Section 11

 

Air Turbine Gearbox- Repair and reconditioning.

 

Key: NVA  Nozzle vein assembly

 

 

DC and AC power supplies are maintained by a Rotol ADE 383 air driven gearbox.

 

The gearbox is of two-part construction. Comprising

 

1)      Gearbox assembly

 

2)      Air Turbine exducer / nozzle housing assembly.

 

The oil filled gearbox is driven by the air turbine, providing rotary movement for the DC generator and AC alternator.200v, 400hz

 

Hot air is directed from the main engine NRV’s (non return valves), through a pre-cooler to the Air turbine assembly duct. Air is directed over a collection of small governor vanes, which in turn directly control the airflow to the main turbine exducer wheel, translating rotary motion at 16,000 rpm, to the main gearbox. The gearbox is both lubricated and cooled by circulatory oil. The main draw back for the ATGB is the air turbine exducer wheel and NVA. The turbine wheel and NVA housings are constructed from mild steel, and as such are not tolerant to moisture ingress, this results in corrosion of the turbine wheel and NVA guides.

 

Due to the location of the turbine exhaust duct, water ingress is guaranteed, when the aircraft is stored outside, unless the exhaust duct is plugged. This results in the bottom half of the turbine wheel assembly filling up with water and corroding. This has occurred on ZF579. The ATGB therefore requires re-conditioning. 4 spare gearboxes and turbines have been acquired to construct 2 serviceable units.

 

Minor damage to blades can be repaired, however the whole blade assembly will require re-balancing to inhibit main gearbox shaft and bearing vibration during operation. Approximately 12 governor vanes in the existing ATGB’s will require new bearings and taper pins, the severity of corrosion will be revealed upon inspection of the assembly. In order to gain access to the vanes, the nozzle vain housing will need to be split in to two. To achieve this, the Exhaust housing, Exducer, pre-cooler and front cover of the ATGB will need to be removed, to separate the entire nozzle vein housing from the ATGB. Special extraction tools will be manufactured in order to remove the various components without damage.

 

 

 

 

 

 

Below: ATGB assembly

 

 

 

Lower left corner of picture: Gold casing is Air Turbine Housing, including Governor nozzle vein housing.

 

Centre section of picture: Black with secondary turbine on top is, Gearbox and pre-cooler

Top half of picture: Two circular modules attached to gearbox are, Dc generator and AC alternator.

 

 

 

 

 

 

 

Below: Same ATGB from a different angle

 

 

 

 

Above: Air turbine within turbine housing, before removal. Corrosion is clear to see, plus minor damage to one blade leading edge.

 

 

 

 

 

 

 

Below. Taurus Housing removed, to reveal governor vein assembly. Corrosion seen

 

 

 

Turbine, removed with special extraction tool. Coated in phosphorous acid, reaction with corrosion can be seen.

 

 

 

 

 

 

 

Below: After several hours immersed in Phosphorous acid and two rounds of sandblasting, the air turbine is ready for  re-balancing before refitting to main gearbox.

 

 

 

 

17/12/03

 

1) Pre- cooler unbolted and removed

2) ATGB front casing removed, along with one main shaft-bearing race. (8 bearings)

3) Pre-cooler bearing housing removed, to allow main shaft removal.

4) Main shaft bearing housing, removed from nozzle vain housing, to allow nozzle         vein housing to be separated.

5) Nozzle vein housing separated, revealing 12 veins badly corroded. Bearings to be replaced with 12 good bearings from spare housing, taper pins to be manufactured to original material specification and profiled to fit, oversize may be required.

 


 

Above: Nozzle vein housing removed, along with front cover

 

 

Above: Nozzle vein assembly, The 12 badly damaged bearings are evident.

 

 

 

Above: after several hours immersed in diesel., the 12 corroded nozzle guides were removed. The roller bearings on the vein shafts were also corroded badly as the next few pictures show. The damaged guides and veins will be replaced as one from the spare ATGB’s. The guide, vein and taper pin have to be replaced as one, since they are matched during assembly.

 

 

 

 

 

 

Above. NVA with the 12 corroded veins and guides, removed. The remaining 13 housings and veins now move freely after soaking in diesel oil.

 

 

 

 

01/04/04

 

 

NVH from zf585 and zf581 dismantled, serviceable veins collars and roller bearings removed from both, and installed in one NVH to make one complete and serviceable unit.

 

See below plates

 

 

 

Above. Old and new. Left hand NVH shows nozzles in the ‘off’ or closed position

 

 

Above :NVH showing nozzles in the ‘ON’ or open position.

 

 

 

As @01/05/04

 

ZF579, Zf581 and f582 ATGB’s dismantled

 

ZF582 and ZF581 NVH refurbished

 

Outstanding as@ 01/05/04

 

Installation of new split taper pins for NVH on 582 and 581 gearboxes.(awaiting manufacturer return) approx 2 weeks until return

 

Re-installation of NVH’s on 582 and 581 gearboxes, using viton/silicon seals from zf579 and zf586 gearboxes. Taurus seals will be replaced with Hermatite silicon gasket paste. New NVH seals not available hence re-usage, evaluation upon full testing.

 

Re-connection of gearbox front assemblies including NVH, torque up with new tabs.

 

Re-installation of CAU on both 582 and 581 boxes. Torque up, new tabs.

 

Replacement oil pressure release valve for 582 box from ZF579.

 

Re-connection of governor actuator arms and adjustment for full range through 56 degrees.

 

Corrossion treat casings and re-enamel where necessary

 

Oil fill with ox38. ALLOW TO SETTLE. RE-CHECK.

 

Refurbishment of turbine exducer wheels (ongoing).

 

ON speed tests for both refurbished boxes.

 

Re-check levels.

 

 

01/03/05

 

Air Turbine Gearbox removed from ZF579 airframe for refurbishment of second gearbox.

 

 

Above. ATGB being removed from ZF579 for refurbishment.


 

03/04/05

 

First of two gearboxes complete. ZF581 gearbox restoration complete. Exducer to be re-balanced and box oil filled, and re-fitted to ZF579 airframe for on speed testing.

 

Dc generator and AC alternator sent to J Brooker for overhaul and re-build. Upon return ATGB will be fitted for full testing.

 

 

 

 

NVH rear cover ready for fitting to nozzle assembly and ZF581 gearbox, installation completes refurbishment.

 

Refurbished NVH and rear cover ready for final assembly.

 

05/06/05

 

ZF581 and ZF579 ATG refurbishment complete. Exducers sent for rebalancing, to be fitted upon return. Gearboxes to be fully tested by way of air frame installation, and Stad/Palouste supply.

 

 

 

 

 

 

 

Below. ZF579 air turbine gearbox refurbished, prior to Taurus housing installation. Discoloration of exducer is protective coating.

 

 

 

 

Below. Gearbox complete, awaiting fitting.