Leopard 2 SG Tank Gun upgrade to New NATO 130mm L51

Leopard 2 SG Tank Gun upgrade to New NATO 130mm L51 can be done by enlargement (EDM die punch) on internal diameter turret "holding sleeve angular block cube" modification or replacement of an newly forge gun sleeve angular block cube as shown in red square.

European Armour Union Pte Ltd10 Anson Road #10-11 Singapore 079903
E-mail: sales@euroau.com 
web site http://www.euroau.com

Leopard 2 Engine upgrade to 2,000 HP

Leopard 2 Engine Power upgrade to 2,000 HP

  

We provide Leopard 2 SG Engine power upgrade to 2,000 HP with Dual "Two" Diesel 1,000 HP - MT 881 Ka-500 bottom mounted together after 90 degree rotate to the right & another to the left with additional a power transfer box (2 engines direct drive shaft gears to drive Transmission main shaft) use for NATO 130 mm or 150 mm main Gun heavy weight application.

The width & height of the Dual "Two" MT 881 Ka-500 engines dimension fit comfortably in the original Leopard 2 A4 1,500HP engine compartment.

Options on Power Transfer Box, Direct Drive Gears or Planetary Drive Gears are for sale.

The Dual Engines Power output ranges from 1,800 to 1,900 HP.

e-mail: sales@euroau.com

European Armour Union Pte Ltd

10 Anson Road #10-11 Singapore 079903
E-mail: sales@euroau.com 
web site http://www.euroau.com

Development of Wind Tunnel Technology use for F15SG & F16 vertical take off on Endurance 160 Helicopter Carrier.

Development of Wind Tunnel Technology use for F15SG & F16 vertical takeoff on Endurance 160 Helicopter Carrier.

We intended to afloat the F15SG fighter jet to 5 meters in the air using the back wind tunnel and only after the F15SG made stable contact with the Crane flexible U shape carbon fiber spring. Next, the twin jet engines are fired up to take-off thrust: 58,000 pound (26,309 kilogram) to afterburning charging and follow by release of the 2 bottom hydraulic quick release latch cables for the plane to take flight.

The whole process must be done under 8 to 10 seconds to prevent instability to set in.

A Crane located next to back wind tunnel is equipped with 2 Carbon Fiber flexible U shape spring with thick honey comb rubber contact pad attached to hold the wings of F15SG to prevent it from flipping over during afloat.

Meanwhile, the 2 bottom hydraulic quick release latch cables also help to stabilize the F15SG fighter jet during afloat in midair with it jet engine turn on at low speed to maintain stability.

The front wind tunnel will continue to push F15SG higher (or maintains altitude) on it wings lift force (artificial wing lift force from front wind tunnel) as it take off from the back wind tunnel moving forward to the front.

The front wind tunnel has 25% more lifting power than the back wind tunnel which it mission is to afloat the F15SG plane only. (Both Wind Tunnel diameter are at 18 meters each)

Design & Build by European Armour Union Pte Ltd.