- Turbo Charger/Compressor/Refrigeration systems (Impeller/Blade/Blisk/Propeller Special Business) - Reverse Engineering - Development and commercialization of mini turbo machinary (Turbo blower/Turbo air compressor)s
We, Alma International Trading FZE, are able to supply Aviation Fuel For Gas Turbine Engines (JET-A1) as below:
AVIATION FUEL FOR GAS TURBINE ENGINES (JET-A1)
SHIPMENT: CIF FUJAHIRA /FOB ROTTERDAM - HUSTON
ORIGIN: RUSSIAN or EUROPEAN
PRICE QUOTE: ON REQUEST BY EMAIL ONLY
MIN QTY: 500,000.00 BBLS
MAX QTY: 5,000,000.00 BBLS
Please read carefully before making a request.
Information on our company policy regarding quotes.
We at Alma International Trading require a Letter of Intent (Loi) from the end purchaser before we can provide a detailed price quote.
Once we receive the Loi, our team will promptly review it and provide you with an accurate and comprehensive price quote.
We do not respond to emails and phone calls to receive information without a written request with the final buyer's details.
Important Notice Regarding False Documents
If the selling company receives any false documents from the buyer or their intermediaries, we will take swift and decisive action. It is our duty to ensure the integrity and legality of all transactions we engage in.
In the event that false documents are presented, we will not hesitate to report the matter to the local police. Furthermore, we will elevate the issue to INTERPOL and the International Chamber of Commerce. Our aim is to protect the interests of all parties involved and maintain a safe and transparent business environment.
We expect all transactions to be conducted in an honest and professional manner.
Used Engines
HS Code 840820
PRICE = US$1,800/PIECE CIF
ORIGIN: THAILAND
PACKAGE: TONS
MIN ORDER:5 PIECES
DESCRIPTION
There are several types of engines used in automobiles. The car engine types are generally described based on two factors: the fuel type and engine layout/number of cylinders (cylinder configuration. One of the most common types of engines is petrol and diesel engines. But that's a generic way to describe a car engine.
SPECIFICATION
General Engine Specifications
Basic Engine Specifications
I-6, 4-Stroke-Cycle-Diesel
Displacement .......................................................................... 12.88 L (in3)
Rated engine speed .................................................................... 2300 rpm
High idle speed ........................................................................... 2530 rpm
Low idle speed (programmable) ................................................... 550 rpm
Peak torque ......................................................... 3,355 N m @ 1200 rpm
Bore ....................................................................................... 135 mm (in)
Stroke ...................................................................................... 150 mm (in)
Aspiration .................................. Supercharged-Turbocharged-Aftercooled
Governor ............................................................................................. ECU
Fuel system type .................................................................. Common Rail
Length ........................................................................... 1960 mm (77.1 in)
Length to flywheel housing ........................................... 1476 mm (58.1 in)
Width ............................................................................. 1195 mm (47.0 in)
Height ............................................................................ 1117 mm (43.9 in)
Weight, net dry (approx.) ................................................1672 kg (3686 lb)
Rotation (from flywheel end) .......................................... Counterclockwise
Flywheel housing/flywheel .................................................... SAE No. 01M
Flywheel teeth ....................................................................................... 155
Tolerances
Power ............................................................................................... +/- 3%
Exhaust Stack Temperature ............................................................ +/- 8%
Inlet Air Flow .................................................................................... +/- 5%
Intake Manifold Pressure ............................................................... +/- 10%
Exhaust Flow ................................................................................... +/- 6%
Specific Fuel Consumption .............................................................. +/- 3%
Heat Rejection ................................