Search results
Results From The WOW.Com Content Network
P-Motor was the class designation given by the New York Central a fleet of 22 ALCO-GE electric passenger locomotives. The P Motors were not only more powerful than previous New York Central electrics, but also a more advanced design using the highly successful 2-C+C-2 wheel arrangement found on the later PRR GG1 and New Haven EP-3 classes as well as nose suspended traction motors.
Vauxhall 12-4 1939 Vauxhall 12-4 I Type A total redesign introduced in September 1938 and given the 12-4 name, the new model featured a longer six-light body based on the Vauxhall 10 and a 4-cylinder 1.4-litre engine
The financial details of the transfer include an initial and base fee of €4 million and a maximum of €1 million add-ons depending on sporting conditions. [4] On 27 November, he scored his first professional goals with a brace in a 2–1 win at Bologna in the 2024–25 UEFA Champions League league phase .
The AAR wheel arrangement system is a method of classifying locomotive (or unit) wheel arrangements that was developed by the Association of American Railroads.Essentially a simplification of the European UIC classification, it is widely used in North America to describe diesel and electric locomotives (including third-rail electric locomotives).
Series 5 tests are used to determine if an article can be assigned to HD1.5 'Very Insensitive Explosive'; series 6 tests are used to determine the classification of an article within Hazard Divisions 1.1, 1.2, 1.3, or 1.4; and series 7 tests are used to determine if an article can be assigned to HD 1.6 as an article containing predominantly ...
The Turbomeca Arrius is one of a family of turboshaft engines for helicopter use, first produced in 1981. As of 2012, some 2,700 units had been sold. Power ranges between 357 kW (479 shp) and 530 kW (716 shp) for different versions.
A T56 on a mobile test unit at MCAS Futenma, 1982 T56-A-1 (Series I) A 1,600 lb weight (730 kg) engine delivering 3,460 shp (2,580 kW) and 725 lbf (329 kgf; 3.22 kN) residual jet thrust, which is equal to 3,750 equivalent shp (2,800 kW); single-shaft 14-stage axial flow compressor, cannular combustion chamber with 6-cylindrical through-flow combustion liners, 4-stage axial flow turbine; 13,800 ...
Lockheed hydraulic drum brakes were fitted all round to the same design as the 10-4 and featured a split circuit to prevent complete loss of braking in the event of a fluid leak. The engine was a 4-cylinder 1.4-litre (1442 cc) with overhead valves enlarged from the 10-4 by increasing the bore from 63.5mm to 69.5mm and keeping the same 95mm stroke.