In order to recover efficiency of the compressor of a gas turbine engine that have been contaminated during operation, engine compressors and turbine sections are routinely cleaned. Wash units connected to wash manifolds are used to spray wash fluid into the engine, most of the time utilizing deionized water or water and detergent mix. This washing of the engine removes contaminants from within the engine and produces a stream of contaminated effluent sprayed out of the engine, in the path of air exiting the engine and from specific engine drains. This wash effluent is contaminated with hydrocarbons, heavy metals and other dangerous materials for the environment and local biosystem. Airport regulations are globally becoming stricter with regards to engine washing and collection of effluent after washing procedure. National, regional and local airport environmental regulations are driving requirement to collect effluent during engine washing maintenance procedure.
A collector for collecting wash liquid from an engine washing operation include a frame; a height adjustable and expandable droplet separator package connected to the frame, the droplet separator package to receive a flow of wash liquid entrained in an airstream emanating from an engine; a height adjustable and extendable chute with side walls and a scissor lift, the chute connected to the droplet separator package and extending at least partially under an engine to collect liquid exiting the engine; a collector tank connected to the frame to collect liquid from the droplet separator package and the chute; and a drainage pipe connecting at least one of the chute and the droplet separator to the collector tank.
A method of collecting wash liquid from an engine during a washing operation includes placing a collector with a frame relative to the engine; adjusting the height of a height adjustable droplet separator package connected to the frame to receive a flow of wash liquid entrained in an airstream emanating from the engine; adjusting the height of an extendable chute with side walls connected to the frame and to the droplet separator package to sit beneath the engine to collect liquid exiting the engine; and collecting wash effluent in a collector tank connected to the frame by separating the wash effluent from the mist exiting the engine with the droplet separator package and transporting wash liquid from the droplet separator package and from the chute to the collector tank.
Frame 14 is on wheels, allowing for the positioning of collector 10 relative to (but not connecting to) engine 12 for collecting wash liquid during a wash operation. Front wheel pair is steerable. Chute 16 with side walls 17 extends and rises with scissor lift 18 on one end to set underneath engine to catch wash liquid from engine drains and other ports. Chute 16 is sloped so that wash liquid collected in chute 16 flows to drainage pipes 24a, 24b.
When performing a washing operation, engine is often cranked, which turns wash fluid into a mist when exiting engine 12. Droplet separator package 20 is raised with lifting system 22 to be positioned directly behind engine 12. Droplet separator package 20 removes the wash liquid entrained in the mist emanating from engine 12 during a washing operation, allowing air to exit. Wash effluent from droplet separator package 20 flows down and is transported to collector tanks 26 through fully enclosed drainage pipes 24a, 24b. Collector tanks 26 can then store wash effluent in frame 14 for proper disposal or treatment for reuse.
Collector 10 with extendable chute 16 with sidewalls 17 and droplet separator package 20 allows for the collection of waste liquid from an engine washing operation and temporary storage in collector tanks 26. By being able to raise and expand both droplet separator package 20 and chute 16, collector 10 is able to provide collection for any size engine 12 and aircraft configuration.
Chute 16 is extendable in three stages with third stage 32 fitting inside of and able to extend from second stage 30 and second stage able to fit inside of and extend from first stage 28. Second and third stages 30, 32 can be extended manually with handle 33. Third stage 32 can be locked in to second stage 30 for extending second stage only. Stages 28, 30, 32 can connect through sliding support beams or other methods. Each stage 28, 30, 32 includes side walls 17a, 17b, 17c that may be rotatable. Second and third stages 30, 32 can be locked through locking pins (not shown) so that chute 16 is secured once desired extension length has been achieved. Add-on side panels 19 can connect between side walls 17a, 17b, 17c and droplet separator package 20 sides to ensure enclosure of engine 12 during a collection operation.
Extendable chute 16 lift includes scissor lift 18, gas spring 38 for vertical chute 16 lifting and manual scissor lift 18 crank 36. When chute 16 is not lifted, as in
In the embodiment shown, scissor lift 18 connects to second stage 30 and includes extension 34 on wheels 37. Extension 34 moves scissor lift 18 out from the center of gravity when lifting chute 16, increasing the torque arm. This increase of the torque arm through extension of scissor lift 18 helps to reduce force on scissor lift 18, allowing for the use of manual crank 36. In other embodiments, scissor lift 18 could connect to other stages of chute 16.
Extendable chute 16 connects to droplet separator package 20 at pivot point 40 to raise with droplet separator package 20. This connection forms a seal to fully contain effluent during washing. Extendable chute 16 also raises with scissor lift 18. This allows extendable chute 16 to be raised at one or both ends and positioned and/or angled properly to collect wash liquid coming from an engine no matter the engine size, height and/or orientation.
Drainage pipe 24b then drains liquid collected by chute 16 to collector tanks 26. The ability to extend, raise, and tilt chute 16 provides for a more flexible system to collect and properly transport wash liquid from underneath an engine during a washing operation. Side walls 17a, 17b, 17c, which are extendable with chute 16 helps to ensure wash liquid is collected and does not run out sides of chute 16, so that it can be transported to collector tanks 26 where it can be properly disposed of and/or treated. Sidewalls 17a, 17b, 17c and additional enclosure panels, for example, panel 19, enclose engine 12 to ensure protection from side wind and compete collection of effluent during washing operations. Extendable scissor lift 18 and gas spring 38 and manually extendable stages 30, 32 ensure that chute can be raised, lowered and extended properly by manual force, making for a more flexible collector system which does not require electric power for operation. While chute 16 is shown with three stages 28, 30, 32, in other embodiments, chute 16 could have more or fewer stages. Additionally, other embodiments could have alternative lift mechanisms depending on system requirements.
Side droplet separator panels 46 connect to and are extendable to the sides of first main droplet separator 42 and second main droplet separator 44. Top droplet separator panels 48 are connected to and extendable on top of second main droplet separator panel 44. Side droplet separator panels 46 and top droplet separator panels 48 can be moved manually and can include locking mechanisms (not shown) to lock the panels 46, 48 at the proper extension and orientation for a collection operation.
First lift linkage wire 52 connects to first (master) crank 50 and to slave lifting rod 59 (see
When the first main droplet separator 42 is lifted, second main droplet separator 44 is also raised. A safety support (not shown) can be used with lift system 22 to ensure droplet separator package 20 is locked in position, for example to allow a maintenance operation.
First crank 54 with first lift linkage wire 52 raises first main droplet separator 42 and second main droplet separator 44 to a desired height for collecting wash liquid emanating from an engine in an airstream. Chute 16 is also lifted at one end with first crank 54, as it is pivotally connected at connection point 40 to first main droplet separator 42 to move vertically with first main droplet separator 42. Second crank 54 with lift wires 56 can then raise second main droplet separator 44 above first main droplet separator 42. Side panels 46 and/or top panels 48 can be individually moved to the sides and/or top of first main droplet separators 42 and/or second main droplet separator 44 to expand the collection area of droplet separator package 20.
Droplet separator package 20 collects spray of liquid exiting an engine during a wash operation. Wash liquid entrained in an airstream flows through a band of curved vanes in droplet separator package 20, subjecting the droplets to forces of inertia and directional flow changes. These forces divert the droplets from their original air flow, causing the droplets to stay within the droplet separator package 20 and collect at the bottom to flow through drainage pipe 24a (see
Lift system 22 allows droplet separator package to be easily manually raised, allowing for a more versatile collector 10 which does not need power to operate. Having a plurality of main droplet separators 42, 44 as well as side extension panels 46 and top extension panels 48 allow the droplet separator package 20 to expand or contract to be able to meet area requirements for collection on an engine of any size. Lifting system 22 that can raise first droplet separator 42 and second main droplet separator 44 together or separately also allows collector to be able to vertically meet height requirements for collection from any engine.
Collector tanks 26 are fully enclosed in frame 14 and can include separate compartments which may or may not be connected. A plurality of compartments can make maintenance and cleaning of collector tanks 26 easier. Drainage pipe connections 66a, 66b receive drainage pipes 24a, 24b to transfer wash liquid collected into collector tanks 26. Outlets 70 can include a quick coupling for connecting to a hose, a treatment system or other device to allow for emptying of collector tanks 26.
Support legs 62 connect to and extend from each side of frame 14. Support legs 62 act to stabilize frame 14 and entire collector 10 during a washing operation. Support legs 62 extend from each side of frame 14 and are vertically adjustable to relieve stress on front wheels 72 and support collector 10. This can be helpful in situations where the ground may be uneven, inclined or adverse conditions are present, such as a strong wind.
Tow bar 64 connects to frame 14 at front axle. Front wheels 72 and axle connect to frame 14 through turntable 68. Mounting front wheels 72 and tow bar 64 on turntable 68 allow for easy manual maneuverability of collector 10. Front wheels 72 can also include a parking brake (not shown) that may be connected to the tow bar 64 position and act to ensure collector 10 does not move during a washing operation. For example, the parking brake can act on the front wheels 72 when the tow bar 64 is in a vertical position. Tow bar 64 may be held in that vertical position through the use of a locking pin, for example.
Frame 14 with fully enclosed collector tanks 26 and support legs 62 provides a stable and secure base to support collector 10 and store wash fluid during a washing operation. Turntable 68 and tow bar 64 allow for easy maneuvering of frame 14 and thus collector 10 as a whole, enabling manual placement at any engine washing location desired. The use of support legs 62 also allows for placement on uneven or inclined ground, where other collector systems may not be able to perform. Dual outlets 70 allow for quick and easy emptying of collector tanks 26 so that collection operations can be quickly resumed.
As seen in
This folding up of collector 10 allows for easy transport and storage. Additionally, this allows for collector 10 to be very versatile, having extension portions in both chute 16 and droplet separator package 20 to expand to collect wash liquid from very large engines, while being able to compact to collect wash liquid from very small engines as well. Compaction also reduces the storage space required for collector 10.
In summary, collector 10 with extendable chute 16 with sidewalls 17 and expandable droplet separator package 20 is a versatile collector that can expand, raise and/or orient parts to collect liquid from a washing operation for any engine type and size and is manually operable. Frame 14 with tow bar 64 and turntable 68 allow for easy maneuvering of collector 10 to where an engine needs washing. Lifting system 22 and scissor lift 18 allow for vertical movement and/or tilting of chute 16. Scissor lift 18 with extension 34 and gas springs 38 allow for the manual crank 36 lifting of chute. Lifting system 22 with first main droplet separator 42 and second main droplet separator 44, manual cranks 50, 54 with lift wires 52, 56, lifting rod 59 and gas springs 60 allows for easy and stable manual raising of droplet separator package 20 and one end of chute 16. Pivotal connections (40) between droplet separator package 20 and chute 16 as well as chute 16 and scissor lift 18 allow for tiling of collector 10 components to adequately collect wash liquid and drain to drainage pipes 24a, 24b. Frame 14 with support legs 62 provide a stable base to support and stabilize collector 10 during wash operations despite environmental conditions and/or challenging terrain. Collector 10 allows for efficient collection of wash liquid from an engine operation for any engine type or size by providing a versatile droplet separator package 20 and chute 16 that can be easily towed to an engine 12 that needs washing, and then manually set up and operated, not requiring power to run. This makes for a more flexible system, as it can be easily transported to anywhere an engine 12 needs cleaning and does not require any connections to power sources or any physical connection to the engine. Thus, collector 10 provides for fully mechanical, safe, low maintenance effective and efficient collection of liquid during a washing operation and allows for washing of a wide range of aircraft and engine combinations without changing components.
While collector 10 and wheels 72 are shown as manually operated systems, in other embodiments, collector system could include an electrically powered system for movement of collector. While lifting system 22 and scissor lift 18 are both shown as manual crank lift systems, in other embodiments, lift systems could include an electrically powered actuator or hydraulic lift system.
While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
Filing Document | Filing Date | Country | Kind |
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PCT/US2014/028255 | 3/14/2014 | WO | 00 |
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WO2014/144023 | 9/18/2014 | WO | A |
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