HYDRODYNAMIC INDUCTION BOW FOIL SOBM^τn or aNE 0IL ^^
TECHNICAL FTFT.n
This invention relates to HYDRODYNAMIC INDUCTION HOW F0Ir SUBMERSION PLANE OIL SKIMMERS. More particularly, it relate " improvements in oil skimmers disclosed in United States Paten Nos 3,715,034 and 5.194.164 which are incorporated herein reference. *
O 98/17585
BACKGROUND ART
This invention comprises improvements in the cil skimmers disclosed n United States Patent :!o . 3,715,034, Issued: Feb¬ ruary 6, 1973 to A. I anc f entitled DEVICE FOR REMOVING OIL SLICKS and United States Patent No. 5,194,164, Issued: March 16, 1993 to George ". Adams. According to the above-identified Ivanof patent "oil floating on a body of water is collected bv moving a sh llow-draft water craft, such as a barge, having sternwarcly slanted bcw section and belew -he water l ne ar. ingress opening in or near the bcw section through an oil slick. The slant of the bow section forces o l m ts path downward!-/ thereby causing the o l, possibly intermingled with water, to flow as a flat layer along tne bottom cf the barge. As the oil reaches the ingress opening t is propelled i to a hold of the barge due to the pressure differential between the c tside and the inside of the barge. Oil thus accumulating in a held of the barge may be removed therefrom from time to time and clear water as may also enter the hold is returned to the body of water."
The effectiveness of skimmers, according to the abcve-iden-
.e er surraoe increases. - r.is is cue to tne cow wave craa—ec by the inclined-plane which tends to collect o l in front cf the bow wave and to reduce the velocity cf the o l relative to tne surface cf the incl ed—cl to the ocmt where he o l does r.o — co down t for collection.
I discovered tna«t o-v.< t-css.».+t-ι•.on„ι..ng a transverse bodv anead «* —a Dow, Λater surface ir.r^ ... -_, - . ,, * °- l"ιa-= s c ceicw zne surface o- --. water a surface wave mav •* r--.=,--.-... ~ v""2 _y ^ cheated wmcn is out of chase wi-h -« .«--:.« wave e ted by -B. lacllne≤-pll,s and d.;.r_c_lv^ -.-.«..-..., ...., ... This .oc., can i o „..„„ .,__ -' it at tne forward surface o- -he ,-,~ι, • ,
----- - .he lnclmεc-plane. The sinus lest . .- .--c_e=. ...eae .c^. S ls a cyIl.≤erf _nβ aχιs of wn is genera../ oarallel -- --- , ,-, e "^ -- - -^--l-i- tti ocdv. Tne --c--- i--1<------i-r-..~g bκ~cd-*„v rna / c-=> eκtencec rearwarc.v towarc -_ne v Λ,a α—___. =«u_..-.*.-.-.a,_, o~c~,w„ mter-^ce = -«c may be extended upwardly m wmglets at tne outer edges tne^ The wmglets also e.tenc inwardly to guide oil „ ZΛ t ιnci ed- Plane wnicn would otnerwise be pushed aside oy tne bow wave Tnis improvement wnich I call cnβ nydrcdynamic induction bow -'o- is discloseα m tne accve-identified United States Patent _!o. 5 , 13-. , - = 4.
Such a submersion plane skimmer employing my hydrodynamic induction bow foil is shewn in Figures 1 through 3 and is manu¬ factured by Webster 3arr.es, Inc. of 13*. McKinley Street, Roway- ton, Connecticut 06853.
As shown in Figures 1 through 3, the body of the skimmer 20 is a barge-like shape with an inclined submersion plane 22 at the bow 24. The separation tank 26 in the center of skimmer 20 has two horizontal layers of baffles or separation decks 28,30 and is open to the sea through a perforated bottom 32. At the forward end of the separation tank 26 is a collection basin or hold 28 where a discharge pump 34 is located. The skimmer body 20 is supported on eacn side by pontoons 36,38 which are detachable for transport. As the skimmer 20 advances, oil 40 and surface water 42 are gently deflected downward by the hydrodynamic induction bow foil 44. The mixture descends along the submersion plane 22 to a scoop 46 that directs the oil, and a thin layer of water, into the separation tank 26. As the mixture slews down, the oil floats upward and the water flows downward and cut through the perforated bottom 32. A weak flow at the surface cf the separation tank rr.oves the separated oil forward ever floating weir 43 to the collection basin 23 and discharge pump (net shewn) .
Several problems have been encountered m operating the skimmer 20. The hydrodynamic induction bow foil ideally should remain at a preset distance below the surface to maximize the reduction in the bow wave. However, trim of the skimmer 20 was found tc change, going bow down with increasing collection s s≡ά . The skimmer 20 tends to pitch in rough water. These effects increased turbulence at the inlet scoop S reducing ccilectio efficiency.
Some turbulence was noted starting between the trailing edge cf the foil 44 and the nearest portion of the submersion plane 22 and seme was induced at high collection speeds by the foil -H itself.
Additional turbulence was induced at the inlet 43 between the scoop 46 and the bottom cf the submersion plane 22.
The placement cf a pump over the collection basin 29 was awkward because cf the self-adjusting weir 43. When placed ever
_.
the collection basin 23 or, even worse, en the forward deck 51, the added weight and high center of mass m. reased the ereviouslv
Ideally, the oil slick should move smoothly down the submer¬ sion plane, through the inlet 43, and into the separation tank 26 without ar.v induced turbulence.
DISCLOSURE OF THE INVENTION
I have discovered that greatly improved r. may b :ee aacchhiieevveedd bbvv: on-turbulent 'low transi
tion , viewed from
p-
l J ne'
wh*n substan
tial
in form
ing
the
-.«,, , =C,cp ... fc= substant^aMv coaxial with said convex portion; ' hinging z e aft en •d ou.f ssaaiic- sec~o~o'o so th-- ≤--.-^ ,-,--.-,.; may be =-ιe- bv «5,-.ι ._-,♦. ■ , " opening y selectiveiy positioning said scooo- cambering rhe foil; -<-1--''
be fastened thereto, as - s. aΛed .
OBJECTS OF THE INVENTION
It is therefore an object of the invention to improve in- clinec-piane cil skimmers.
Another object of the invention is to increase the velocity with which such o l skimmers may operate effectively.
A furtner cb;ect cf the invention is to decrease turbulence in the collection cf an cil slick by such skimmers.
More specific o ^ ec s cf the invention are: to decrease turbulence caused by a hydrodynamic inductien bcw foil m such a skimmer; to decrease turbulence caused by the presence cf said bow foil adjacent the inclined plane; to decrease turbulence induced at tne inlet of an oil slick into such skimmer; to decrease turbulence caused by velocity dependent trim effects; and to decrease turbulence caused by wave induced pitching cf such skimmers .
Other objects of the invention will in part be obvious and will i part appear hereinafter.
The invention accordingly comprises the features cf construction, combinations cf elements, and arrangements cf parts nioh '. ll ce exempli ied 1.1 the constructions neremafter set forth.
The scooe cf t e invention will be indicated m tne claims.
O 98/17585
3RIEF DESCRIPTION CF THE DRAWINGS
For a fuller understanding of the nature and objects of the invention, reference snould be had to the following detailed description, taken m connection with the accompanying drawings, in which:
FIGURE 1 is a perspective view of an oil skimmer according to the prior art lasned tc a tender therefore;
FIGURE 2 is a diagrammatic top view cf tne pr cr art skimmer of Figure 1;
FIGURE 3 is a diagrammatic side view cf tne prior art skimmer cf Figure 1 ;
FIGURE 4 is a perspective view of a hydrodynamic induction bow foil submersion plane oil skimmer according to my present invention;
FIGURE 5 is a diagrammatic plan view of the skimmer cf Figure 4 ;
FIGURES 6, 7, and 8 are diagrammatic side views of the skimmer cf Figure 5;
FIGURES 9, 10, and 11 are diagrammatic side views cf tne separation d=cκs and oettom cf tne o l skimmer of Figure 4 ,-
FIGURE 12 is a diagrammatic cross-sectional view, partially cut away, takes along tne line 12-12 of Figure 7;
FIGURE 13 is a diagrammatic side view, partially cut away, cf tne bow of one cf the pontoons of the skimmer cf Figure ;
FIGURE 14 s a cross-sectional view taxen ong tne line 14-14 cf Figure 1 ;
FIGURE 15 is a crcss-≤ecticnal view similar to Figure 14 showing how differing boc connectors may be εfixed tc tne shimmer cf Figure 4; and,
FIGURE 15 is a diagrammatic cross-sect cnal view, part: cut away, showing now the scoop opening may be varied.
The same reference characters refer tc the same ele~ througnout tne several views of the drawings.
BEST MODE FOR CARRYIMP.
0ϋτ TKΞ I;iVg ; .
rΛ.
Now referring
■ to Figure 4, a hydrodynamic induction b suomersion :!s". ow foil s ;..dcimmeerr 5500,, according t isent comprises a pair cf null-lι e- invention,
..< pontoons 52,54 terminating deck- ike portions 56.53. .<?+•< g in upper
30,33. Stern portion 60 may also be a sealed compartment termir.ati.i- portion 62,
The pontoons 52,54 terminate at r.arr; τm„ae _--_-,r-..J^a-r-.„c- buo„w. c s cw Portions 64,66,
.or-tie- _, o.- p.p-o,o-,,nn,t+t.o.o-,oo_nn_ ϊwec b dceecc..--::,s ,505 βarn.cd D5ύ3 aarre; nearL pi.anr.er •«::.-. a oow e* 53 wnich <s s'.,.-!.. , - ._ -
-s s..g».. inclined rrom bcw to art ever an inclined submersion plane 70 (see Figure 6). Attacnme.it means 7"> 74 -r - -, ,
' ' ' ,0' a-n-c 73 are provided for launcnmg ana removing tne skimmer 50 frem tne wate.r .
?he upper separation decx or baffles SO mav oe seen 1 Figure 1. Oil comes up tnrougn the slot-like openings 82 therein during skimming operations. The oil, on top cf any water that may have been collected flows forward over floating weirs 34 and 36 (only cr.e cf whicn is shewn m Figure -) into a small oil coi- lecticn tank or no id 33.
A pump (not s own 1.1 Figure -) may oe located within and aoove t e center cf t e collection tar.Λ for removing tna oil tnεrefro to a work ecat wit.i the s.<ι mer 50 1.1 tew.
An arm 90 s prcviced for adjusting t e scooo (not sncwn 1.1 - --a ' ' '
Now referring to Figures 5, ό, a: ■ , ■.r.- ≤.ιm er rav ce
; " ~ "- - -"" - aDOU- "* u=?er peripnery tnereof.
The pump s4 (as cast seen -1.--> .r_,.,-..„,,.-=- _ z \) 1B enterec in tne c l collection .-.old 33 en chair-like stand £9 (£≤s Figure 3).
-•"•= weirs o, 33 _:e r.inc 'ec- -=-- 935o, oas0 a- ...-.= zz'.i enc e: secarat on dec. ΞC. The' .- a-r-e_ -_r-^.., ι-_:.-. ,w,i,_.π_ r.oataticr. means 103, 132 at their top edges.
The hydred narric induction bow foil 104 is lccated uncer tne inclined submersion cow cla.ie 70. -- , - -_ --*.-,.- - „_,, w_... .ne t-a__ιr.g upper surrace 106 thereof r.earl- carallel to the plane 70.
Plane 70, as seen from the bottom, terιr.1.1— ,- - -^ve portion 108 then a concave portion 110 and tne- a -<a*e zontal portion 112. A plane portion 114 is located between con-
vex portion 103 and concave portion 110.
The o
il collect
ing hold 88 and pump 94 are located ove-
th concave port
ion 103
terminating the immersion plane 70 w
ith the center or mass cf
tne oil and pump being slign
tlv af
t of concave crtio.i 108
igu ■irree SS,, i
i ccaann bbee ssweenn
_o,lane ≤ ≤mmcoth.lv trans
itions from planar to convex (to planar),
to concave and to planar, mime w
ith tne bottom of separa
tion deck 115. The ow
is fur
tner gu
ided by sccop 113 which is hinged to
the bo
ttom l*
0' The scoop 113 may oe adjusted to several posi
tions as d
"~
' cussed below. "°
Frame memoers 122 support tne immersion plane I Q and the eck 63
The forward wall 122 and rear wall 124 of the oil collection hold 88 are shown Figure 7.
I s "S" shaped ootto is generally indicated at 1 6 and structural rios at 123. The corners 130,132 may be seen m Fig- ures 5 and 3
Figures 99,. 11 n0, a-n^d 1i '1 s_h,ew tne upper and. .lows separation decks 80,116 and the bottom 120, respectively. Each is oerfo- rated cy transverse cnanneis indicated at 124 m deck S 0 , i 36 m deck 115, and 1 -2-3- .-.-. ~rc-...,,Γ_Λ _ * -_,:*0. .>..c„te t at t ese vary n size
--<-.. ^r... _n CSCΛ. OO .-.c :lo anc cottcm 120.
F
igure 12
is a partial representative cross-sec
ticn snewmg
tne pon
toon 52
; decks 30,116 and oottom 120. The pon
toon 52 compr
ises a vertical
s-.-cimmer
tc wr.icn are mounted decks 3
V- 0
J,-"-
1
uooer ver
tical wall 142 terminates ---- --
*--se
-.,■-• c-- aoout tne wa
ter line. lower iacc„.^.aa'_. ■
,. = -.ιi i -,^ •
0 - _te.,r,min„a.te-s at ≤
traicn
t oo
ttom section 143.
Varicus cro -s-is.. r..r≤cr.-.'.hλec_-bς I[,-.,-j,-. s-n•_,o„,w._n>) =_.r„e_ ,u,sec- to e"*cπ, """ sη ---> pontoon 52. Pontoon 54 is tne mirror image of pontoon 52."'"
Vertical inner side wall 140 of forward pontoon 54 is ex¬ tended forward at 152 m front of skimmer 50 (see Figures 13-15 and 6). Diagonal side wall 154 is welded to wall 140 as sncwn.
Extended portion 152 has holes 155 ther-i -or ^ Λ - . bolts 156 for affixmc d< '** * „ • -aceiving
- c-β-ing coom connecters 153 aid isn tneretc when booms a--» _-ac?3ιi-o,y,e.dj as shown Figure 1. i50
- = -_r.ι.._ _o .-igure 16, sccoo 113 is hinc=d *-- •-,
120 at -ce 15~ ^,..-..; '-J-ig-α _.„ ccttom
..-..g« lo-. Λ.j a.iag arm 90 is llL„ sh r»ta ^ about oivot 154 τιf< ι S ;. . *vl-ates
--1-. -o3 m arm 9, ceoperate with holes 170 and a removable bolt
(not sncwn, to allow positioning scoop 113 in cne of a „„„_., '] positions as rac *uired bv- --'•i•se r π"-=*t-,u,r-e^ cr- f "* collection. —^ cc- i- sc?1i-iil a=.-c,: s-oeed of
One of several c-=~*--s uV(-ι,^,. e.<cluslo.ι cars 163 can also be seen in
: lσu
I have tested a camoered ^oii : -i t , α -oli iD wnicn was a NACA 5517 =>nd it reduced turbulence due to th«» f-ii , o tne rυii itsel: significantly over my uncambered orior a-- 01 D1,
-.oils. Placing the trailing surface of tne roil substantia -l-l-y t-arrseiJ.!lβeii *t.,o-, tne immersion plane 70, re- ducec turbulence induced -=lloonncg tnn.e. pιlane -/„0 c-ue to the orr=esence or the foil 104. However, : believe
'e a thinner cambered foil such as NACA 5512 would furth;
»er reduce turbulence due to the foil itself. NACA 5617 has a thick: ess to cord ratio cf 17% while
5≤£ "D cord ---- cf 12%. sct.i of t ese -°- -
2 ~ave tneir
. *oomt o-
c„a-..,e•„er cenmd the cen
ter of
*"'"Cs 5e"^ t vιty to angle of attack.
. t j . cambered foil, properly contieureα, has strong advantages over the uncambered lifting surface. Among othe things- • At the same lift coefficients, it results in more gradual stall (that s, it shifts the stall rearward) during severe attack angle variations resulting from pitching of the entire unit o uri f irioumiii i ww naavvveeuss.. β
At the same lift coefficients and thickness ratios, it allows the leading edge of the foil to be lower relative to the water surface, thus intersecting a larger vertical portion of the incoming flow stream.
A . t
Λ the same li .s ,t coefficien
Λts it allow , s t
ιh
ne
e fa
I0i
Ul t
tr
o» κ«
e
whi-ch L. red Juces th ■ e f
*•orward buoyancy problem, and reduces turbulence
It allows the lift distribution, and hence the resulting water surface, to be more " r 10 , requirements-for example, to cause a smooth transition locally at the waterhne intersection with the inclined plane, avoiding local mixing of the oil and water. σ "
It allows the trailing edge of the foil to be better geometrically aligned with the inclined plane while preservmg the low attack angle of the foil at the leading edge
It allows the foil to more closely conform to the prevailing flow field, reducing the necessity for abrupt flow transitions particularly at the trailing region be most effecuve m these applications, the camber should be unusually large and the ation ofthe camber should be unusually far aft. *»" "»=
z4&t~Α-l5L e£≠+ , ~ £i-fέJ øL&rø _ ,_
__^^^- ii^4^^t-
Each cf the above described features add to the efficiency and speed of collection. Ai but t.-.a multiple boom connectors comparatively decrease tne turbulence cf tne flow cf cil and water into tne s.iimmar to minimize r. xir.g cf o l and water and allowing t e cil siicx tc flow smootn y ir.der tr.2 middle collec
More speci ically , the taper cf t.-.= pontoons c≤lcv the wate line reduces pitching and variation n tr m cue tc speed. Placement cf the cil collection held a d pump over tne inlet and low dcv/n also reduces pitching and tr m variation due to speed. Use of a rear cambered foil (one with the maximum camsar cehir.d the mid point of the ccrd) allows fine adjustment of the angle cf attack of the foil to minimize turbulence and greatly decreases turbulence caused by an le of attack variation ue tc pitching or skimmer trim variation. The smoothly varying terminating portion cf immersion plane beginning below the bottom of lowest separation deck, initially convex, than concave, then piar.ar with the bottom cf the lowest .separation deck and t.-.a coaxial snape of the scoop all direct t a flew of the slick under t.-.a lowest separatio deck w th minimum turoulence. Having the near surface of the foil substantially parallel to the immersion plane minimizes the turbulence due to the interaction between the foil and the immersion plane. The adjustable scoop opening allows the amount of water taken nto the skimmer to be minimized.