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    High Performance Low Flow Fume Hood Design

    Chandra Manik Senior Mechanical Engineer of ESCO Micro Pte Ltd

    Peh Jingpeng Product Specialist of ESCO Micro Pte Ltd

    Abstract

    Fume hoods have always been an integral part of a chemical laboratory. For many years,

    face velocity for fume hoods has been set at 0.5m/s (100FPM ). With escalating energy

    cost, it has become prudent to explore lower face velocity to ensure fume hood

    containment. Esco Micro Pte Ltd performs research focusing on fluid flow characteristicssuch as: reverse flow, turbulence intensity and boundary layers. It was concluded that

    these significantly influenced the containment performance of the fume hood.

    Therefore changes were made to the design of our fume hood to increase the overall

    aerodynamics. Reverse flow in the fume hood were reduced and turbulence was minimized

    with the newly engineered designs.

    The new design established was a new high performance low velocity fume hood. Final

    prototype designed was named as Frontier Acela (for 5 foot size) and tested according to

    fume hood performance test protocol, ASHRAE 110:1995 and EN14175: 2003. Frontier

    Acela passes the tests when operating at a face velocity of 0.3 m/s with the same resultsfor other sizes of Frontier Acela: 4,6,8 foot.

    1.Introduction

    History of fume hoods

    Fume hoods are one of the important equipment in the laboratory. It must guarantee the

    operator safety from being exposed to hazardous gas when performing their experiments.

    Its working principles are divided into three major concepts, extract, contain and finally

    exhaust into the environment. According to history, the first fume hood was a fireplace used

    by alchemist [1]. It was connected to very tall chimneys where the hazardous gas orparticles were exhausted to the environment by thermo-lift effect. In mid 1800s ventilation

    engineers added gas burning rings in the stack to achieve greater thermo-lift. During the

    industrial age, the gas ring gave way to mechanical fans.

    The first major improvement to the fume hood was the addition of the baffle system. With

    this addition, fume hoods started to work like a safety device. Thereafter other types of

    fume hood were introduced, like auxiliary fume hoods and variable air volume fume hood.

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    Measuring fume hood performance

    As fume hoods have an important role in protecting the operators, its performance chart iscompulsory and should be presented both qualitatively and quantitatively. The main

    protocols to measure the performance of fume hoods are ASHRAE 110:1995 and

    EN14175: 2003. These protocols measure the performance at specified operational face

    velocity. Performing smoke tests on the fume hoods provides qualitative assessment, while

    tracer gas containment provides quantitative data. Despite the difference in methods of

    these protocols to each other, they principally represent the same concept.

    Factors influencing fume hood performance

    Fume hood performance is influenced by two factors; first the fume hood designs itself and

    secondly the environment or the system where it is installed. Understanding well thecorrelations of how fluid flow behaves when passing such a shape and its effects on fume

    hood performance is the key for advance development.

    2.Existing problems

    Presence of vortex

    Present designs of fume hoods are unable to fully reduce the vortex in the fume hood

    chamber, especially at the sash opening. To reduce the vortex, the sash handle, airfoil and

    even the edges of the sidewall should be aerodynamically designed to improve uniform

    flow into the internal chamber.

    VAV installation and operating cost

    Variable air volume (VAV) fume hoods were introduced to lower running cost of a fume

    hood by reducing outflow air. Initial installation cost for VAV fume hoods were high, as cost

    for the control system is high. Furthermore, annual calibration of the controller incurs further

    running costs.

    Motorized baffles with sensor

    Motorized baffles that change the angle of incline according to flow of air was installed in

    some current designs of fume hoods. These fume hoods are acting on the principles of

    changing the flow pattern based on the airflow to improve the uniformity of flow and reduce

    turbulence in the fume hood. The main drawback of this system is that it is a feedback

    control system, therefore response time is relatively slow and will not be able to react to

    changes fast enough to reduce vortex formation in the fume hood. Since containment of

    chemical fumes is the main objective of a fume hood, this is not a viable solution.

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    Laminar flow fume hoods

    Recently, a new type of fume hood was introduced. It is the laminar flow fume hood, whereair flow horizontally across the work surface and into the back of the fume hood. This is a

    highly idealized design and will not necessarily work, particularly in cases where hot plates

    are used and will interfere with the horizontal flow. In addition, there is very slow evacuation

    of air at the top of the internal fume hood chamber.

    Face velocity and energy saving

    Although when a fume hood is operated under the specified face velocity is used properly,

    this does not mean the fume hood is capable to contain the hazardous gases. When air

    mixes with chemical substances inside fume hood chamber produces aerosol or other

    mixing types, it can be seen that the velocity will not be the only factor to determine thesuccessfulness in transporting the fluid into exhaust system. Other factors like turbulence

    intensity and flow behavior should be taken into consideration. Some approach should be

    engaged to seek the correlation to each other: changes on fume hood feature to be more

    aerodynamically, baffle orientation and additional auxiliary features.

    3.Objective

    The main purpose of this research are divided into three major objectives as follows:

    1. Recognize the factors influencing fume hood containment performance instead of

    dogmatic operational face velocity at 0.5 m/s

    2. Building features to increase fume hood containment performance

    3. Test fume hood performance according to ASHRAE 110:1995 and EN 14175:2003

    4. Current Fume Hood Concepts

    Push Pull Concept

    Push-pull concept uses auxiliary fan tubular type. This concept consumes less energy

    compared to raising the face velocity of fume hood to meet traditional dogmatic operationalface velocity at 0.5 m/s (100 FPM). Energy saving was achieved by changing the area of

    breathing zone and push the vortex to the back of the fume hood and finally exhausted into

    environment. It is well recognized that vortex is the source for leakage.

    This concept faces challenges when dealing with bigger sizes of fume hood where tubular

    fan at more than 4 feet length is unavailable in market. So in reality, though theoretically

    sound, it is hard to apply.

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    Air dilution and laminar flow concept

    Air dilution concept is purposely used to align the airflow direction from bypass and aimedto counter the area of vortex above the fume hood chamber by becoming an air curtain to

    avoid excessive vortex flow in this zone. The air curtain layers need to be more than one

    and to achieve this condition high density perforated holes on baffle should be applied. In

    fact this method decrease the negative pressure behind the baffle, further creates low

    speed flow as if it is a laminar flow regime.

    When dealing with high-density gases compare to air, this concept faces a difficult

    challenge. The heavy gases tend to occupy the top portion of fume hood and have little

    chance to be exhausted to the environment immediately since there is no slot opening in

    that zone.

    Moving baffle concept

    This concept was generated by deliberating on the possibilities to create laminar flow inside

    fume hood at 0.3 m/s (60 FPM) face velocity. The vortex can be reduced and stabilize

    using Bi-vortex Stable Concept. The main action to make stable vortex is by re-orientation

    of the baffle mechanically using servomotor and with Laplace transformation formula, the

    orientation of baffle adjusted according to the reading of the vortex sensor and counter it by

    such appropriate orientation of baffle.

    Although this concept is sound, the response of baffle is not fast enough to the changes of

    the fume hood performance. Besides, difficulties in maintenance of motor make it less

    appealing.

    Bypass concept

    The concept is simple; introduce air from bypass to sweep the breathing zone of operator.

    Flow was very active even though the airflow from bypass was not as purposed. After

    studying the design concept, it was found that manufacturing a reduce depth of fume hood

    by about 20% compare to other fume hoods help reduce strong negative pressure and

    reduce the flow losses.

    This concept works properly but geometric design will have significant effect in market

    since reduction in depth also reduce the comfort and design space in daily use of the fume

    hood.

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    Supportive flow concept

    The supportive flow concept is similar to push pull concept. An approach to replace thetubular fan using centrifugal fan works properly. Discharge port of the centrifugal pump was

    connected to the armrest airfoil using flexible PVC tube.

    There is a small hole nozzle placed on the side wall of the hood to discharge air from

    blower to sweep the wall area, thus clearing possible contaminant by strong momentum of

    air to the back of the baffle. This concept tried to counter the reverse flow occurring near

    sidewall.

    The concept is a success in countering reverse flow near sidewall and the working table but

    the baffle orientation does not guarantee the user safety when dealing with high-density

    gases. Also high noise from top wall perforated reduces the user comfort.

    5.Computational Fluid Diagram

    Computational fluid dynamics (CFD) is a branch of fluid mechanics that uses numerical

    techniques and algorithms to analyze problems that involve fluid flows. Computers do these

    analyses, as it requires many complex equations. Navier Stokes equations govern the

    CFD problems, and these equations will define any single phase fluid flow. Making use of

    these equations, a stimulation program can do and used to produce a CFD diagram as

    shown below.

    CFD Diagram of Frontier Acela

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    6.Designing the ESCO Frontier Acela

    Frontier Acela was designed to increase energy savings. To achieve this, operational face

    velocity was reduce to 0.3 m/s (60 FPM).

    Concepts and Ideas

    After performing careful research by performing numerical calculation and literature study, it

    was found that changes in design of baffle orientation, sash airfoil, armrest airfoil, exhaust

    collar and bypass can increase the performance of Frontier Acela.

    Compromise Solution(s)

    The various features to support the concepts and ideas generated in previous stage are

    selected to meet the technical merit with regards to mechanical and manufacturability,

    electrical and electronic issues where the high reliability, humble and simple design are the

    focus.

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    Aerodynamic designs of Frontier Acela

    Baffle Orientation

    The mid-baffle was inclined to meet the

    requirement when users deal with high-density

    gases compared to air. The inclined baffle

    leads the flow into exhaust system smoothly

    where its inclined orientation avoid the

    possibility of rolling inside the fume hood

    chamber. A perforated down baffle is designed

    by the consideration to maintain sufficient

    negative pressure for easy transportation of

    hazardous gases and particles directly to the

    back of the baffle.

    Sash Airfoil

    Aerodynamic sash airfoil helps to reduce the

    turbulence intensity at the breathing zone. The

    shape of airfoil was designed after much

    testing and numerical calculation with the

    objective of avoiding vortex flow behind the

    sash and reducing the turbulence intensity.

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    Armrest Airfoil

    One of the most important features in a

    fume hood is armrest airfoil. A correctly

    designed armrest airfoil enhances the

    flow characteristic entering the fume

    hood face by eliminating the vortex

    above working table.

    Bypass

    Bypass maintains the location behind sash, which is close to breathing zone, free from

    contamination by introducing fresh air from the upper baffle. The bypass is also used as an

    air curtain to minimize the possibilities of sudden backflow into operator zone due to the

    environmental changes in laboratory.

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    Exhaust Collar

    Exhaust collar shall be designed to reduce pressure drop and create uniform flow above

    working surface. Saving the energy by lowering face velocity will be useless if high

    pressure drop at exhaust collar still exists. The Frontier Acela (EFA) exhaust collar was

    designed by considering on how to reduce flow resistance, pressure drop and the

    excessive noise that may occur.

    Frontier Acela 5 Ft Pressure Drop

    Diameter exhaust: 305 mm

    Exhaust flow rate: 664 m3/h

    Face Velocity*: 0.3 m/s

    DP sash 500 mm open: 7.64 pa

    DP sash closed: 9.74 pa

    *) About 5-10% additional flow from

    Bypass.

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    Model and Prototype

    The model was built to prove that the design meets the technical challenges. Variousfeatures were analyzed and summarized in protocol based on factory standard in quality,

    manufacturability, electrical and electronic.

    Testing According to ASHRAE 110

    Table 1 show the summary where Frontier Acela was tested according to ASHRAE

    110:1995

    Table.1. Frontier Acela performance test according to ASHRAE 110:1995

    The test performed under condition As Manufactured in ESCO Fume Hood laboratory at

    various face velocity from 0.5 m/s (100FPM) to 0.3 m/s (60 FPM).

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    Testing According to EN14175

    The test set-up of EN 14175 divided into outer grid test (OG), robustness test (RO) and theInner grid test (IG) as shown in Figure

    Outer Grid Test (OG)

    Frontier Acela 5 Ft leak characteristic

    Outer Grid Test

    t(s) Average Leak (ppm)

    60 0.000

    360 0.000

    420 0.003

    600 0.004

    Inner Grid Test (IG)

    Frontier Acela 5 Ft Leak

    Characteristic

    Inner Grid Test

    t(s) Average Leak (ppm)

    60 0.000

    360 0.000

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    Robustness Test (RO)

    Frontier Acela 5 Ft LeakCharacteristic

    Robustness Test

    t(s) Average Leak (ppm)

    60 0.237

    240 0.000

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    7.Conclusion

    To increase Frontier Acela containment performance when operated at 0.3 m/s face

    velocity, several ideas and concepts relating to fluid mechanics were developed and

    applied as follows:

    - Design aerodynamic Side Wall to avoid reverse flow where less aerodynamic design

    will lead to failure.

    - Proper design on sash handle airfoil eliminates separation at boundary edge, which

    enhances protection to the operator breathing zone.

    - Designing carefully and numerically on armrest airfoil was proven to increase the

    protection to operator by countering flow separation above working table.

    - Inclined middle baffle to enhance the reduction of vortex flow inside fume hood

    chamber.

    - Bypass from top baffle helps to reduce the risk of reverse blow into operator breathing

    zone and also used as air curtain to protect sudden back flow due to the laboratory

    environment change.

    - Unique exhaust collar shape, statistically proven to reduction in pressure drop and

    noise levels thus increase energy savings and uniformity of air stream above working

    table.

    Final prototype Frontier Acela 4Ft, 5Ft, 6Ft and 8Ft pass the performance test according to

    ASHRAE 110:1995 The average leak was below the acceptance level of 0.05 ppm for

    condition As Manufactured (AM) according to the protocol ASHRAE 110:1995. Frontier

    Acela also pass the performance test according to EN 14175 (except the EFA 8Ft whichwas not typically familiar in Europe Market, in this case EN14175 was not executed). The

    average leak (see table below) pass the acceptance criterion where the value in Europe

    (Especially in Germany) for Outer grid and robustness test shall be below 0.65 ppm, for the

    inner grid test the acceptance value was referred to French standard that demands the

    maximum leak is below 0.1 ppm.

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    Type of Test EFA-4 EFA-5 EFA-6 AcceptanceValue

    Inner Grid Test 0.000 0.000 0.000 0.100(French)

    Outer Grid Test 0.006 0.004 0.109 0.650(Germany)

    Robustness Test 0.111 0.237 0.242 0.650(Germany)

    8.References

    [1] Saunders GT. Laboratory fume hood-a user manual. New York;Wiley;1993

    [2] Fletcher,B and Jhonson, A.E (1992). Containment testing of fume cupboards-II. Test

    room measurement. British Occupational Hygiene Society.UK.

    [3] Munsen 1989

    [4] Hitching 1996, Hitching and Maupins 1997, Caplan and Knutson 1997; Saunders 1993

    [5] William Peters. Performance Review- the journal of the controlled environment testing

    association; San Antonio; CETA 2008.

    [6] Bell et al 1996

    [7] Lars E. Ekberg, Jan Melin. Required response time for variable air volume fume hood

    controllers. Department of Building Service Engineering, Chalmers University of

    Technology; Sweden;1999

    [8] Bell G, Sartor D, Mills E. The Berkeley hood: development and commercialization of an

    innovative high-performance laboratory fume hood. Berkeley, CA : Lawrence Berkeley

    National Laboratory; 2002 (Report No. 48983)