The jet engine case is a pressure chamber designed to carry jet engine inner core components while withstanding drastic temperature changes and mechanical stresses. The inner structure of the jet engine is composed External Rough Turning Outer Profile Milling Face Milling Internal Rough Turning Internal Groove Turning

of stationary and rotational parts. The jet engine case is typically manufactured on CNC machining centers for a variety of different materials based on their structural location. The casing is cold and made of Titanium and composite materials while the hot area is made of superalloys such as Inconel, Hastelloy and Waspalloy which tend to have high strength machinability resistance. Shoulder Milling Shoulder Milling

A blisk is a turbomachine component comprising both rotor disks and blades which are made of removable single-part blade rings. Blisks may be integrally cast, machined from a solid piece or made by welding the individual blades to a rotor disk. Each structure requires a different machining Titanium Blisk Face Pocket Rough Zigzag Turning 9 Outer Profiling Face Turning Finishing Outer Radial Groovin

technology. ISCAR has developed a variety of substrate materials for inserts intended to machine and sustain high temperatures. Titanium blisks are used for the fan disk at the front end, while superalloy blisks are made for high temperature and pressure compressor zones. Inner Pocket Rough Grooving and Finish Profiling Rough Inner Diameter Machining Inner Pocket Machining Zig Zag Turning and Finish Profiling Inner Pocket Rough Zigzag Turning Inner Profiling, Rough Finish and Grooving

A blisk is a turbomachine component comprising both rotor disks and blades which are made of removable single-part blade rings. Blisks may be integrally cast, machined from a solid piece or made by welding the individual blades to a rotor disk. Each structure requires a different Inconel Blisk Rough Face Turning Face Profile Turn Grooving Rough Blade Profiling Rough Face Grooving Finish Face Turning Inner Diameter Turning Face Profile Turn Grooving 9

machining technology. ISCAR has developed a variety of substrate materials for inserts intended to machine and sustain high temperatures. Titanium blisks are used for the fan disk at the front end, while superalloy blisks are made for high temperature and pressure compressor zones Finish Inner Grooving Finish and Bottom Radius Milling Rough Trochoidal Milling Semi Finish Profile Milling 10

Turbine Blade Turbine blades are part of the jet engine’s hot section (combustor and turbine) rotational part. The blades extract the energy from the high temperature and high-pressure gas produced by the combustor for rotational propulsion. To Blade Root Radius Milling Airfoil Rough Milling

survive this difficult environment, turbine blades are made of special Nickel-based super alloy materials. There are few common machining methods to produce blades according to the shape and size they are made of. Airfoil Finish Milling Root Profile Milling

Landing Gear Landing gear is categorized in three types; nose, body, and wing landing gear; designed and manufactured to withstand drastic temperature changes, outstanding loads, and mechanical stresses. The majority of landing gear is High Feed Milling 6 Profile Milling Pocket Rough Milling

manufactured from high strength steel M300, Ti. 5-5-5-2 and Ti. 10-2-3. There are several methods to produce landing gear, some of which combine dedicated deep drill machining with multi-task or milling center machines. Profile Milling Semi-Finish Milling Slot Milling

Landing Gear Landing gear is categorized in three types; nose, body, and wing landing gear; designed and manufactured to withstand drastic temperature changes, outstanding loads, and mechanical stresses. The majority of landing gear is Small Pocket Milling 6

manufactured from high strength steel M300, Ti. 5-5-5-2 and Ti. 10-2-3. There are several methods to produce landing gear, some of which combine dedicated deep drill machining with multi-task or milling center machines. Fine Boring

Torque Link Torsion links are made of Ti alloy frames which couple the inner and outer cylinders of a landing gear strut together. Typically manufactured in machining centers with relatively high metal removal stock. High Feed Milling

Helical Interpolation Milling High Feed Milling Fine Boring

The cylinder block is the supporting structure portion of the engine between the cylinder head and sump (oil pan), traditionally manufactured from cast iron and was upgraded to a bi-metal block design (aluminum block with Cylinder Block Bush Rods Hole Step Drilling and Chamfering Engine Bottom Block Face Milling Bearing Seats Rough Milling Side Bearing Caps Gang Milling Cylinder Bore Rough Boring

inserted cast iron liners) to reduce weight. Nowadays, newer technology of thermal spray coating processes on the cylinder bore is being used on aluminum blocks. ISCAR provides a wide range of standard and special tooling and machining technology for a variety of block configurations, sizes and materials. Cylinder Bore Semi-Finish Boring Cylinder Bore Finish Boring Thrust Face Milling 6 Bearing Seats Pilot Reamer and Long Reamer Finishing

Cylinder heads perform several functions in the car engine. These includ housing the exhaust and intake valves, the fuel injector, necessary linkages and passages for the fuel and air mixture. They are commonly produced from gray cast iron or cast aluminum for Cylinder Head Top and Bottom Face Milling Valve Line Intake and Exhaust Semi-Finish Reaming Valve Line Intake (before press in) Boring and Spot Facing Valve Line Intake and Exhaust Finish Reaming Valve Line Exhaust Boring and Spot Face Injector Hole Boring and Spot Face

the newer light weight vehicles. ISCAR provides a wide range of standard and special tooling and machining technology for a variety of cylinder head configurations, sizes and materials. Spring Seat Boring and Bottom Facing Cam Axis Inlet and Exhaust Reaming 3 1 Cam Shaft Axis Pilot Boring Spring Seat Back Chamfering Cam Shaft Axis Boring and Spot Facing