Tupolev tb- 3

Continue TB-3 (it); TB-3重轟炸機 (zh-hant); TB-3重轰炸机 (zh-cn); Tupolev TB-3 (fi); Tupolev TB-3 (eo); Tupolev טופולב ;(From the Commons, the free repository of mediaTepolov TB-3 (es); No3 (ru); TB-3 (de); TB-3 (en-GB); Тупољев-6 (sr-ec); No3 (bg); TB-3 (yes); Tupolev TB-3 (ro); TB-3 (ja); Tupolev TB-3 (sk TB-3 (cs); Tupolev ANT-6 (he); Tupolev TB-3 (ph); Tupolev TB-3 (vi); No 6/X-3 (m); Тупољев No.6 (senior); Tupolev TB-3 (sl); TB-3 (en-ka); 圖波列夫 TB-3重型轟炸機 (g); Tupolev TB-3 (Az); Tupolev TB-3 (id); TB-3 (pl); Tupolev TB-3 (nb); Toepolev TB-3 (nn); Tupolev TB-3 (t); Tupolev ANT-6 (wed-el); fa); Tupolev TB-3 (Fri); TB-3 (An); TB-3 (s); TB-3重轰炸机 (zh-hans); B-3 (UK) bomber strategic Tupolev (he); avion militaire (fr); Militurflugzeug (de); 1930 Tupolev bomber family (en); The 1930 bomber family of the stupid (en-GB); 1930 Tupolev bomber family (en-ka); Soviet scorer flyer) ﺗﻮﭘﻮﻟﻒ ﺗﯽ ﺑﯽ۳- (cs); Bombardment pesado sovyetico (es) Ant 6, Tupolev TB 3 4M, Tupolev TB-3 4M, Tupolev TB 3, ANT-6, Tupolev TB-3 (es); Tupolev ANT-6 (f); TB-3 (s); ANT-6, Tupolev ANT-6, TB - 3 (pl); No 6, HT-6, 6-4M-34, 3-4M-17 (en); Tupolev TB-3, TB-3 (he); Tupolev ANT-6, Tupolev TB-3, Tupolev G-2, Tupolev TB-3 (de); ANT-6, TB-3 (fi); Tupolev TB-3, heavy bomber 3, Tupolev ANT-3, ANT-3, TB3, ANT3 (en); Tupolev ANT-6, TB-3, ANT-6 (cs); TB-3重轰炸机 (g); Тупољев ТБ-3, З-3 (старший) Английский: Туполев ТБ-3 ТБ-3 (АНТ-6) ТБ-3 Вено Роль Тяжелый бомбардировщик Производитель Воронежской авиационной производственной ассоциации Конструктор Андрей Туполев Первый полет 22 декабря 1930 Введение 1932 Пенсионеры 1939 ВВС СССР (официально)1945 Ввс СССР (де-факто) Первичные пользователи Советских ВВСАэрофлот Произвел 1932-1934, 1935- 1937 годы Номер построен 818 Разработано из Туполева ТБ-1 Разработано в Туполев АНТ-16 Туполев ТБ-3 (русский: Тьяжоли Бомбардировчик, Тяжелый бомбардировщик гражданского назначения АНТ-6 — тяжелый бомбардировщик, который был развернут советскими ВВС в 1930-х годах и во время Второй мировой войны. Это был первый в мире четырехмоторный тяжелый бомбардировщик cantilever. Несмотря на устаревание и официальное выведение из эксплуатации в 1939 году, ТБ-3 выполнял бомбардировщики и транспортные обязанности на протяжении большей части Второй мировой войны. ТБ-3 также видел боевые действия в качестве истребителя проекта «Цвено» и легкого танкового транспорта. Разработка В 1925 году советские ВВС подошли к TsAGI с требованием для тяжелого бомбардировщика с общей мощностью двигателя 2000 л.с. (1,970 л.с.) и либо колесные или поплавок шасси. Туполев The Design Bureau began design work in 1926, and in 1929 the state operational requirements were completed. Tupolev TB-1 was taken as the basis for the design and The aircraft was originally equipped with 600 hp (590 hp) Curtiss V-1570 Conqueror engines each, with the aim of switching to the Mikulin M-17 (modified BMW VIs) in production. The layout was approved on March 21, 1930, and the first prototype was completed on October 31, 1930. The plane was flying on December 22, 1930 with Mikhail Gromov behind control and with a ski landing gear. Despite almost crashing due to the vibration causing the throttle to close, the test flight was successful. On February 20, 1931, the Soviet Air Force approved the production of the ANT-6 with M-17 engines. The prototype was refitted with BMW VIz 500 730 hp (720 hp) engines each, large radiators and wooden propellers of the TsAGI design. The unicycle chassis was deemed too weak and was replaced by a tandem with a 1350 mm × 300 mm (53 in × 12 inches). The first pre-production TB-3 4M-17 took off on January 4, 1932 with A.B. Yamashev and I.F. Petrov for control. Unexpectedly, it was found that subsequent serial aircraft are 10-12% heavier than the prototype, which makes performance much more difficult. This discrepancy was found to be due to a high positive tolerance to raw materials, resulting in steel sheeting, pipes and wires becoming much thicker than the carefully constructed prototypes. The planes were also more crudely painted with a thick layer of camouflage and varnish. The plants turned to the workers for proposals to reduce weight, paying 100 rubles for each kilogram (2.2 pounds) removed from the plane. Combined with OKB's efforts, this resulted in weight savings of almost 1,000 kilograms (2,200 pounds). Despite this, production aircraft can differ from each other by several hundred kilograms. In 1933, one TB-3 4M-17F was streamlined with the removal of towers and bomb shackles, the coating of all the holes and the installation of wheeled swords. This resulted in only a 4.5% increase in the top speed and a similar increase in the range. Tupolev concluded that optimization was minimally beneficial for large and slow aircraft. To study the effect of corrugated skin, in January-February 1935, one TB-3 4AM-34R had corrugated, gradually covered with tissue. This led to a 5.5% increase in the top speed and an increase in the ceiling by 27.5%. The same aircraft showed a significant increase in the speed of lifting when equipped with experimental four-bladed propellers. Record-breaking TB-3 4M-34R flights set an endurance record of 18 hours and 30 minutes. TB-3 4AM-34FRN with A.B. Yamashev at control controls set a number of payload records for height: September 11, 1936 - 5,000 kilograms (11,000 pounds) to 8,116 meters (26,627 feet), improved to 8,980 meters (29,460 feet) on October 28. September 16, 1936 - 10,000 kilograms (22,000 pounds) to 6,605 meters (21,670 feet) 20 1936 - 12,000 kilograms (26,000 pounds) to 2,700 meters (8,900 feet) Design TB-3 after an emergency landing during the Winter War in March 1940 TB-3 was an all-metal aircraft of steel construction, as one of the projects of the design bureau of , which will be based on the 1918 all-metal aircraft development practices and technology for the first time Hugo Junkers. The frame consisted of V-section beams covered with uncoated corrugated skin from 0.3 mm (1⁄64 inches) to 0.8 mm (1⁄32 inches). The corrugated were 13 mm (0.51 inches) deep and 50 mm (1.97 inches) apart. The wing of the cantilever was supported by four spars from the tubular section. In 1934, thanks to the development of stronger steel alloys, the wingspan was increased from 39.5 to 41.85 meters (129.6 to 137.3 feet) with a simultaneous increase in wing area from 230 to 234.5 m2 (2476 to 2524 sq m). Any part of the aircraft can walk in soft shoes without damaging the skin, and the leading edges of the wings swung down to form tracks to service the engine. The controls were activated using the tail aircraft variable frequency and the trim compensation system in the event of engine failure on one side. The fixed main chassis was not equipped with brakes. Fuel tanks had no fire protection or protection from leakage, although the engines had an internal fire suppression system. The M-17 engines were set for a maximum theoretical range of 3,250 kilometers (1,750 nm; 2,020 miles) without a ignition candle or carb. Defensive weapons consisted of light machine guns in five towers - one in the nose, two on top of the middle fuselage, and one retractable trash can under each wing between the nacelles of the engine. Later variants moved one of the upper towers of the fuselage into a beam of tail fin. Although it was officially decommissioned in 1939, at the beginning of World War II on June 22, 1941, the Soviet Air Force had 516 active TB-3s, and another 25 were operated by the Soviet navy. Located far from the western border of the USSR, the BB-3 escaped catastrophic losses during the first German airstrikes, after which THE TB-3 of the 3rd TBAP (Heavy Bombing Regiment) began flying night bombardment on June 23. The shortage of combat-capable aircraft also required daylight using UNaccompanied TB-3 fighters, and in this role the bombers, operating at low and medium altitudes, suffered heavy losses for enemy fighters and ground fire. By August 1941, TB-3 made up 25% of Soviet bombers and, operated by elite Air Force crews, performed up to three sorties per night. The aircraft was involved in all major until 1943, including the first Battle of Smolensk, the Battle of , the Battle of Stalingrad, the siege of Leningrad and the Battle of Kursk. On July 1, 1945, the 18th Air Force still had ten TB-3s in active force. THE TB-3 was widely used as a cargo and tunnel transport, carrying up to 35 soldiers in the latter role. During the first five months of the war, the aircraft transported 2,797 tons of cargo and 2,300 personnel. THE TB-3 was also used in several special projects as the parent fighter ship in the Tsveno project and for the delivery of light tanks T-27, T-37 and T-38. On August 1, 1941, a pair of TB-3s in the Configuration of The Ring-SPB, each of which had two Polycarp I-16 fighter jets with a pair of bombs weighing 250 kilograms (550 pounds), destroyed an oil depot without loss in the port of Constanța, Romania. On August 11 and 13, 1941, The Ring-SPB successfully damaged the King Carol I bridge across the Danube in Romania. Operations in Tsveno ended in the autumn of 1942 due to the high vulnerability of the mother ships. In recognition of the role of TB-3 played during the war, three aircraft were included in the first post-war air parade on 18 June 1945. Options TB-3 4AM-34FRN in the configuration of Aveno- SPB with Polycarp I-16 fighters, armed with bombs FAB-250 Paratroopers jumping from Tupolev TB-3 Source: Shavrov-3 4M-17F The first production version, made up about half of all built TB-3. TB-3 4M-34 Mikulin AM-34 engines with revised radiators, added oil coolers, built several dozen. TB-3 4M- 34R Mikulin AM-34R with gearboxes providing significantly improved performance, additional tail fin tower drive, tail wheels with hydraulic brakes, aerodynamic modifications of the fuselage wing and radiators, retractable wind turbines. TB-3 4AM-34RD Series of long-range demonstration aircraft with streamlined fuselage and wheel brakes. Some airplanes had single basic gear wheels of 2 meters (6.6 ft) in diameter and three-blade metal propellers. Used for flights to , and in 1933-1934. TB-3 4AM-34RN high-altitude version with AM-34RN engines, four-blade propellers on suspension engines and two-bladed on suspension, 2 meters (6.6 feet) single-stage wheels, turrets upgraded to SHKAS machine guns, a top speed of 288 kilometers per hour (156 kn; 179 mph) at 4,200 meters (13,800 feet), a service ceiling of 7,740 meters (25,390 feet). Tested in August-October 1935, but did not enter production as the main TB-3 design is outdated. THE TB-3 4AM-34FRN/FRNV AM-34FRN/FRNV engines with increased power and four-blade propellers, aerodynamic improvements including streamlined towers, 2 meters (6.6 feet) of main brake wheels, top speed of more than 300 kilometers per hour (160 kn; 190 mph). TB-3D Proposed option with engines An-1 Charomsky 750 hp (740 hp) and design range 4280 km (2310 Nm, Nm, did not enter production, as other performance characteristics were inferior to TB-3 4AM-34RN. THE TB-3 G-2 with M-17 and M-34 engines converted for cargo transport with ANT-6-4M-34R Airactic TB-3, modified for the 1937 expedition to the North Pole with a closed cockpit, one 2 meters (6.6 feet) wheels, three-bladed metal screws. Operators of the Chinese nationalist China Air Force of the Soviet Union Soviet naval aviation accidents and incidents on March 17, 1938, the Polyar Aviation G-2 (CCCP-N210) crashed while landing in The Gelta-Teplica; ground fog forced the crew to perform go-around. Due to the bad CRM, the plane re-entered the fog. The descent continued until the left landing ski fell into the snow, ripping off the landing gear and causing the plane to crash; All seven on board survived, but the plane was decommissioned. The plane was operating on a cargo flight from Tashkent-Fergana. On August 27, 1941, the Aeroflot G-2 (CCCP-L1996) crashed into a hill near Kyzyl Arvat, Turkmenistan, while attempting to land after the crew failed to determine its destination, killing six of the nine people on board. The plane was operating on a cargo flight from Tashkent to Ashgabat. On December 26, 1941, the Aeroflot G-2 (CCCP-L3043) crashed near Dmitrievka (now Bizerke), Kazakhstan, after the plane lost altitude at a turn, killing 26 of the 34 people on board. The plane was operating on a passenger flight from Alma-Ata (now Almaty)-Karaganda-Kazan with high-ranking Kazakh party and government officials. This accident is the deadliest involving the G-2. On December 29, 1941, Aeroflot's G-2 (CCCP-L2010) crashed in the Amu Darya River near Charjou Airport after the plane quickly lost altitude due to spatial disorientation of the pilot, killing seven of the 36 people on board. The plane was operating on a passenger flight from Chardzhou-Ugonch. [16] Specifications (TB-3 4M-17F, 1934 model) Tupolev TB-3 Data from Shavrov[2]General characteristics Crew: 8-10 Length: 24.4 m (80 ft 1 in) Wingspan: 41.8 m (137 ft 2 in) Height: 8.5 m (27 ft 11 in) Wing area: 234.5 m2 (2,524 sq ft) Airfoil: Tupolev A0 (20%) ; tip: Tupolev A0 (10%)[17] Empty weight: 11,200 kg (24,692 lb) Gross weight: 17,200 kg (37,920 lb) Max takeoff weight: 19,300 kg (42,549 lb) Powerplant: 4 × Mikulin M-17F V-12 liquid-cooled piston engines 715 PS (705 hp; 526 kW) Propellers: 2-bladed fixed-pitch propellers Performance Maximum speed: 212 km/h (132 mph, 114 kn) Range: 2,000 km (1,200 mi, 1,100 nmi) Service ceiling: 4,800 m (15,700 ft) Rate of climb: 1.25 m/s (246 ft/min) Time to altitude : 1000 m (3,281 ft) in 4 minutes 3000 m (9,843 ft) in 22 Wing loading: 73 kg/m2 (15 lb/sq.m) Power/mass: 0.15 kW/kg (0.091 hp/lb) Takeoff: 300 m (984 ft) Landing run: 330 m (1083 Cannons: 6-8× 7.62×54mmR DA Machine Guns, 100 63-round magazine Bombs: Up to 5,000 kg (11,000 lb) of standard load bombs See also Tsveno Project Aircraft of comparable role, Configuration, and the Mitsubishi Ki-20 SAB AB-20 Related Lists of Interwar Military Aircraft List of World War II Aircraft List of Soviet Union And CIS List of Bombers Links Wikimedia Commons has media related to Tupolev TB-3. Notes - User, Super. Enterprise. www.vaso.ru. a b c d e f g h i j k l m n Shavrov V.B. (1985). History Design Aircraft v SSSR do 1938 (3 izd.) (in Russian language). Engineering. ISBN 5-217-03112-3. Gunston 1995, page 384-385. a b Duffy and Kandals 1996, p.42. Vanags-Baginskis 1988, p.5. a b Gunston 1995, p.385. a b Duffy and Kandal 1996, p.43. Gunston 1995, p.386. Vanags-Baginskis 1988, p.12. Duffy and the Kandals 1996, p.211. b c d e f g TB-3 (ANT-6). OAO Tupolev (in Russian language). Received on April 16, 2007. Description of accidents for CCCP-N210 on the Aviation Safety Network. Received on November 6, 2016. Description of accidents for CCCP-L1496 on the Aviation Safety Network. Received on November 6, 2016. Description of accidents for CCCP-L1996 on the Aviation Safety Network. Received on November 6, 2016. Description of accidents for CCCP-L3043 on the Aviation Safety Network. Received on November 6, 2016. Description of accidents for CCCP-L2010 on the Aviation Safety Network. Received on November 6, 2016. Glacier, David. An incomplete guide to using airfoil. m-selig.ae.illinois.edu. Received april 16, 2019. The bibliography of Duffy, Paul and Andrey Kandalov. Tupolev: The man and his plane. Shrewsbury, United Kingdom:Airlife Publishing, 1996. ISBN 1-85310-728-X. Gordon, Efim and Vladimir Rigmalt. Tupolev Design Bureau: The history of the Design Bureau and its aircraft. Hinckley, Leicestershire, United Kingdom: Midland Countys Publishing, 2005. ISBN 1-85780-214-4. Gunston, Bill. Encyclopedia of Russian Osprey aircraft from 1875 to 1995. London:Osprey Aerospace, 1995. ISBN 1-85532-405-9. Viktor Kulikov and Mikhail Masslov. Les Bombardiers quadrimothers Sovjetiques Tupolev TB3 and Petkyakov PE8 (in French). Autoro, France: Lela Press, 2001. ISBN 2-914017-05-7. Shavrov V.B. History of Construction Aircraft - SSR 1938 (3 izd.). Machine builders, 1985. ISBN 5-217-03112-3. Vanags-Baginskis, Alex. Chronicle of the Remarkable ANT-6... Blackjack's progenitor Air Enthusiast No. 35, January-April 1988. Bromley, Kent, United Kingdom: Pilot Press ISSN 0143-5450. 1-18. Extracted from the tupolev tb-3. tupolev tb-3 paratroopers. tupolev tb-3 model. tupolev tb-3 icm 1/72. tupolev tb-3 war thunder. tupolev tb-3 zveno. tupolev tb-3 model kit. tupolev tb 3 1/72

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