1616834880 air end
Product Description
The Atlas Copco 1616834880 is a genuine screw compressor air end manufactured in Belgium for small-capacity industrial rotary screw compressors. This precision-engineered element serves as the core compression module in Atlas Copco GA 5-7 and GX 5-7 series machines. It converts mechanical input power into compressed air through a proprietary rotor profile and a heavy-duty bearing system. Atlas Copco designs this air end for continuous-duty operation at 8 bar, 10 bar, and 13 bar pressure configurations across the 3.7 kW to 7.5 kW power range.
The 1616834880 air end may also appear in technical documentation as 1616-8348-80 or 1616 8348 80. All three formats reference the identical factory component. Maintenance teams should always verify the compressor nameplate and serial number before ordering a replacement element. This verification ensures correct internal clearance matching and confirms the exact factory configuration for the target machine.
Product Overview
The 1616834880 air end is the compression heart of GA and GX series rotary screw compressors. Inside the cast iron housing, a matched pair of helical rotors turns in synchronization. The male rotor receives shaft power from the drive motor through a belt or direct coupling. The male rotor then drives the female rotor through the meshing action of their interlocking lobes. Atmospheric air enters the inlet port at one end of the housing. As the rotors turn, the trapped air volume decreases continuously along the rotor profile. Pressure builds until the compressed air-oil mixture discharges at the working pressure of the compressor system.
This air end operates on the oil-injected compression principle. Pressurized oil enters the compression chamber near the inlet side. The oil film seals the running clearance between the rotor lobes. This sealing action maintains high volumetric efficiency by preventing compressed air from leaking back to the inlet zone. The oil also absorbs compression heat and lubricates the support bearings at both ends of the rotor shafts.
Atlas Copco engineers the 1616834880 for the 3.7 kW to 7.5 kW power class. This places it in the small-capacity industrial segment. Typical end-user applications include automated production line pneumatic controls, automotive repair shop air supply, CNC machining center clamping and tool blow-off, and food and beverage auxiliary packaging systems. The air end supports both belt drive and direct drive configurations. Facilities select the drive type based on motor speed, available space, and maintenance preferences for the specific compressor installation.
| Parameter | Specification |
| Part Number | 1616834880 |
| Alternate Formats | 1616-8348-80 / 1616 8348 80 |
| Product Type | Screw Compressor Air End / Element Assembly |
| Country of Origin | Belgium (BE) |
| Power Range | 3.7 kW – 7.5 kW (5 – 10 HP) |
| Operating Pressure | 8 bar / 10 bar / 13 bar |
| Dimensions (W × H × L) | 570 × 560 × 750 mm |
| Weight | 245 kg |
| Design Feature | Specification |
| Rotor Profile | SAP (Standard Atlas Copco Profile) asymmetric |
| Rotor Configuration | 4/6 lobe (4 male, 6 female) |
| Housing Material | High-strength cast iron |
| Rotor Material | Precision alloy steel |
| Bearing System | High-precision heavy-duty industrial bearings |
| Drive Configuration | Belt drive and direct drive compatible |
| Model Series | Compressor Type |
| GA 5 – GA 7 | Oil-injected rotary screw, stationary industrial |
| GX 5 – GX 7 | Oil-injected rotary screw, workplace/compact |
The 1616834880 air end is cataloged for selected production batches of GA 5 through GA 7 and GX 5 through GX 7 compressor models. These compact rotary screw compressors serve light industrial environments where a reliable compressed air supply is essential. Because Atlas Copco updates internal configurations across production years, always verify the exact compatibility by checking the data nameplate on the compressor canopy and providing the serial number to an authorized parts channel before finalizing an air end order.
Working Principle
The 1616834880 air end incorporates the proprietary SAP (Standard Atlas Copco Profile) rotor design. This profile features an optimized sealing line geometry. During rotation, the rotor lobes maintain a controlled running clearance against each other and the housing bore. The SAP profile shapes the contact line between the male and female rotors to minimize the physical leakage triangle at the discharge end. A smaller leakage triangle means less compressed air recirculates from the high-pressure discharge zone back to the low-pressure inlet zone. This directly improves volumetric efficiency and reduces specific power consumption during continuous-duty operation.
The 4/6 rotor arrangement pairs a four-lobe male rotor with a six-lobe female rotor. This geometric combination balances internal gas forces across the rotor length. The even distribution of pressure loads prevents rotor deflection under full-load conditions. Rotor deformation would increase the running clearance and degrade compression performance over time. The 4/6 configuration also produces lower torque ripple at the drive shaft compared to alternative lobe counts. Smoother torque delivery reduces vibration transmitted to the compressor frame and connected pipework.
Oil enters the compression chamber through dedicated injection ports near the inlet side of the housing. Internal oil galleries cast into the housing deliver pressurized lubricant to each bearing location. Radial bearings at the inlet and discharge ends of both rotors handle the gas pressure loads. An axial thrust bearing absorbs the net thrust force from the pressure gradient along the rotor length. High-precision clearances between the oil seals and air seals prevent lubricant migration into the compression chamber. A dedicated drainage path vents any oil that approaches the air seal boundary. This isolation design ensures the compressed air output remains free of lubricant contamination while maintaining full bearing lubrication.
Failure Symptoms and Replacement Timing
Under normal industrial operating conditions with regular lubricant changes, the 1616834880 air end delivers an expected service life of 20,000 to 40,000 hours before requiring its first bearing overhaul. Several indicators signal that the air end approaches the end of its service interval:
In most service scenarios, the 1616834880 air end can be rebuilt using a complete overhaul kit. The rebuild process replaces the high-precision bearings, shaft seals, and clearance shims. A successful rebuild restores the factory tolerances and extends operational life at a lower cost than purchasing a new element. Full element replacement becomes necessary only when the housing casting shows physical cracks, the rotor surfaces exhibit severe scoring beyond re-machining limits, or the element has suffered total mechanical seizure. Oil analysis results guide the rebuild versus replacement decision. Rising bearing wear metal concentrations signal deteriorating bearing surfaces before vibration levels become critical.
The 1616834880 air end begins with forgings that undergo precision profile grinding. This grinding process holds the SAP rotor lobe geometry within micron-level tolerance of the engineering specification. Atlas Copco controls the surface finish on the rotor flanks to ensure stable oil film retention during loaded operation. A consistent surface finish across the rotor profile contributes to volumetric efficiency and reduces internal friction losses. Atlas Copco also applies a protective surface treatment to the rotor lobes. This treatment resists corrosion from moisture that enters the compression chamber during humid operating conditions.
Each genuine 1616834880 air end is assembled in an Atlas Copco factory under controlled conditions. The bearing mounting procedure controls preload and housing fit to factory specifications. Correct bearing preload prevents rolling element skidding during unloaded compressor operation. Proper housing fit prevents outer ring movement that could damage the bearing seat over time. Before shipment, every air end undergoes a production test stand validation. The test documents airflow rate, power consumption, vibration levels, and discharge temperature at rated operating conditions. This test data confirms that the air end meets the performance specification before it reaches the customer facility.
The serial number on the housing links to the complete assembly records and production test documentation. This traceability supports warranty coverage and simplifies technical support inquiries. Facilities operating multiple compressors benefit from consistent part supply and the confidence of factory-validated replacement elements.
FAQ
More Air Ends List
If you need other Atlas Copco air compressor air ends, we provide more models in the table below or you can submit your requirements to us directly.
| Part Number | Part Name | Part-Number |
|---|---|---|
| 1088005110 | END SOCKET 16MM² | 1088-0051-10 |
| 1088005112 | END SOCKET | 1088-0051-12 |
| 1088005113 | END SOCKET | 1088-0051-13 |
| 1088006130 | PLATE END | 1088-0061-30 |
| 1088006190 | END PLATE | 1088-0061-90 |
| 1088006195 | END PLATE | 1088-0061-95 |
| 1088006197 | END PLATE | 1088-0061-97 |
| 1088151015 | END PLATE HMT.2/2+2/PT/GR | 1088-1510-15 |
| 1088151309 | END PLATE | 1088-1513-09 |
| 1088151516 | END PLATE HMD.1/PT/GR | 1088-1515-16 |
| 1089040691 | END PLATE | 1089-0406-91 |
| 1089050630 | END BRACKET | 1089-0506-30 |
| 1089057313 | PLATE END | 1089-0573-13 |
| 1089057721 | END SECTION | 1089-0577-21 |
| 1089057758 | END RETAINER CLIF FIX35 | 1089-0577-58 |
| 1089928411 | PLATE END | 1089-9284-11 |
| 1089936651 | END CLAMP | 1089-9366-51 |
| 1089936667 | PLATE END | 1089-9366-67 |
| 1089936668 | PLATE END | 1089-9366-68 |
| 1089936669 | PLATE END | 1089-9366-69 |
| 1089942721 | PLATE END | 1089-9427-21 |
| 1089942746 | PLATE END | 1089-9427-46 |
| 1089942748 | PLATE END | 1089-9427-48 |
| 1089950022 | END SEAL KIT | 1089-9500-22 |
| 1091636448 | END BRACKET | 1091-6364-48 |
| 1092000133 | Pre-insulation end | 1092-0001-33 |
| 1092000545 | END PLATE | 1092-0005-45 |
| 1092000811 | END PANEL | 1092-0008-11 |
| 1092000902 | END BRACKET | 1092-0009-02 |
| 1092001271 | END PLATE | 1092-0012-71 |
| 1092001768 | END PANEL | 1092-0017-68 |
| 1092005471 | END PANEL | 1092-0054-71 |
| 1092073301 | END BRACKET | 1092-0733-01 |
| 1092138870 | END PANEL A | 1092-1388-70 |
| 1092138880 | PANEL END | 1092-1388-80 |
| 1092138890 | PANEL END | 1092-1388-90 |
| 1615805800 | BEND | 1615-8058-00 |
| 1615461400 | PANEL-END | 1615-4614-00 |
| 1615458700 | TUBE-2BEND | 1615-4587-00 |
| 1615456100 | TUBE ASY-2BEND | 1615-4561-00 |
| 1615388000 | PANEL-END | 1615-3880-00 |
| 1615381100 | TUBE ASY-1BEND | 1615-3811-00 |
| 1302260400 | TUBE-4BEND | 1302-2604-00 |
| 1302260400 | TUBE-4BEND | 1302-2604-00 |
| 1302246900 | TUBE-2BEND M | 1302-2469-00 |
| 1302246900 | TUBE-2BEND M | 1302-2469-00 |
| 1302246700 | TUBE-2BEND M | 1302-2467-00 |
| 1302246700 | TUBE-2BEND M | 1302-2467-00 |
| 1302246600 | TUBE-2BEND M | 1302-2466-00 |
| 1302246600 | TUBE-2BEND M | 1302-2466-00 |