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2. Ajax Engines - Wikipedia

   en.wikipedia.org/wiki/Ajax_Engines

   Starting in 1946, Ajax gas engines became a primary product utilized by oil and gas companies. In 1958, the first Ajax integral engine / compressor was manufactured and was specifically designed for field gas gathering applications. It was a DPC 230 and was soon followed by a complete line of Ajax integral engine-compressors from 30-360 horsepower.

3. Toyota UZ engine - Wikipedia

   en.wikipedia.org/wiki/Toyota_UZ_engine

   In 1998, a marine derivative of the UZ powerplant was produced for boating applications. The 4.0 L VT300i engine, producing 224 kW; 304 PS (300 hp) at 6000 rpm and 420 N⋅m (310 lb⋅ft) at 4200 rpm, used the same block as the UZ engine on the Lexus SC 400, GS 400, and LS 400. Applications (calendar years): 1998 Toyota Epic S21 [11]

4. Burckhardt Compression - Wikipedia

   en.wikipedia.org/wiki/Burckhardt_Compression

   These compressors are essential for compressing, cooling, or liquefying gases like hydrocarbon gases or industrial gases. The company operates in two main divisions: - Systems Division: This division focuses on the development, manufacture, and sale of compressor systems and equipment tailored to meet specific customer requirements.

5. General Electric F101 - Wikipedia

   en.wikipedia.org/wiki/General_Electric_F101

   CFM International CFM56: The General Electric F101 is an afterburning turbofan jet engine. ... Compressor: Axial flow, 2 stage fan, 9 stage HP compressor; Combustors: ...

6. Europrop TP400 - Wikipedia

   en.wikipedia.org/wiki/Europrop_TP400

   400+ [1] The Europrop International TP400-D6 is an 11,000 shp (8,200 kW) powerplant, developed and produced by Europrop International for the Airbus A400M Atlas military transport aircraft . The TP400 is the most powerful turboprop in service using a single propeller; only the Soviet-designed Kuznetsov NK-12 and Progress D-27 , using contra ...

7. Pratt & Whitney JT8D - Wikipedia

   en.wikipedia.org/wiki/Pratt_&_Whitney_JT8D

   The JT8D is an axial-flow front turbofan engine incorporating a two-spool design. There are two coaxially-mounted independent rotating assemblies: one rotating assembly for the low pressure compressor (LPC) which consists of the first six stages (i.e. six pairs of rotating and stator blades, including the first two stages which are for the bypass turbofan), driven by the second (downstream ...