OEM Customized wholesale Cylinder Head for kazakhstan Factories
Company Core Philosophy
The company is specialized in casting mould technology design, tooling development, mould making,gravity casting aluminum alloy products, machining service as a whole, and has 36 seniorr&dengineers. 20 years experience in professional mould making.Strong technical team with certain research and development capabilities.Full machinery focus on quality and after-sales service.
Payment & Delivery
Payment Terms: 30% for deposit, 70% before shipment.
Package Details: usually use the standard 1200*800mm wood pallet, but can customized packaging according to the different products.
Delivery： 45 days after order confirmation.
There are 4 workshops in the company which including tooling workshop, casting workshop , machining workshop ,cleaning workshop and one full-equipped laboratory.
China Foundry Expo
Participate in China Foundry Expo every year.
Q:Plant Maturity – Years in service?
Q:Project Management is existed for new production?
Q:Ownership – Main Share Holders?
Q:Export License and/ or Experience?
Q:Products Development time?
Q:Products Cycle time ?
We consistently carry out our spirit of ''Innovation bringing development, Highly-quality ensuring subsistence, Management promoting benefit, Credit attracting customers for OEM Customized wholesale Cylinder Head for kazakhstan Factories, All the opinions and suggestions will be greatly appreciated! The good cooperation could improve both of us into better development!
Unigraphic nx 9 0 mold winzard basic tutorial how to design ejector pin systems
made by: Nguyen Xuan Cung
http://AviationExplorer.com – Delta Air Lines Flight 1141 was a routine domestic passenger flight between Dallas Fort Worth International Airport and Salt Lake City International Airport, Salt Lake City, Utah. On August 31, 1988, the flight, operated by a Boeing 727, crashed upon takeoff from Dallas-Fort Worth, killing 14 of the 108 passengers and crew on board, and injuring 76 others.
Two causes were primarily blamed for the accident: The crew had not ensured that the wing’s flaps and slats were properly positioned for take-off, and the plane’s takeoff warning horn, designed to alert the crew if the engines are throttled to take-off power without the flaps and slats being correctly set, was not operating correctly. The airplane did not gain sufficient speed to climb in a flaps-and-slats-retracted condition, causing a loss of lift and subsequent collision with equipment pertaining to the ILS (instrument landing system) at the departure end of the runway.
DETAILED INFO – Flight DL1141 (Jackson – Dallas – Salt Lake City) left Gate 15 at 08:30 and was instructed to taxi to runway 18L. When first in line for take-off (at 08:59) the flight was cleared for takeoff. The takeoff was uneventful until the airplane reached the rotation phase (at 154 knots, 6017 feet down the runway). As the main gear wheels left the ground, the airplane began to roll violently, causing the right wingtip to contact the runway (1033 feet after lift-off), followed by compressor surges. The plane continued and struck the ILS localizer antenna array 1000 feet past the end of runway 18L. After impacting the antenna installation, the airplane remained airborne for an additional 400 feet, then struck the ground, traversed a ground depression and slid sideways until it came to rest near the airport perimeter fence, 3200 feet from the runway end. Parts of the aircraft had separated in the slide and a fire had erupted in the right wing area, quickly engulfing the rear, right side of the airplane after it came to rest.