The Embraer EMB 110 Bandeirante (English: pioneer ) is a Brazilian twin- turboprop light transport aircraft designed by Embraer for military and civil use.
51-635: P95 or p95 may refer to: Embraer P-95 Bandeirulha , a maritime patrol aircraft of the Brazilian Air Force HMAS ; Bandolier (P 95) , a patrol boat of the Royal Australian Navy HMS ; Virulent (P95) , a submarine of the Royal Navy Papyrus 95 , a biblical manuscript Ruger P95 , a 1996 pistol model P95, a NIOSH air filtration rating P95,
102-571: A state regional road in Latvia [REDACTED] Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination. If an internal link led you here, you may wish to change the link to point directly to the intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=P95&oldid=1118164428 " Category : Letter–number combination disambiguation pages Hidden categories: Short description
153-406: A constant-speed propeller increase their pitch as aircraft speed increases. Another benefit of this type of propeller is that it can also be used to generate reverse thrust to reduce stopping distance on the runway. Additionally, in the event of an engine failure, the propeller can be feathered , thus minimizing the drag of the non-functioning propeller. While the power turbine may be integral with
204-416: A large amount of air by a small degree than a small amount of air by a large degree, a low disc loading (thrust per unit disc area) increases the aircraft's energy efficiency , and this reduces the fuel use. Propellers work well until the flight speed of the aircraft is high enough that the airflow past the blade tips reaches the speed of sound. Beyond that speed, the proportion of the power that drives
255-633: A low operational cost and high reliability. On 26 October 1968, the YV-95 prototype performed its maiden flight ; an additional two EMB 110 development aircraft would follow along with an initial order for 80 transport aircraft for the Brazilian Air Force in the following year. Type certification was received from the Brazilian aviation authorities in late 1972, permitting its entry to service in April 1973 with
306-501: A low-mounted wing, and have sufficient capacity to accommodate eight personnel; these stipulations had been drawn from a study of Brazilian commercial air traffic, and aimed to produce an aircraft that would be well suited to the existing airport infrastructure of the country at that time. The resulting specification that had been generated under the IPD-6504 programme would greatly shape the future aircraft. Early work on what would become
357-513: A result, production of the EMB 110 was terminated during 1990. The origins of the EMB 110 Bandeirante can be traced back to the issuing of a directive by the Brazilian Ministry of Aeronautics in 1965; this called for the production of a transport aircraft for both civilian and military operations that would be reliable and possess low operating costs. It was to be equipped with turboprop engines,
408-450: A service ceiling of 21,500 feet (6,600 m). During the 1970s, Embraer opted to build on the success of the EMB 110 by designing an enlarged derivative of the aircraft, designated as the EMB 120 Brasilia ; beyond being large enough to accommodate up to 30 passengers, it was also faster and furnished with a pressurized cabin . All further development of the EMB 110 was halted by Embraer during
459-575: A test-bed not intended for production. It first flew on 20 September 1945. From their experience with the Trent, Rolls-Royce developed the Rolls-Royce Clyde , the first turboprop engine to receive a type certificate for military and civil use, and the Dart , which became one of the most reliable turboprop engines ever built. Dart production continued for more than fifty years. The Dart-powered Vickers Viscount
510-429: Is a turbine engine that drives an aircraft propeller . A turboprop consists of an intake , reduction gearbox , compressor , combustor , turbine , and a propelling nozzle . Air enters the intake and is compressed by the compressor. Fuel is then added to the compressed air in the combustor, where the fuel-air mixture then combusts . The hot combustion gases expand through the turbine stages, generating power at
561-457: Is different from Wikidata All article disambiguation pages All disambiguation pages Embraer P-95 Bandeirulha The EMB 110 was designed by the French engineer Max Holste ; it had been designed in line with specifications issued by the Brazilian Ministry of Aeronautics in 1965. The goal was to create a general purpose aircraft, suitable for both civilian and military roles with
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#1732851162044612-482: Is normally a constant-speed (variable pitch) propeller type similar to that used with larger aircraft reciprocating engines , except that the propeller-control requirements are very different. Due to the turbine engine's slow response to power inputs, particularly at low speeds, the propeller has a greater range of selected travel in order to make rapid thrust changes, notably for taxi, reverse, and other ground operations. The propeller has 2 modes, Alpha and Beta. Alpha
663-494: Is sacrificed in favor of shaft power, which is obtained by extracting additional power (beyond that necessary to drive the compressor) from turbine expansion. Owing to the additional expansion in the turbine system, the residual energy in the exhaust jet is low. Consequently, the exhaust jet produces about 10% of the total thrust. A higher proportion of the thrust comes from the propeller at low speeds and less at higher speeds. Turboprops have bypass ratios of 50–100, although
714-404: Is the mode for all flight operations including takeoff. Beta, a mode typically consisting of zero to negative thrust, is used for all ground operations aside from takeoff. The Beta mode is further broken down into 2 additional modes, Beta for taxi and Beta plus power. Beta for taxi as the name implies is used for taxi operations and consists of all pitch ranges from the lowest alpha range pitch, all
765-616: The P-3 Orion , and the C-130 Hercules military transport aircraft. The first turbine-powered, shaft-driven helicopter was the Kaman K-225 , a development of Charles Kaman 's K-125 synchropter , which used a Boeing T50 turboshaft engine to power it on 11 December 1951. December 1963 saw the first delivery of Pratt & Whitney Canada's PT6 turboprop engine for the then Beechcraft 87, soon to become Beechcraft King Air . 1964 saw
816-830: The Piper Meridian , Socata TBM , Pilatus PC-12 , Piaggio P.180 Avanti , Beechcraft King Air and Super King Air . In April 2017, there were 14,311 business turboprops in the worldwide fleet. Between 2012 and 2016, the ATSB observed 417 events with turboprop aircraft, 83 per year, over 1.4 million flight hours: 2.2 per 10,000 hours. Three were "high risk" involving engine malfunction and unplanned landing in single‑engine Cessna 208 Caravans , four "medium risk" and 96% "low risk". Two occurrences resulted in minor injuries due to engine malfunction and terrain collision in agricultural aircraft and five accidents involved aerial work: four in agriculture and one in an air ambulance . Jane's All
867-590: The Tupolev Tu-114 can reach 470 kn (870 km/h; 540 mph). Large military aircraft , like the Tupolev Tu-95 , and civil aircraft , such as the Lockheed L-188 Electra , were also turboprop powered. The Airbus A400M is powered by four Europrop TP400 engines, which are the second most powerful turboprop engines ever produced, after the 11 MW (15,000 hp) Kuznetsov NK-12 . In 2017,
918-415: The 1980s in order to concentrate its resources on the further development and production of the newer EMB 120 instead. Between 1968 and 1990, Embraer constructed a total of 494 aircraft in numerous configurations for a variety of roles. The passenger model first flew on 9 August 1972 and entered commercial service on 16 April 1973 with the now defunct Brazilian airline company Transbrasil . On 8 July 1985,
969-700: The Brazilian Air Force was reportedly operating 48 EMB 110s. In 2020, 39 Bandeirantes were still in airline service with 15 operators, 31 in North/South America, 1 in Africa and 7 in Asia Pacific & Middle East. The main operators are: Data from Jane's All The World's Aircraft 1988–89 General characteristics Performance Related development Aircraft of comparable role, configuration, and era Turboprop A turboprop
1020-426: The Brazilian airline company Transbrasil . Various customers in both the military and civilian sectors opted to procure the EMB 110 during its 22-year production run. Over one hundred examples would serve with the Brazilian Air Force, who would modernise numerous examples during the twenty-first century to permit their continued operation. The EMB 110, being customisable to suit various roles and operator requirements,
1071-501: The EMB 110 actually predates the establishment of its manufacturer, Embraer , which was founded in August 1969. The lead designer was the French engineer Max Holste. Construction of the prototype was supervised by the Brazilian aeronautical engineer Ozires Silva, who would also play a key role in founding and running of Embraer. The company was created to undertake the aircraft's commercialisation and serial production. On 26 October 1968,
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#17328511620441122-564: The EMB 110 having been superseded by the Embraer EMB 120 Brasilia , a derived successor. During February 1973, deliveries of the type commenced to the Brazilian Air Force. A pair of EMB 111A Patrulha maritime patrol aircraft were leased to the Argentine Navy during the Falklands War , acting as a stop-gap measure between the retirement of the service's last Lockheed SP-2H Neptune and
1173-519: The Soviet Union had the technology to create the airframe for a jet-powered strategic bomber comparable to Boeing's B-52 Stratofortress , they instead produced the Tupolev Tu-95 Bear, powered with four Kuznetsov NK-12 turboprops, mated to eight contra-rotating propellers (two per nacelle) with supersonic tip speeds to achieve maximum cruise speeds in excess of 575 mph, faster than many of
1224-417: The compressor intake is at the aft of the engine, and the exhaust is situated forward, reducing the distance between the turbine and the propeller. Unlike the small-diameter fans used in turbofan engines, the propeller has a large diameter that lets it accelerate a large volume of air. This permits a lower airstream velocity for a given amount of thrust. Since it is more efficient at low speeds to accelerate
1275-459: The control system. The turboprop system consists of 3 propeller governors , a governor, and overspeed governor, and a fuel-topping governor. The governor works in much the same way a reciprocating engine propeller governor works, though a turboprop governor may incorporate beta control valve or beta lift rod for beta operation and is typically located in the 12 o'clock position. There are also other governors that are included in addition depending on
1326-493: The first jet aircraft and comparable to jet cruising speeds for most missions. The Bear would serve as their most successful long-range combat and surveillance aircraft and symbol of Soviet power projection through to the end of the 20th century. The USA used turboprop engines with contra-rotating propellers, such as the Allison T40 , on some experimental aircraft during the 1950s. The T40-powered Convair R3Y Tradewind flying-boat
1377-448: The first aircraft to be operated by the Irish budget airline Ryanair in 1985 was 15-seat EMB 110; the airline continued to operate the type up until 1989. By October 2018, 50 years after its first flight and 498 deliveries, about 150 EMB 110s were still operating at airlines, air taxis , government entities, and air forces around the world. Production of the type came to an end in 1990,
1428-546: The first deliveries of the Garrett AiResearch TPE331 , (now owned by Honeywell Aerospace ) on the Mitsubishi MU-2 , making it the fastest turboprop aircraft for that year. In contrast to turbofans , turboprops are most efficient at flight speeds below 725 km/h (450 mph; 390 knots) because the jet velocity of the propeller (and exhaust) is relatively low. Modern turboprop airliners operate at nearly
1479-534: The first prototype, carrying the military designation YC-95 , performed its maiden flight from São José dos Campos Airport . Piloted by José Mariotto Ferreira and accompanied by flight engineer Michel Cury, it landed after roughly 50 minutes. Prior to this point, a total of 110,000 project hours had been worked, producing 12,000 manufacturing drawings, supported by 22,000 hours of structural and aerodynamic calculations; an estimated 282,000 hours of aircraft manufacturing and tooling has also been expended. The prototype
1530-558: The gas generator section, many turboprops today feature a free power turbine on a separate coaxial shaft. This enables the propeller to rotate freely, independent of compressor speed. Alan Arnold Griffith had published a paper on compressor design in 1926. Subsequent work at the Royal Aircraft Establishment investigated axial compressor-based designs that would drive a propeller. From 1929, Frank Whittle began work on centrifugal compressor-based designs that would use all
1581-455: The gas power produced by the engine for jet thrust. The world's first turboprop was designed by the Hungarian mechanical engineer György Jendrassik . Jendrassik published a turboprop idea in 1928, and on 12 March 1929 he patented his invention. In 1938, he built a small-scale (100 Hp; 74.6 kW) experimental gas turbine. The larger Jendrassik Cs-1 , with a predicted output of 1,000 bhp,
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1632-421: The introduction of modified Lockheed L-188 Electras . On 15 December 2010, the Brazilian Air Force flew its first upgraded EMB 110, which had been equipped with modern avionics equipment. Designated as C/P-95 , the aircraft has had several new systems installed by Israeli firm Elbit Systems ' Brazilian subsidiary, Aeroeletronica . At the time, the Brazilian Air Force had an active fleet of 96 EMB 110s. In 2017,
1683-406: The model, such as an overspeed and fuel topping governor on a Pratt & Whitney Canada PT6 , and an under-speed governor on a Honeywell TPE331 . The turboprop is also distinguished from other kinds of turbine engine in that the fuel control unit is connected to the governor to help dictate power. To make the engine more compact, reverse airflow can be used. On a reverse-flow turboprop engine,
1734-657: The most widespread turboprop airliners in service were the ATR 42 / 72 (950 aircraft), Bombardier Q400 (506), De Havilland Canada Dash 8 -100/200/300 (374), Beechcraft 1900 (328), de Havilland Canada DHC-6 Twin Otter (270), Saab 340 (225). Less widespread and older airliners include the BAe Jetstream 31 , Embraer EMB 120 Brasilia , Fairchild Swearingen Metroliner , Dornier 328 , Saab 2000 , Xian MA60 , MA600 and MA700 , Fokker 27 and 50 . Turboprop business aircraft include
1785-416: The pilot not being able to see out of the rear of the aircraft for backing and the amount of debris reverse stirs up, manufacturers will often limit the speeds beta plus power may be used and restrict its use on unimproved runways. Feathering of these propellers is performed by the propeller control lever. The constant-speed propeller is distinguished from the reciprocating engine constant-speed propeller by
1836-403: The point of exhaust. Some of the power generated by the turbine is used to drive the compressor and electric generator . The gases are then exhausted from the turbine. In contrast to a turbojet or turbofan , the engine's exhaust gases do not provide enough power to create significant thrust, since almost all of the engine's power is used to drive the propeller. Exhaust thrust in a turboprop
1887-621: The programme was bolstered by the Brazilian Air Force (FAB) deciding to issue Embraer with an initial order for 80 production aircraft. Near the end of 1972, the Bandeirante received its Brazilian airworthiness certificate . On 9 February 1973, the first delivery was made to FAB. In a typical configuration, the EMB 110 seated between 15 and 21 passengers, and was flown by a pair of pilots. Various configurations and customisations were possible in order to suit customers' diverse requirements and operating conditions. The EMB 110P1A/41 model, which
1938-494: The propeller that is converted to propeller thrust falls dramatically. For this reason turboprop engines are not commonly used on aircraft that fly faster than 0.6–0.7 Mach , with some exceptions such as the Tupolev Tu-95 . However, propfan engines, which are very similar to turboprop engines, can cruise at flight speeds approaching 0.75 Mach. To maintain propeller efficiency across a wide range of airspeeds, turboprops use constant-speed (variable-pitch) propellers. The blades of
1989-477: The propeller. This allows for propeller strike or similar damage to occur without damaging the gas generator and allowing for only the power section (turbine and gearbox) to be removed and replaced in such an event, and also allows for less stress on the start during engine ground starts. Whereas a fixed shaft has the gearbox and gas generator connected, such as on the Honeywell TPE331 . The propeller itself
2040-446: The propulsion airflow is less clearly defined for propellers than for fans. The propeller is coupled to the turbine through a reduction gear that converts the high RPM /low torque output to low RPM/high torque. This can be of two primary designs, free-turbine and fixed. A free-turbine turboshaft found on the Pratt & Whitney Canada PT6 , where the gas generator is not connected to
2091-585: The same speed as small regional jet airliners but burn two-thirds of the fuel per passenger. Compared to piston engines, their greater power-to-weight ratio (which allows for shorter takeoffs) and reliability can offset their higher initial cost, maintenance and fuel consumption. As jet fuel can be easier to obtain than avgas in remote areas, turboprop-powered aircraft like the Cessna Caravan and Quest Kodiak are used as bush airplanes . Turboprop engines are generally used on small subsonic aircraft, but
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2142-485: The second prototype performed its first flight, while the third prototype followed on 29 June 1970. While these prototypes yielded positive test results, it was recognised that market conditions had shifted to the point where an eight-seat aircraft appeared to be less viable than it had previously appeared; thus, it was decided to quickly redesign the EMB 100 into the EMB 110 Bandeirante , which featured several technological advances along with greater capacity. In May 1970,
2193-410: The way down to zero pitch, producing very little to zero-thrust and is typically accessed by moving the power lever to a beta for taxi range. Beta plus power is a reverse range and produces negative thrust, often used for landing on short runways where the aircraft would need to rapidly slow down, as well as backing operations and is accessed by moving the power lever below the beta for taxi range. Due to
2244-409: Was adapted for various specialist roles, including aerial observation , maritime patrol , and search and rescue missions. During the 1970s, Embraer opted to design an enlarged derivative of the EMB 110, designated as the EMB 120 Brasilia ; being faster, outfitted with a pressurized cabin , and able to accommodate up to 30 passengers, Embraer opted to concentrate its resources on the new aircraft. As
2295-504: Was destroyed in a bombing raid. In 1941, the engine was abandoned due to war, and the factory converted to conventional engine production. The first mention of turboprop engines in the general public press was in the February 1944 issue of the British aviation publication Flight , which included a detailed cutaway drawing of what a possible future turboprop engine could look like. The drawing
2346-480: Was furnished with seats for 18 passengers, had a length of 15.1 metres (50 ft), a height of 4.92 metres (16.1 ft), and a wingspan of 15.33 metres (50.3 ft). It has a maximum cruising speed of 411 km/h (222 kn), while its more economical cruising speed was 341 km/h (184 kn), at which speed an effective range of 1,964 km (1,060 nmi) can be achieved even while retaining reserve fuels for another 45 minutes of flight. The EMB 110 has
2397-524: Was officially presented before various civil and military officials along with members of the press at an event held four days later, during which its maiden flight was repeated. The positive performance of the prototype led to production of the aircraft, and thus the establishment of Embraer, being approved in mid-1969; the newly created company would assume responsibility for its production on 2 January 1970. An additional pair of prototypes were constructed, which were designated EMB 100 . On 19 October 1969,
2448-686: Was operated by the U.S. Navy for a short time. The first American turboprop engine was the General Electric XT31 , first used in the experimental Consolidated Vultee XP-81 . The XP-81 first flew in December 1945, the first aircraft to use a combination of turboprop and turbojet power. The technology of Allison's earlier T38 design evolved into the Allison T56 , used to power the Lockheed Electra airliner, its military maritime patrol derivative
2499-629: Was produced and tested at the Ganz Works in Budapest between 1937 and 1941. It was of axial-flow design with 15 compressor and 7 turbine stages, annular combustion chamber. First run in 1940, combustion problems limited its output to 400 bhp. Two Jendrassik Cs-1s were the engines for the world's first turboprop aircraft – the Varga RMI-1 X/H . This was a Hungarian fighter-bomber of WWII which had one model completed, but before its first flight it
2550-593: Was the first turboprop aircraft of any kind to go into production and sold in large numbers. It was also the first four-engined turboprop. Its first flight was on 16 July 1948. The world's first single engined turboprop aircraft was the Armstrong Siddeley Mamba -powered Boulton Paul Balliol , which first flew on 24 March 1948. The Soviet Union built on German World War II turboprop preliminary design work by Junkers Motorenwerke, while BMW, Heinkel-Hirth and Daimler-Benz also worked on projected designs. While
2601-481: Was very close to what the future Rolls-Royce Trent would look like. The first British turboprop engine was the Rolls-Royce RB.50 Trent , a converted Derwent II fitted with reduction gear and a Rotol 7 ft 11 in (2.41 m) five-bladed propeller. Two Trents were fitted to Gloster Meteor EE227 — the sole "Trent-Meteor" — which thus became the world's first turboprop-powered aircraft to fly, albeit as
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