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AC)-A158 596 PERFOfImANCE COUPAINISON OF THIRTY TiIOSTAGE DEiAPO I/I REWULATOAS(U3 ADUIRALTY RESEARCH ESTADLISHMENT fIARINE TECHNOLOOY) POATSOU.. I A HIMNS JAN 84 UNCLASSIFIED ARE1I08 -3aIa DRIC- KR- 41-10 I/ Rill No AIY

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Page 1: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

AC)-A158 596 PERFOfImANCE COUPAINISON OF THIRTY TiIOSTAGE DEiAPO I/I

REWULATOAS(U3 ADUIRALTY RESEARCH ESTADLISHMENT fIARINETECHNOLOOY) POATSOU.. I A HIMNS JAN 84

UNCLASSIFIED ARE1I08 -3aIa DRIC- KR- 41-10 I/ Rill No

AIY

Page 2: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

1 0 a

R. "I= IZ11111 1*10I~mono

l126 now4

Page 3: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

-h ----- - ---....

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9 7

i

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Page 5: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

ARE(M6) TM 83818

PERFORMANCE COMPARISON OF THIRTY, TWO-STAGE DEMAND REGULATORS

by

I A HIMMENS

Summary

The results of the ARE(EDU) tests on thirty, two-stage demandregulators showed that only two met the RECO4MENDED LIMITSfor breathing resistance and work of breathing for the threeventilation rates at the maximum depth of 50 mew. A majorityof the regulators exhibited a rapid degradation of inhalationresponse at a ventilation rate of 62.5 1/sin, beyond theirrespective maximum depths or as cylinder pressures approached

e 30 Bar

ARE Experimental Divinr Unitc/o HMS VERNON

Portsmouth Hants POI 3ER January 1c94

(C)

Copyright

Controller HNSO London

1984

W I

I

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CONTENTS Pare

INTRODUCTION

TEST PROCEDURE

a. Setting up the regulator for test

b. Testinr the regulators

c. Instrumentation

RESULTS 2

DISCUSSION OF RESLTS 2

a. General comments

b. Effect of cylinder pressure on demand regulator

performance Ic. Demand Regulator Classification

CONCLUSIONS Accession For 4

us RA&I1DTIC TABUnannounced 0justificatio

4By

Distribution/

Availability Codes

Dist Special

J

• , "

Page 7: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

NT.RTION

1. 4 his report presents the results obtained from an evaluation of thirtycommercially available two stage air demand regulators. The tests, carried outin the Admiralty Research Establishment Experimental Diving Unit (APE/EU)unmanned hyperbaric facility, followed procedures which have been agreed betweenAE/EDU and NEDU Naval Experimentr' Diving Unit in the USA-T7 One rerulator ofeach type submitted for test was supplied to ARE/EDU by the B and UEAA onbehalf of the Society for Underwater Technology.

/ e objo ec tive oe tests were:

a. to determine the variation in breathing resistance and work ofbreathing for each of the demand regulators submitted for test; and

b. to compare and assess the results with respect to chosen physiologicallimits (see Annex A).

For the purposes of this study:

Each demand regulator was tested in the "as received" condition, and theresults were compared and assessed with respect to recommended and acceptablelimits proposed by Morrison et al (2) for Work of Breathing and BreathingResistance contained in Annex A.

TEST PROCEDURE

a. Setting up the Regulator for Test

2. The demand regulator was mounted vertically within the HyperbaricChamber as shown in Fig 1. The air supply to the first stage of the demand

* Iregulator was provided via a standard twin cylinder manifold, one side ofwhich was connected to the air supply from the main control console of thetest facility and the other side to a 82 cu/ft steel cylinder mounted withinthe pressure chamber. This arrangement enabled tests to be carried out. I

a. at a constant supply pressure via the main control console, or

b. with a falling supply pressure via the steel cylinder: in thiscase the supply from the main control console was isolated aftercharging the cylinder to the required starting pressure.

3. First of all, air pressure was applied to the equipment and all connec-tions were checked for leaks. The pressure vessel was then closed and floodedto a depth which prevented surface effects interfering with the performanceof the regulator.

b. Testing the Regulators

4. Initially, each regulator was tested under surface conditions, ie normal* atmospheric pressure, and then at pressures corresponding to depths between

10 maw and 50 maw in increments of 10 ow. At each depth the regulatorswere tested at the ventilation rates listed in Table 1. Testinp was completedwhen results corresponding to all ventilation rates had been obtained at eachtest depth or when the breathing resistance of the demand regulator at a

1

ib - -

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ventilation rate of 62.51RMV was high enough to exceed the recording limitsof the instrumentation.

5. The main tests were carried out with a pressure of 70 Bar applied to thefirst stage of the demand regulator via the main control console supply. Inaddition, the effect of falling cylinder pressure on the performance of thedemand regulator was investigated as the pressure of the air supply from thecylinder was reduced from 180 Bar to 30 Bar. This was determined at a venti-lation rate of 62.51RMV and at the depth at which the performance of theregulator just remained within the ACCEPTABLE LIMITS.

c. Instrumentation

6. During the testing of each regulator the first stage supply and outletpressure were monitored by strain gauge type pressure transducers, the out-puts beinp displayed on a Y-Time chart recorder. A differential pressuretransducer was connected at the mouthpiece of the second stare of the demandregulator to measure the variations (Delta P) in pressure from ambient withinthe chamber. The output from this transducer was recorded simultaneouslywith the corresponding breathing machine piston displacement on an X-Yplotter to produce a pressure-volume diagram. An example of such a P-V loopis shown in figure 2, the area of which is proportional to work of breathing,measured in Joules/litre (J/l). The maximum inhale and exhale pressures inKilo Pascals (kPa) are determined from a reference line on the P-V diagram,corresponding to zero pressure variation. At the intersection with thisreference line there is assumed to be no gas flow. 'Spikes' within the P-Vloop which were small in area were ignored in computing the Work of Breathing,unless clearly of significance.

0 , RESULTS

7. A large number of P-V diagrams were obtpined during this trial and these areheld under separate cover at ARE(EDU). Only selected P-V loops have been includedin this report in order to illustrate specific points raised in the discussion ofresults. Figures 3 and 4 show the maximum depths at which the RECOMMEDED LIMITS Iwere met for inhale and exhale breathing resistance respectively, at ventilation

rates equivalent to 22.5, 4o.0 and 62.5 litre RV. Figures 5 and 6 show the depthsat which the combined results for inhale/exhale breathing resistance and work ofbreathing met the RECOMMENDED LIMITS AND ACCEPTABLE LIMITS respectively, for theventilation rates of 22.5, 40.0 and 62.5 litre RMV.

DISCUSSION OF RESULTS

a. General Comments

8. The performance of the r-gulators varied greatly over the entire depthrange. It would be desirable for the breathing resistance and work ofbreathing of any underwater breathing apparatus to be independent of depthand ventilation rate but in practice this is not generally so. (It wouldalso be desirable for the inhale and exhale work to be of similar magnitudewhen the total work of breathing approached the RECOMMVDED LIMITS and thiswas the case for some of the regulators tested). The P-V diagrams for atypical two stage demand regulator, as shown in figure 7, indicate that theinhalation resistance and work of breathing increases more rapidly withincreasing depth at a ventilation rate of 62.51RqV. In one case, however,

47

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(see fi,-ure 8) the breathing resistance and work of breathinp increasedwith depth gradually. Of the thirty regulators which were tested only twomet the RECOMMENDED LIMITS for breathinp resistance and wort, of breathinp,at the three ventilation rates and at the maximum test depth of 50 maw(see figure 5). One regulator, indeed, did not even meet the RECOY?1 DEDLIMITS for work of breathing at any of the ventilation rates for surfaceconditions.

9. In one particular regulator there was a very low inhalation resistancewhich appeared to be independent of both depth and ventilation rate, butthe exhale resistance exceeded the RECOMMENDED LIMITS at a depth of only18 maw. In this case, shown in figure 9, the exhale work of breathing fora ventilation rate of 62.5 1/min at 50 maw represents over 90% of the totalwork measured. Several regulators exhibited very high cracking pressuresat the beginning of inhalation so that a significant level of work wasrenuired to initiate glas flow as illustrated in figure 10. The response ofone of the regulators with a venturi assisted second stage contained a veryhigh positive pressure during inhalation (see figure 11). The magnitude ofthis positive peak was found to be both depth and ventilation rate dependent,and results from a gas flow rate which greatly exceeds that required durinrinhalation. Although such conditions reduce the area contained within thePV diagram the diver is required to do work in resisting the excess pas flowduring inhalation as shown in figure 11. The work of breathing is thenthat contained in the two half cycles as shown cross hatched in figure 12.The work done in resisting excess gas flow during inhalation has been neglectedin deriving the results contained in figures 5 and 6. However, the physiologicalimplications of such high levels of positive pressure during inhalationrequires further investigation.

b. Effect of Cylinder Pressure on Demand Regulator Performance

10. The results obtained from the initial 70 Bar cylinder pressure testswere used to determine the depth at which the regulator could reasonably beused with reducing cylinder pressures. In general, the design of a firststare regulator can be classified as balanced or unbalanced; the outputpressure above ambient beinp controlled by a piston or diaphragm sensingmechanism respectively. It would be expected that a balanced first stageregulator would have an output pressure above ambient that did not changesignificantly with cylinder pressure. The series of P-V diagrams for abalanced first stage shown in figure 13, for a ventilation rate of 62.5 1/sinat the maximum depth of 50 maw, indicates relatively small increases ofinhalation resistance and work of breathing for decreasinp cylinder pressure.In contrast, the output pressure from an unbalanced first stage regulatorwould be expected to change significantly with decreasing cylinder pressure,as shown in figure 14.

11. In the present tests, approximately fifty per cent of the demandreulators, irrespective of type (balanced or unbalanced) showed a rapidincrease of inhalation resistance and work of breathing at their respectivemaximum depths, as the cylinder pressure apuroached 30 Bar. The differentdepths and cylinder pressures at which these effects were measured makesgraphic comparisons between regulators impracticable.

, 3

OnL

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C. Demand Regulator Classification

12. The criteria by which the performance of underwater breathingapparatus should be judged on a generally agreed basis has yet to beresolved. Morrison has suggested that the limits for breathing resis-tance and work of breathing proposed by him (2) might be used to deter-mine the suitability of a demand regulator for use at depths of 30m and50m. The depth of 30m was selected as the "normal practical limit formost sports divers" whilst 50m is the recommended maximum depth for airdiving. If adopted, regulators meeting the lower limit (see Annex A)would be classified as RECOMMENDED for use at the appropriate depthwhilst those meeting the upper limit would only be classified asACCEPTABLE for use at the apprrpriate depth. The results Dresented inFigure 5 show that even at 30 msw a large proportion of tie regulatorstested failed to meet the RECOMMENDED LIMITS. Fipure 6 shows that thespread in the results is reduced if the ACCEPTABLE LIMITS are used asthe accentance criteria. However, this is only achieved at the expenseof a significant reduction in the acceptance standards.

13. These tests have demonstrated that the RECOMMENDED LIMITS proposedby Morrison are achieveable. However, in view of the wide variation inthe measured performance of tke regulators, it seems that it would bedifficult to obtain universal acceptance of the RECOMMENDED LIMITSproposed by Morrison. The minimum information required to define theperformance of each demand regulator is contained in Table 2.

CONCLUSIONS

1. Marked variations in performance were observed during the testinr of 30demand regulators at ARE/EDU. In general, the breathing resistance and work

*of breathing increased with increasing depth and ventilation rate.

2. Approximately fifty per cent of regulators, irrespective op type, showed ararid decrease in performance as the cylinder supply pressure was reduced to 30 Bar.A small degradation in 'erformance during inhalation was achieved by only a fewbalanced first stage regulators at a cylinder pressure of 30 Bar.

3. Only two demand regulators were able to meet the performance limitsproposed by Morrison, and recommended by the SUT at a depth of 50 msw and aventilation rate of 62.51RMV, but there was a greater ability in mpeting theaccentable limits.

References:

1) Standardised unmanned underwater breathinF anparatus testprocedures.

2) Proposed unmanned test procedures and physiological acceptancecriteria.

J B Morrison, J T Florio, A G Thornton and M K Todd.Journal of the Society of Underwater Technology.

Sprinr 1Q2

[ ' .

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ACKNOWYEDGEMENTS

M.y thank-, to Mr A Luboff nnd Mr S Parvin for their persistence in completin;- the

enormous number of repetitive tests, and Dr J Livesey for his assistance in

completinr this report.

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LU CC

w0.0

w

w

o.i

rnr1Cc

,~ I

00

I-L

I 4%

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PRESSURE-VOLUMhE DI AGRM

EXHALE --------

DELTA P

INHALE

DISPLACEMEN2T (LITRE)

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FIGURE 3

2 - - t -- -_-- __ --ic

m~ -u

~~~1 - - Lus__I ___ L1..~~ __

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FIGIJRE 4

'I I F.. ui_ _ _us

- -_ _ - -MN4", oz

U)

U -A

- - - - - t

S - -- -- --- -- - - - -I- L cc

INE

- -- *-4-*0.I--.i

i.7

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FIGURE 5 '.

* IL

40 0)

_0 Ix

Bu

-Ir

0.

V.CD

NoN

-* .. __ 7liil!I

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FIGURE 6

I, *I

Iz 0

.. . . L

-Ii- - __cc

A.o

hi

HR I0 1 ~ -. cc

On___________________

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Lp 30Omsw 50OMSW

0 ISW

4. 0 .I

EFFECT OF DEPTH ON DEMAAND REGULATOR

PERFORL-W\NCE

(2.5L TIDAL VOLUMIE x 25 BPI,/ - (0 BAR SUPPLY) j

lbi

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FIGURE8

P

50 MSW

IRECOMAMENDE D -LIMAIT50VS

ACCEPTABLE LIMIlT

IEFFEICT OF DEPTH O14 DEI!.ANDREGULATOR

PERF ORMANCE

(2.5L T IDAL VOLUME x 2,5 6PM 70 EAR SUPPLY) I

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FIGURE 9

EXAMPLE OF HIGH EXHALE RESISTANCE

62.5

DELTA PkPa

FIGURE 10

EXAMPLE OF HIGH CRACKIN4G PRESSURE AT BFXT.NNING OF INHALATION

DISPLACF)r.E'4T (LITRES)

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FIGURE 11

EXAMPLE (WF POSITIVE PRESSURE OCCURRING DURING INHALATION

DEM.: 50 mew

DELTA P

kPa

D

JI

DISPLACD4I T (LITRES)

JIIL_ - • " - .... _ _ 1 <.....

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10(4

0

At U

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FIGURE 13

EFFEC"-OF REDUCING CYLINDER PRESSURE ON THE PERFORIM]7CEOF A BALANCE FIRST STAGE DEMAND REGULATOR

DEPTH: 5Omew

DELTA PkPa 62.5 1 RKV

Uf

ko~ Bar

100 Bar

300 Bar

DI SPLACEDNT

71.. .....

Page 24: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

EMT OF REUJXING CYLlurER ~~ Z ON THEPEROMANCE OF AN UNBALANCD YlRST STAGE DD-A!:D REGULATOR

DEPTH: 40 mew

62.5 1 RmV

DELTA P in B"jcpa

85 Bar

50 Bar

40 Barr

Page 25: AIY - DTIC · 2014. 9. 27. · ac)-a158 596 perfofimance coupainison of thirty tiiostage deiapo i/i rewulatoas(u3 aduiralty research estadlishment fiarine technolooy) poatsou.. i

TAFLE 1

U0**88*1

ul 0 -~45

0~ 0 %.

v~ 0'64 U

z

0 r

-4 -A

-0 i" 0 0

U4

~I) S

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o iI

TA7rLE 2

ARE EXPERIMENTAL DIVING UNIT

HYPERBARIC TEST AND EVALUATION LABORATORY

CERTIFICATE OF DDEAND REGULATOR PERI)RMANCE

DATE OF TF.ST: . o ED] Ret: f

DEMAND REULATOR MODEL:-

MANUFACTURER/AGENT: -

MODEL TYPE:- SINGLE/TWO STAGE.

FIRST STAGE TYPE:- DIAPHRAGM - PISTON BALANCED/UNBALANCED

RECOMMENDED INTER-STAGE PRESSURE:- . Bar to _ Bar.

FIRST STAGE Ser No:- SECOND STAGE Ser No:-

RESULTS (STANDARD TESTS COMPLETED WITH 70 BAR SUPPLY)

WATER TEMPERATURE % _ Centigrade

MEASURED INTER-STAGE PRESSURE : .Bar

DEPTH RECOMMENDED LIMITS MET FOR 62.5 1 RMV : -- msw (1.75 J/l, + 1.5 kPa)

DEPTH ACCEPTABLE LIMITS MET FOR 62.5 1 RMV : mew (3.00 J/1, + 2.5 kPa)

EFFECT OF CYLINDER PRESSURE MEASURED AT : kamkw a

(A) for 62.5 1 ]MV at 180 Bar . J/l,+ .kPa, . kPa

(B) " " " i o 70 Bar : J/, __ kPa, - kPa

(c) " " " " 30 Bar : _J/1, + . kPa, - . kPa

GE NERAL COMPsENTS

1.0

MAXi11UM RECOMENDED WORKING DEPTH msw

----------------------------------------------------------------------------------------

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~II" 1

Arrex A

Physiolorical performance criteria propoced

by Morrison (1) for underwater breathinp apparatus

(a) Maximum RECOMMENDED LIMITS for (i) Work 0.5 + 0.02 x V J/1

(ii) B/resist + 1.5 kPa

(b) Maximum ACCEPTABLE LIMITS for (i) Work = 0.5 + 0.04 x i J/l

(ii) B/resist + 2.5 kPa

(Ventilation rate V 1/min)

The breathing apparatus is considered to be UNACCEPTABLE for use, if the work of

breathing and breathing resistance exceeded the ACCEPTABLE LIMITS.

pJ

t *

"

ih 7-

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IA'

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