Air Dynamics: Aerospace Manufacturing and Design Magazine Features Desert Wind Environmental Test Chambers

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Central Vacuum System for Advanced Aerospace Manufacturing

Background
During the manufacturing, assembly and rework process of building aircraft, debris is created while forming and joining these structures. Today, aircraft assemblies are procured via the global supply chain. Nose to tail assemblies such as cockpit, passenger compartment, wing, stabilizer and tail cone sections are constructed in a variety of facilities worldwide.

This debris is referred to as Foreign Object Debris or “F.O.D.” This debris is generated during the manufacturing process and assembly of aircraft structures and sub-systems. All aircraft systems are vulnerable to FOD intrusion – avionics, power plants, transmissions, gearboxes, electrical distribution, flight controls, cabin controls, fuel and hydraulic systems. FOD affects all manner of aircraft and airborne vehicles including fixed wing, rotary wing, satellite, satellite launch vehicles, missiles and spacecraft.

FOD encompasses all size and type of debris affecting the inside and outside of the craft, including machining dust, metal chips, nuts, bolts, composites, jewelry, coins, tools, clothing articles, coffee cups, remove-before-flight pitot tube covers, foam insulating materials, water from aircraft washing & rain test, super-cooled upper atmosphere water, ice, snow, desert sand, dust, rodents, birds and so on

FOD can drop into and remain suspended in the radial crevasses of an airframe remaining secure and undetected through pre-flight inspection. Seemingly benign items bring the potential of rendering an aircraft system non-responsive or inoperative affecting any phase of flight.  Catastrophic consequences do occur when FOD interacts with these aircraft systems. Negative G forces in flight may dislodge FOD causing it to interact with the craft’s systems.

This interaction could cause an electrical short, jam flight controls, overheat avionics and navigation systems, puncture in the craft’s skin and block airflow to critical components. Military aircraft are especially prone to these circumstances due to their wider flight envelope.

FOD sources in the Advanced Aerospace Manufacturing Environment
Aerospace aircraft manufacturing starts with raw materials such as metal alloys, composites, laminates and carbon fibers. These materials take the shape of wings, fuselage, landing gear and numerous other aircraft parts. The parts require machining, stamping, de-burring, grinding, sanding and cutting. For example, windows are cut out from aluminum or carbon fiber tube section of an aircraft shell. Various size and shapes of debris are generated during the aircraft manufacturing process.

Without detection and removal, FOD is a leading contributor to loss of property and life. Loosely enforced or lack of procedures and sub-standard FOD removal equipment are inevitable contributors to this ever-present risk factor of flight. In a recent single incident, FOD was identified as the cause, costing the company about five billion dollars.

A proven solution for FOD removal
The Engineered Central Vacuum System
Properly planned and engineered, the central vacuum system integrates specialized equipment and worker procedures resulting in a process to collect debris amidst manufacturing and assembly. The system incorporates a low volume / high velocity collection system designed around the manufacturing processes. Typically, the system parallels the production line with other worker utilities.

FOD critical areas encompass the manufacturing floor and work platforms along the production line including the craft interior. The user guided vacuum system collects FOD with task specific attachments at high velocity.  The system operates continuous during production hours incorporating “clean as you go” programs.

Numerous approaches to FOD removal
FOD practices vary considerably between airframe manufacturers as well as between commercial, military, rotary and space programs. In one instance, workers are checked into and out of critical FOD zones with personal item and tool cart inventories to help ensure best practice in a LEAN environment.

Conversely, even today some aircraft manufacturers use a lackadaisical approach incorporating open shop boundaries, no inventories and shop vacuums attached to the outside of overhead handrails on worker platforms twenty or thirty feet overhead, while producing two hundred million dollar aircraft.

One Canadian manufacturer has identified FOD containment the number one priority of the company – for good reason.

Integration of an FOD system
Air Dynamics provides design and integration services for Advanced Aerospace Manufacturing. A site survey is conducted to determine specific needs based on specific operations. Design criterion is developed for the system. Design, manufacture and installation of a system to service a production line area of 100,000 square feet, could take several months from design to installation.

Air Dynamics FOD Central Vacuum System

  • Features 2 to 50 simultaneous users
  • Covers over 100,000+ square feet of manufacturing floor space
  • System turndown ratio of 50:1 saves energy when idle
  • 316 stainless steel finish for durable life span
  • System is PLC controlled with critical component monitoring & automatic shutdown
  • Automatic hopper emptying

Installation includes training and customized tools and vacuum attachments.

Before
Note: The buildup of FOD collected in the bottom of the pipe.
This presents many maintenance problems
including fire and explosion hazards.
Continual system clogs were costly to maintain

 After
Completed FOD central vacuum indoor installation

FOD vacuum system details
Foreign Object Debris (FOD) Industrial Central Vacuum Systems for advanced aerospace manufacturing.

  • Complete Design, Manufacturing & Turnkey Installation of Air Dynamics engineered vacuum systems
  • Installed horsepower base of 1300+ over twelve systems, serving 200 system users, covering over 1 million square feet. 

Final note
The FOD vacuum systems are one of the least understood types of air and material handling systems. System planners must incorporate adaptable designs for a constantly changing manufacturing environment.

Dan Lehman
President
Air Dynamics
dlehman@airdynamics.net
717-854-4050
www.airdynamics.net

Posted in Aerospace Manufacturing F.O.D. Central Vacuum System, F.O.D. System, FOD System, Foreign Object Debris System | Comments Off

Industrial Fryer – Scrubber Application Example

An Industrial fryer, scrubber or Air Pollution Control Device for commercial cooking is mainly used in two applications:

  • Made to order food in commercial restaurants
  • Food manufacturing of continuous cooking. This includes mixing and formulation of batches of recipes which are then cooked in continuous fryers.

Most of these operations are running 24 hours a day, 365 days a year.

Case history:
Problem:
Industrial fryer in non-compliance within a US EPA “non-attainment” area.

Background:

In the USA there are pollution control laws set by the EPA (Environmental Protection Agency) which regulates pollution for air and water. This problem arose because the EPA designated certain areas as “non-attainment areas” where certain pollutants are not within the Federal guidelines.

The United States Environmental Protection Agency is focusing its efforts to reduce pollution in certain areas across the country. These areas, called US EPA non-attainment areas are receiving more attention from State and Federal regulators in an effort to curb air pollution. The US EPA non-attainment areas are usually in low lying geographic regions of the country, such as large river basins and valleys. Examples are the Ohio River Valley and San Fernando Valley.

Pollutants are categorized as Criteria Pollutants and Hazardous Air Pollutants (HAPS)

The criteria air pollutants and precursors are:
CO – Carbon monoxide
NH3 – Ammonia
NOx – Nitrogen oxides
PM10 – Particulate matter (10 micrometers diameter or less)
PM2.5 – Particulate matter (2.5 micrometers diameter or less)
SO2 – Sulfur dioxide
VOC – Volatile organic compounds

Hazardous Air Pollutants (about 188 of them) start with Acetaldehyde and end with Xylenes.

The Potato Chip Fryer Stack Scrubber was designed to remove particulate matter and oil mist from the Fryer exhaust generated by the potato chip or frying process. In addition to Particulate Matter (PM) the food manufacturing frying process emits oil mist.

Air Pollution Control Devices can capture these pollution emissions to within State and Federal limits.

Several options are available to limit pollution from high capacity fryer operations.

Air Pollution Control Device Examples for High Capacity Fryers are:
· Regenerative Thermal Oxidizer (RTO)
· High Velocity Cyclonic Scrubber
· Low Velocity Mist Eliminator.

These areas are mostly river valleys, bay areas, etc. and if they are not within the EPA guidelines the state must enforce the laws and each environmental district must comply with the law.

This particular site (Potato Chip Maker) was within a US EPA non-attainment area. Upon inspection of the environmental permit, one of the commercial fryers was not in compliance. In this instance, the pollutants in pounds per hours were about a pound per hour (particulate matter in solid and liquid form). The limit was .75 pounds per hour. The commercial fryer was approximately one quarter pounds per hour over the limit.

This issue was brought to Air dynamics by an environmental testing firm because they had prior experience with Air Dynamics success with a different scrubber application.

We visited the site and collected the data. Then, we discussed several approaches with the new client on the best way (at the lowest cost & least maintenance) to solve the problem. The State recommended the “BACT” – “best available control technology”. This was a Regenerative Thermal Oxidizer (RTO). The RTO had a 200hp requirement to run the motors and fans and needed a two inch natural gas line to feed the burner. While this was a viable option, the cost was over $1million to acquire the equipment and many thousands per year to operate and maintain.

Another technology investigated was a Cyclone Scrubber. Basically this is a very tall tower approximately 50 feet high. This tower required substantial steel supports and the equipment required 30hp to operate. The customer did not want to invest the capital to construct the steel structure required.

Solution and Results:

We listened to concerns and designed a scrubber that was easy to access and only 4 feet tall. By using a horizontal configuration and low pressure drop design, we reduced the height significantly and energy consumption was only 15hp. The investment in comparison to an RTO was one fourth the acquisition cost of the RTO and fractionally less to operate. Total cost was approximately 40% less than the Vertical scrubber as well as 50% less in horse power.

We designed the system to remove at least .46lbs per hour, again to minimize cost. During final testing total pollution output was .3 lbs per hour. The design and removal efficiency exceeded our estimates by 40%.

Averse to maintenance ourselves, our goal is to reduce or eliminate maintenance, period. In this case, we designed “CIP”into the system.

Clean-In-Place literally cleans the inside of the unit, similar to a dishwasher. After a year in operation, the result is zero maintenance but still requires periodic inspections. The system is constructed of 100% stainless steel. Even though this was a custom project it took about 10 weeks to manufacture with 6 weeks for the design process.

            

        Before                                     After
The unit and the exhaust from the fan was designed to keep structural requirements to a minimum

                   

         Before                                After

The ports, on right, after the fan exhaust were oriented to avoid the requirement for scaffolding during stack testing saving the customer added expense and contributing towards safety.

Project Notes:

Other units would have had to be ground mounted due to the extreme weight:

  • RTO system – 100,000 lbs.
  • Cyclone Scrubber – 4,000 lbs plus wind loading
  • Air Dynamics Scrubber – 2,000 lbs.

This system was 10,000CFM with a stack temperature of 228 degrees and a super-saturated air stream. We were able to use the existing controls from the previous system that provided adjustable flow with a 30% turndown ratio.

This is the first “green” chip manufacturer in the state of Pennsylvania. Other chip makers typically do not have such controls on their fryer stacks. This system has been operating since July of 2010.

Dan Lehman
President
Air Dynamics
dlehman@airdynamics.net
717-854-4050
www.airdynamics.net

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Environmental Test Chambers: Testing Equipment for Desert Conditions

Background:
In 1991 US military was brought to a point of reality when previous mission planners were not fully prepared for desert operations. When the military began operations under desert conditions, they immediately discovered that critical equipment didn’t last long. It became evident that military hardware and commercially manufactured items, optics, navigation systems, instrumentation computers, etc., began to fail due to the extreme desert environment.

Testing standards with too much variance:
To prepare for these conditions, the test community had limited resources to perform reliable and repeatable tests with sand and dust. This is evident if you look at the mil standard of MIL-STD-810G method 5.10.4.

That current standard has a concentration tolerance of plus or minus 70% under specific test protocols. To put this into perspective, compare this to the MIL-STD-810G for temperature which is +/- 2 degrees Celsius. This equates to a tolerance of 1%. This wide variance in concentration is allowance for test chambers previously available to the test community. Compared to other environmental tests, they are within a few percentage points of the minimum or maximum parameter setpoint. Less variance translates into a more repeatable test. Now we can plot a trend analysis and predict how long equipment will last in a particular desert environment. We can maintain this accuracy with many types of test media including volcanic ash, planetary crustal dust and cosmic dust.

How items should be tested:
Testing a commercial, military or space vehicle/craft, we need to replicate the conditions that nature produces during the sand and dust storm or space travel with one exception – nature produces constantly varied temperature, pressure, particle concentration and wind velocity. In a laboratory environment, a continuously variable test, results in unpredictability for any item subjected to the environmental test.

We want to remove all the variables for a constant state of sand or dust concentration – for wind velocity, temperature, and humidity.

Now we have an environment with constants that we can subject a part or piece of equipment and conduct multiple tests for specimens such as a shoulder weapon, handheld computer system or avionics. If we can produce a failure during the test, and do it in “X” number of minutes, and repeat that again, and a third time…we just plotted the mean time between failures under those very precise conditions.

How desert condition testing was conducted in the Lab and the Military:
Many desert simulations were done using a cobbled together piece of equipment brought into a lab environment (a few major aerospace companies currently have dust chambers made of plywood!).

The tests were performed through a combination of widely varying equipment configurations. Commercial labs would announce their capabilities to perform accurate tests while meeting the standards. The labs tested and usually passed items, only to later fail under field trials. Of course the tests were and still are very low cost, while using patched together chambers using technology suggested in the MIL-STD-810. This type of test is usually accompanied by a hand written checklist as verification that all went well during the test.

Frustrated with the lab results and determined (at a high cost) to test mission critical components, the problem remained. The logical approach, while resource intensive, placed the specimen under real life field conditions.

Several routine approaches were used to ensure specimens were field-ready:

  • By simulating a war-game under desert conditions
  • By strapping a component onto the front of a hum-vee and drive around in a single file convoy for a period of time
  • Employ low flying rotorcraft as a means to generate high particle concentrations and high velocities while following closely behind in a hum-vee where the specimen was strapped to the front of the vehicle.

Again, this produced widely variable test conditions, a cluster bomb approach.

New technology with precise control of variables:
The Desert WindTM system is a compilation of scientific grade equipment that utilizes precision equipment that delivers accurate concentrations of sand or dust using “mass-over-time methodology”. The system provides stable particle concentration, temperature, humidity and velocity. The Desert WindTM technology removes the variables found in nature, hobbled together test chambers and simulated field operations to +/- 5% and below.

Typical laboratory test equipment is constructed using commercial grade enclosures and components. The sand and dust test process requires heavy duty industrial construction using manufacturing process equipment components along with the most powerful industrial microprocessor to accomplish the testing.

Where to go to get items tested:
If you are in the US military or a NATO approved entity, the Naval Air Warfare Center will test specimens for a fee. They have a Desert WindTM system installed in their facility. They explain the systems capability as “the most sophisticated environmental test chamber in the world”

Website: http://www.navair.navy.mil/nawcad/index.cfm

The Center for Aerospace Technology in Canada will test commercialized items. They are ISO 17025 certified and will provide documentable system of protocol for testing for guaranteed repeatability in the test protocol process.

Stéphane Carpentier
Directeur Innovation & développement / Manager Innovation & Development
stephane.carpentier@college-em.qc.ca

CTA – Centre technologique en aérospatiale
5555, place de la Savane,
St-Hubert (Qc) Canada J3Y 8Y9
Tél. /Tel.: (450) 678-2001 p./ext.: 4553
Téléc. /Fax: (450) 678-1702 * www.aerospatiale.org

Items for testing in desert conditions:
Here is a sample of the requests for items to be tested in the Desert Wind environmental test chamber:

  • Sidearms and shoulder arms
    Land based TOE missile (surface to surface) surface to air missile, War fighter personal computer, GPS equipment.
  • Appurtenances on a land based vehicle or aircraft
  • Any part or component on an aircraft for wear abrasion or intrusion while ground based (rotary or fixed wing)
  • Cockpit or canopy, FLIR lens
  • Aerospace coatings
  • Gun turrets

Final note:
We want to test under the most rigid conditions to have the equipment perform as expected – this brings people home alive…


Dan Lehman
President
Air Dynamics
dlehman@airdynamics.net
717-854-4050
www.airdynamics.net

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