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The Legkij Tank Provornova (LTP) is a light tank designed by Lieutenant K. J. Provornov in July 1942. Blueprints for the LTP were discovered in the Main Automotive-Armoured Directorate of the Ministry of Defence of the Russian Federation inventions department, but no prototypes have ever been made.
The cause of the shutdowns has been traced to problems with the Low-Pressure Turbine (LPT). [85] On 1 November 2019 the Indian Directorate General of Civil Aviation (DGCA) asked IndiGo to replace engines on all of the 98 A320neo airplanes it currently operates by January 31, 2020 and suggested to defer future deliveries until the existing fleet ...
The Lycoming (now Honeywell) LTS101 is a turboshaft engine family ranging from 650 to 850 shaft horsepower, used in a number of popular helicopters, [1] and, as the LTP101 turboprop, light aircraft.
Using the PRV method of control, means that the pressure of the feed oil must be below a critical value (usually controlled by other valves which can leak out excess oil back to tank if it exceeds the critical value). The valve opens at a certain pressure and oil is kept moving at a constant rate into the bearing chamber.
Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.
The Pratt & Whitney PW4000 is a family of dual-spool, axial-flow, high-bypass turbofan aircraft engines produced by Pratt & Whitney as the successor to the JT9D.It was first run in April 1984, was FAA certified in July 1986, and was introduced in June 1987.
The IP compressor has a pressure ratio of 3.5:1, and the HP compressor a pressure ratio of 7:1. [36] A closeup of the highly swept Ratier-Figeac propellers. The low pressure turbine (LPT) is provided by Industria de Turbo Propulsores (ITP), and it is derived from the LPT of the Rolls-Royce BR715 regional turbofan. [13]
Data from DTIC, Smithsonian National Air and Space Museum General characteristics Type: Afterburning turbofan Length: 191 inches (485 cm) Diameter: 34.8 inches (88 cm) inlet, 46.5 inches (118 cm) maximum external Dry weight: 3,035 pounds (1,377 kg) Components Compressor: Dual Spool Axial compressor with 3-stage fan, 10-stage compressor Combustors: annular Turbine: 2-stage high pressure, 2 ...
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