Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: Beskrivning: rblogo2färg3 

 

Arboga Robotmuseum

TM2B

Robothistoriska Föreningen i Arboga

Webansvarig

Sidan uppdaterad:2012-07-23 20:19

Start

Missile

Engine

Radar

Simulator

 

Engines and components

 

Turbo Jet Engines

 

RM1, de Havilland Goblin II

 

RM6B, Rolls-Royce Avon

 

RM9B, Turbomeca Aubisque

 

RM8A, Volvo Aero ( P&W JT8D-22)

 

RM8, Afterburner (Volvo Aero)

 

Turbo Shaft Engines

 

GT1A/B, Rolls-Royce Proteus

 

GT1A/B, Compressor Assembly

 

TM2B, Rolls-Royce Gnome

 

GT5, Motoren und Turbinen Union 6022

  

TAM4 Allison 250-C20

 

Piston Engines

 

LY1 Lycoming 0-435-A

 

 

 

              

TM2B (Rolls-Royce Gnome H.1200)

 

 

Technical data

This engine type is manufactured by Rolls-Royce and is powering the Swedish Marine helicopter HKP4 (Boeing Vertol 107 II-14/15).

 

Engine Type: Turbo Shaft Engine with 10 compressor stages, one High Pressure Turbine stage, one Low Pressure Turbine stage.

Length: 61 inch

Width: 17,7 inch

Height: 19,7 inch

Free Turbine Power:1 250 hp

Free Turbine Speed: 19 500 rpm

Free Turbine: The Free Turbine consists of one Turbine stage which rotates with a constant speed of 19 500 rpm

Static Thrust: 152 lb

Engine Speed: 26300 rpm

Engine Compressor Ratio: 8,21:1 at 26 300 rpm

Exhaust gas temperature: 1 265 degrees Fahrenheit

Weight: 485 lb

 

 

 

 

Beskrivning: C:\Users\Ingemar Johansson\Desktop\HKP4 2.jpg

Helicopter 4