Only the UH-1 Huey helicopters were uploaded because only one picture could be uploaded, the S-70/UH-60 Blackhawk helicopters
were not uploaded.
U.S. UH-1 Huey helicopter? The U.S. UH-1 Huey utility helicopter (UH-1?Huey)
The UH-1 Huey utility helicopter was the most famous U.S. Army helicopter of the Vietnam War, produced by the famous Bell Aircraft Company, and the same series of helicopters had already appeared in 1963 to support the military in Vietnam. The same series of helicopters had already appeared in Vietnam in 1963 to support military missions, and this type of utility helicopter is currently the most used model in the world. The helicopter has a crew of one and is equipped with a T53-L-13 turboshaft engine with 1x1400 shaft horsepower. It can carry 11-14 soldiers or 1,759 kilograms of cargo. Technical data: Main rotor diameter 14.63 meters, Length 17.62, Width 2.86 meters, Height 4.41 meters, Maximum speed 204 kilometers per hour, Practical ceiling 3800 meters, Maximum takeoff weight 4309 kilograms, Maximum range 511 kilometers. Following flight time 2 hours 30 minutes. The main categories are: UH-1H for Army. HH-1H, Air Force Ambulance. EH-1H, Army electronic countermeasures type. Transformations: AH-1: Cobra series of helicopter gunships Helicopters in Vietnam loyalty? The UH-1 Huey? Development Overview The UH-1 is a military medium utility helicopter developed by Bell Helicopter, a division of the U.S. company Textron, and is primarily used for evacuation of casualties from the battlefield, general business transportation, and instrument flight training. The military number was originally HU-1, changed to UH-1 in 1963. nicknamed "Huey" (Huey), but commonly nicknamed "Iroquois" (Iroquois). The company number is "Bell" 204. This helicopter is mainly developed to meet the U.S. Army tender requirements, mainly equipped with the Army, the Air Force, the Navy is also equipped, of which the U.S. Marine Corps is equipped with UH-1E, the U.S. Navy is equipped with the HH-1K and TH-1L, UH-1L, and other models. The U.S. Army put out a tender in 1954, and Bell's program was selected in 1955. On October 20, 1956, the first of three prototypes flew for the first time, followed by the development of six YH-40 trial and nine pre-production HU-1. The first HU-1 flew for the first time in September 1958, and deliveries began on June 30, 1959, and were converted in 1963 to the UH -1 numbering in 1963. The UH-1 Huey helicopter? The UH-1 has many modifications, in addition to the U.S. Armed Forces, but also exported to the U.S., Europe, Australia, Asia, many countries and regions, the total production of more than 2,500, is the world's production of the largest number of helicopters one of the several types of helicopters. UH-1 series of helicopters to the end of the 1970s is still the main U.S. Army Assault Transportation Helicopter fleet, from the beginning of the 80's, its status is gradually replaced by the UH-60 helicopter. helicopters. All models of the UH-1 series have been discontinued. Technical features General layout? Single-engine single-rotor with tail rotor layout, the tail rotor is mounted on the left side of the tail ramp. The fuselage is an ordinary all-metal semi-monocoque fuselage structure, consisting of two longitudinal beams and a number of spacer frames and metal skins. The fuselage is divided into two sections, the front section is the main body and the rear section is the tail beam. Rotor system?2-propeller semi-rigid seesaw rotor. Pre-taper and suspension measures are used for smooth operation. The rotor blades are all-metal glued, consisting of extruded aluminum alloy beams, aluminum skins and peak-and-nest cores, with anti-abrasive stainless steel cladding strips wrapped around the leading edges. The rotor blades are attached to the hub body with a paddle root sleeve. The main body of the hub is connected to the main shaft of the rotor in the form of a universal joint. Above the rotor is equipped with a stabilizer bar at 90° to the paddle and connected to a hydraulic swing reducer. The tail rotor is a rigid structure of 2 metal paddles, and the tail rotor shaft is articulated with a diagonal intersecting ball head with pre-taper and suspension, and the engine power turbine is connected to the input shaft of the main reducer through a floating shaft, and the main reducer reduces the rotor speed to drive the rotor and tail rotor. The main reducer drive shaft and circuit are provided with quick release fittings for rapid removal and replacement. Powerplant?The UH-1B is fitted with an American Avico Lycoming T53-L-11 turboshaft engine with a takeoff power of 820 kW. Electronics? Full set of all-weather flight instruments, multi-channel high-frequency transceiver, omnidirectional indicator of heading, relative position of the fuselage to the downtrack and instrument landing indicator, VHF beacon receiver, C-4 navigation compass, 12.7 cm full attitude flight indicator. Modifications The main types of UH-1 are UH-1E, HH-1K, TH-1L, UH-1L, UH-1A, UH-1B, UH-1C, UH-1F, UH-1M.? Data? &? Pictures? Crew: 2 Length: 16.15 meters Rotor diameter: 13.41 meters Height: 3.84 meters? Rotor Diameter (m): 13.41 Tail Rotor Diameter (m): 2.59 Crew Length (rotor placed front and rear) (m): 16.15? UH-1 in the Vietnam War, the first time to prove to the people the role of helicopters in modern warfare, and the first time helicopters large-scale to the battlefield. Also in the Vietnam battlefield, the U.S. Army equipped UH-1 helicopter demonstrated its excellent performance, and thus became famous in one battle, opened up the world market, and almost became synonymous with the world's general-purpose helicopters. And one of the most prominent battles of its performance is the Battle of Ladrone Valley. In a 4-day war in November 1965, U.S. cavalry units met with Vietnamese infantry units, and the two sides confronted each other on the high ground in the center of Vietnam, near Pielku, and thereafter engaged in brutal, near-face-to-face combat in the tall elephant grass. The war lasted four days and four nights, making it almost impossible to tell night from day. The two sides were so close that rifles, grenades and even daggers were used, and, of course, the U.S. Army used helicopters. The end of the battle was marked by the raid known as the Albany Landing, one of the bloodiest single operations of the Vietnam War. It was after this battle that the Bell UH-1 Iroquois helicopter "Huey" (Huey) nickname began to become the name of the battlefield in Vietnam, the U.S. Army Air Corps, an air assault brigade in the battle was almost wiped out. was wiped out. According to Lee Kmiec, who participated in the battle, "the "It was the Huey that helped turn the tide of the war," recalled Kmiec. Known as the Battle of Ladron Valley, the battle began on November 14, 1965, lasted four days, and ended on the 17th. U.S. Army UH-1 helicopters were in and out of Vietnamese fire several times during the battle, successfully transporting men and equipment to two newly opened landing strips known as XRay?and Albany (Albany). Kmiec was a new pilot who began his service in the Army Air Corps in 1964, and prior to that, he had served in the Infantry Regiment at Fort Benning, Georgia. It was at Fort Benning that the U.S. formed the Army's 11th Air Assault Division, which at the time was just an experiment by the U.S. Department of Defense to try to use helicopters on a large scale, and Kmiec was fortunate enough to join the division. Before being sent to war, the division's soldiers were issued new equipment and received new armbands, which were black on yellow with a horse's head embroidered in the center. Subsequently, their unit number changed, and from then on they had a sacred name: 1st Cavalry Division. At that time, the U.S. Army's 1st Cavalry Division trained with UH-1A helicopters, which did not have a good reputation at the time because their engines did not have enough thrust to meet the needs of the multiple missions at that time. Later, the training base at Fort Benning began to switch to the UH-1B helicopter, which many pilots enjoyed flying, but the engine had a drawback in that it took a long time to restart after stopping. In addition, the engines were not equipped with air filters, so debris was usually sucked into the engines during training, and there was a shortage of engine parts at the base at the time, which caused many aircraft to be grounded. The problem was not solved until Bell later improved the engine air intake design and replenished it with a large number of accessories.The UH-60 Black Hawk helicopter is a medium-sized utility/attack helicopter developed from the Sikorsky twin-turboshaft-engined, single-rotor helicopter, the S-70.
Type? Utility helicopter? Production company? Sikorsky Aircraft Corporation? Primary user? U.S. Army Australian Army? Unit cost? $5.9 million? Derived from? Sikorsky S-70? Derivatives?SH-60 Seahawk HH-60 Pave Hawk HH-60 Pine Duck Hawk? <Overview> The Blackhawk series of helicopters can perform a number of different missions, including: tactical personnel transportation, electronic warfare, and air rescue, and several VH-60N Blackhawks have even been utilized as the President's aircraft, Marine One? (also known as the VH-60 White Hawk). On air assault missions, the Black Hawk can carry 11 soldiers and appropriate equipment, or one 105mm M102 howitzer, 30 rounds of 105mm ammunition and four gunners at a time at the same time. When transporting supplies, the Black Hawk can carry 1,170 kg? (2,600 lbs) of cargo, or lift 4,050 kg? (4,000 lbs) of cargo. The Black Hawk is equipped with advanced avionics? (such as GPS) to enhance its battlefield survivability and performance. <History> The instrument panel of the S-70/UH-60 Black Hawk helicopter? A UH-60 Black Hawk helicopter armed with an M60 machine gun, near Najaf, Iraq, May 2005 The Black Hawk was designed in 1972 at the behest of the U.S. Army to replace the UH-1 Iroquois helicopter. Sikorsky*** built four prototypes, the first prototype? (YUH-60) first flew in October 1974, competing with Boeing-Vertol's Boeing-Vertol?YUH-61.Eventually the Blackhawk won the bid for mass production, and the UH-60A entered service in 1979 with the U.S. Army. In the late 1980s, the model was upgraded to the UH-60L?(the first of which was 89-26179), with major upgrades to the more powerful and lifting General Electric T700-GE-701C engines. The model now under development? (UH-60M), which will extend the service life of the UH-60A and UH-60L into the 2120s, will be equipped with more powerful T700-GE-701D engines and state-of-the-art electronics, flight control and navigation systems. <Derivative Models> The UH-60 has been derived from a number of models and versions, with the standard U.S. Army version equipped with the External Storage Support System (ESSS)[1] and the U.S. Army's External Storage Support System (ESSS)[2]. (ESSS)[1], which increases range and performance by adding wings[2] for up to four compartments of secondary fuel tanks and a variety of weapons. Other derivatives are equipped with different equipment and have different capabilities to meet different needs. The UH-60A Black Hawk? The earliest U.S. Army version, the UH-60A Black Hawk. The earliest U.S. Army version, which could carry up to 11 crew members in addition to a crew of four[3] and was powered by T-700-GE-700 engines[4]? The UH-60A?RASCAL?-? A modified version of Nasa's $25 million Rotorcraft-Crew Systems Concepts Airlift Laboratory (RASCAL) program to study helicopter manoeuvrability in three sub-programs: Superaugmented, RASCAL, RASCAL, RASCAL, RASCAL, RASCAL, RASCAL, RASCAL, and RASCAL. Superaugmented?Controls?for?Agile?Maneuvering?Performance?(SCAMP). Automated?Nap-of-the-Earth?(ANOE) Automated Global Point-to-Point Program? Rotorcraft?Agility?and?Pilotage?Improvement?Demonstration?Helicopter Maneuvering and Navigation Improvement Project (RAPID)[5][6]? A UH-60 Blackhawk of the 5th Battalion, 101st Aviation Regiment, provides air support to U.S. ground forces in Salahuddin Province, Iraq? The U.S. executive jet type? The MH-60S is used to extinguish fires EH-60A?Blackhawks? The MH-60S is used to fight EH-60A Black Hawk fires. Modified electronic systems and operator's console to accommodate two electronic systems mission operators. [4]? The MH-60A?Black Hawk? The MH-60A Blackhawk is a new aircraft that has been modified with additional avionics. Modified with additional avionics, precision navigation system FLIR and aerial refueling capability and equipped with T-700-GE-701 engines. [4]? The YEH-60B Blackhawk is a new version of the YEH-60B. The YEH-60B Black Hawk is the first Black Hawk to be built in the United States. Modified the radar and avionics of the UH-60A to serve as a prototype for the Long Range Target Search (LRTS) system. [4]? YSH-60B?Seahawk? -? prototype, which was eventually developed into the SH-60B.[4]? The SH-60B?Seahawk? -? U.S. Navy sea version, based on the UH-60A plus the mark?III avionics system.? Uses the T-700-GE-401 engine. [4]? The NSH-60B Seahawk? -? Permanently used for flight testing. [4]? UH-60C Black Hawk? -? Modified version for the 'C2 mission'. EH-60C Black Hawk? The EH-60C Black Hawk is a modified version of the UH-60A. Modification of special electronic equipment and off-board antennas on the UH-60A? [4]? VH-60D?Nighthawk? The VH-60D Nighthawk is a presidential and VIP aircraft. Presidential and VIP aircraft, also with T-700-GE-401 engines. [4]? SH-60F?Seahawk? The SH-60F Seahawk was a Navy upgrade. Navy upgrade, released in 1988, with air-dropped sonar. [4]? NSH-60F?Seahawk? -?The SH-60F modification used the VH-60N cockpit upgrade program. [4]? HH-60G?Pave Hawk? -?UH-60A modification? used for battlefield search and rescue, has a pod that can lift 200ft of weight, and cables that can withstand a 270kg pull. [4]? The MH-60G?Pave Hawk? -? Special operations-specific version with long-range fuel tanks and aerial refueling tubes, improved radar, with T-700-GE-700/701 engines. [4]? HH-60H?Seahawk? -? Modified SH-60F with attack weapons and defense countermeasure systems, T-700-GE-401 engines. [4]? HH-60J?Jayhawk?-? A US Coast Guard-specific version with a pod that can lift 200ft of weight and cables that can withstand a 270kg pull.? The MH-60K?Blackhawk? -? Special operations-specific version, used by the 160th Special Flight Wing (Night Stalkers), based at Fort Campbell, Kentucky.? The UH-60L?Blackhawk? -? Upgraded T-700-GE-701C engines from the UH-60A?[4]? modified gearbox and shock absorbers. [4]? EUH-60L?(no official name)? The EUH-60L (no official name) -? Increased electronic equipment and can be transported by air. [4]? EH-60L?Blackhawk? -Upgraded version of the EH-60A. [4]? The EH-60L is an upgraded version of the EH-60A. HH-60L?(no official name)? -?UH-60L?Significantly modified upgraded version. [4] The external rescue pod has built-in medical equipment, a complete patient monitoring system, and a change in crew position in the rear cabin. [5]? The MH-60L?Infiltrator (DAP)? MH-60L?Infiltrator (DAP)? Special operations-specific version, used by the 160th Special Flight Wing (Night Stalkers), [7] can be armed with a 30mm chain gun and 2.75" caliber rockets, M134 Green machine gun on the side door or front end.? The AH-60L?Arpía?III?-? The AH-60L?Arpía?III?-?sold to Colombia as an export version. AH-60L?Battle?Hawk?-? The AH-60L?Battle?Hawk?-?sold as an export version to Australia. The UH-60M?Black Hawk? The UH-60M Black Hawk - an upgraded version of the UH-60L[4] - was designed as a wide-rotor system. Designed as a wide rotor system with T-700-GE-701D engines. Modified gearbox . Integral Vehicle Management System computer (IVHMS)? and modernized glass cockpit, light equipment cases. The plan is to replace all of the Army's UH-60A and UH-60L.[6]? The HH-60M?{no official name}? -?UH-60M Medical Mission Edition. [4]? VH-60N?Nighthawk? -? Modified HH-60D for presidential aircraft. [4]? UH-60P?Black Hawk? -? Bought for South Korea as an export version, similar to the UH-60L configuration. [4]? UH-60Q?Blackhawk? -?UH-60A?Medical evacuation version. [4]? YMH-60R?Seahawk? -?MH-60R prototype with ?T-700-GE-701C engines. [4]? MH-60R?Seahawk? -?SH-60B modification? for multi-mission use with T-700-GE-401 engines. [4]? SH-60R?Seahawk? -? Modified SH-60B with better radar and sonar. [4]? NSH-60R?Seahawk? -? US Navy special test version with T-700-GE-701C engine. [4]? CH-60S?Seahawk? -?UH-60L or SH-60R upgraded for cargo transportation. [4]? MH-60S (Knight?Hawk)? The MH-60S (Knight?Hawk) -? Navy casualty evacuation or fleet replenishment, with T-700-GE-401 engines. [4] <User country/region> Australia uses the Black Hawk? Israel uses the Black Hawk? SH-60J for Japan Self-Defense Forces Sikorsky sold the UH-60 design on the defense market, and as a result, more than 20 countries and territories besides the U.S. have purchased the UH-60.Now the UH-60 is in service with the armies of the following countries or territories: Argentina? (Agrupación?Aérea?Presidencial, AAP)? Australia? Austria? Bahrain? Brazil? Brunei Darussalam? Chile? China? Colombia? Egypt? Israel? Japan? Jordan? Korea? Malaysia? Mexico? Morocco? The Philippines? Republic of China? ROC Air Force: 14 S-70C-1s, 4 S-70C-6s, 1 lost so far? ROC Navy: 12 S-70C(M)-1, 10 S-70C(M)-2, 3 lost so far? ROC Army: scheduled to purchase UH-60M, currently under review? Saudi Arabia? Turkey? Thailand? United States Detailed Data General Information Crew: ? At least two pilots? Capacity:? Cargo hold capacity of 2,645 pounds, including 14 soldiers or 6 stretchers, with a maximum external lift of 8,000 pounds? (UH-60A) or 9,000 lbs. (UH-60L) of cargo. Length: ?64?ft?10?in?(19.76?m)? Rotor Diameter:?53?ft?8?in?(16.36?m)? Height:?16?ft?10?in?(5.13?m)? Rotor area:?2,260?ft²? (210?m²)? Empty weight: ?10,624?lb?(4,819?kg)? Loaded weight: ?16,260?lb?(7,375?kg)? Maximum takeoff weight: ?24,500?lb?(11,113?kg)? Engines: ?2×? General Electric T700-GE-701?free turboshaft engines,?1,560?hp?(1,160?kW)? (1,160 kW) each. Performance Maximum airspeed limit:?193?knots?(222?mph,?357?km/h)? Combat radius: ?368?mi?(420?nm,?592?km)? Delivery range: ?1,380?mi?(1,200?nm,?2,220?km)? Practical ceiling: ?19,000?ft?(5,790?m)? Rate of climb: ?700?ft/min?(3.6?m/s)? Rotor load:?7.19?lb/ft²? (35.4?kg/m²)? Thrust-to-weight ratio: ?0.959?hp/lb?(158?W/kg)? Weapons Two 7.62mm M60 or M134 six-barrel aerial machine guns? Can be equipped with a Volcano mine-clearing system? AGM-119 Penguin anti-ship missile? AGM-114?Hellfire missiles? 19 rocket nests of 70-millimeter rockets