 2002. ISBN 1-85780-131-8
Hans-Heiri Stapfer, Polikarpov Fighters in Action, Part 2, Aircraft in Action number 158., Carrollton, TX, Squadron/Signal Publications, Inc., 1996. ISBN 0-89747-355-8.
Michail Maslov, Istrebitěl I-16, Выпуск №2: М. Aрмада, 1997
http://i16fighter.ru/mods/uti4/uti4.htm
http://crimso.msk.ru/Site/Crafts/Craft20034.htm
http://www.airwar.ru/enc/other2/uti2.html
archiv autora

Polikarpov UTI-4 typ 15 -


Polikarpov UTI-4 typ 15 -


Polikarpov UTI-4 typ 15 -


Polikarpov UTI-4 typ 15 -


URL : https://www.valka.cz/Polikarpov-UTI-4-typ-15-t81598#461821 Version : 0

Polikarpov UTI-4 type 15


The transition of pilots to the then-modern Polikarpov I-16 fighter was quite challenging if the pilot was transitioning from the I-15 series of biplanes, he had to get used to the high surface load and also to the completely different behaviour of the single-plane "sixteeners", even worse for young pilots who had been flying training Polikarpov Po-2. Therefore, a total of 115 two-seat trainers UTI-2 were built, based on the combat I-16 Type 4, i.e., it was powered by a nine-cylinder Svecov M-22 with 480 hp, but this engine ceased to be produced over time and so it was necessary to proceed to the production of a more modern trainer. The other reasons were that in 1935 the performance of the next versions of the "sixteen" increased and this was mainly due to the Švecov M-25 engine and in addition the new versions were equipped with flaps, thus creating a new aircraft for continued training as the UTI-3, which was powered by the M-58 engine. The prototype was tested, but engines were in short supply, and so the UTI-3 remained a single example. In the same year, another aircraft designated UTI-4 was built.


This aircraft was based on the I-16 Type 5, the prototype flew in the autumn of 1935, flying unarmed, with smaller fuel tanks, no radio equipment and no breathers, the landing gear was retractable. The aircraft was powered by a M-25A engine of 715 hp. After some time, the aircraft continued to be lightened and the UTI-4 was to be delivered with a fixed undercarriage, if you say that this is detrimental to the quality of training, it is not true in Russian terms, only the instructor could operate the undercarriage from his seat! From 1 January 1939 aircraft were delivered with fixed undercarriage, i.e. only some had fixed undercarriage, some had retractable undercarriage but fixed in the open position and the undercarriage shafts were covered with the original covers, now bolted on - the order was obeyed. The rigid chassis made it easy to swap wheels for skis.


Towards the end of production, the UTI-4s finally saw newly manufactured covers and parts that eliminated the undercarriage shafts. These last production blocks were delivered with 750 hp M-25V engines and dyno starters. Production at Moscow, Gorky and Novosibirsk was completed in 1940, the Rostov plant was evacuated to Baku and production continued there until 1942. Several dozen combat aircraft, designated UTI-4B, were also produced at this factory.
These planes were single-seaters with a flush rear cockpit, two Berezin UBK machine guns of 12.7 mm calibre in the wings, and could be fitted with six RS-82 unguided rockets or two 50-pound FAB-50 bombs. These fighters formed the armament of the 266th Air Regiment.
The training aircraft were gradually used up and so were replaced by more modern aircraft such as the Yak-7UTI. A few aircraft, however, lasted in service until the end of the war, but these were used in the role of courier aircraft. A total of 1,660 trainer aircraft were produced and approximately 130 aircraft were converted from single-seat fighters.



Sources used:
Yefim Gordon and Keith Dexter. Polikarpov's I-16 Fighter, Its Forerunners and Progeny, Red Star, Vol.3., Earl Shilton, Leicester, UK, Midland Publishing Ltd., 2002. ISBN 1-85780-131-8
Hans-Heiri Stapfer, Polikarpov Fighters in Action, Part 2, Aircraft in Action number 158., Carrollton, TX, Squadron/Signal Publications, Inc., 1996. ISBN 0-89747-355-8.
Mikhail Maslov, Istrebitel I-16, Issue No. 2: M. Armada, 1997
http://i16fighter.ru/mods/uti4/uti4.htm
http://www.airwar.ru/enc/other2/uti2.html
http://i16fighter.ru/mods/uti4/uti4.htm
author's archive
URL : https://www.valka.cz/Polikarpov-UTI-4-typ-15-t81598#555593 Version : 0

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I-16 UTI


Zdroj :http://englishrussia.com/?p=2239#more-2239
Polikarpov UTI-4 typ 15 - I-16 UTI-4

I-16 UTI-4
URL : https://www.valka.cz/Polikarpov-UTI-4-typ-15-t81598#299149 Version : 0
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