HOV.A2T
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ThE ThYLUC OF Th HOYCRAPT O
IP DIGM
OF THE itn.E
A LXTJR T
Bi PR.3ZNTE) TN aOTI'DA?
Y 16.
C.LIST OF SLIDE
Fie. I esistanco of typical ditplacenent craft. i&. 2 Speed and draG
Fi.
3 Speed/weijht envelope of civil craft operating over water (without Hovercraft)L K C T U R S N 0.: 12,
HOVEACRAYT LZCTUREIt is now reoogoised that the greatest application for
Hovaroreft in the oonercial field te in the roh
of a high speed
boat or ship carrying passengers or low density sargo.
Thsre are, of coures, aa
applications over land, but thee
generally depend on the typs of terrain and in under davslop.d areas
are considered in the light of existing facilities,
If one considers developnent in the transport field over. tbs
last oentuxy
the motor oar has increased in speed frez about 10 edles
an hour to 130 m.p.h.
The first passenger tram had a speed of about 10 miles
on hour
and today one can travel by rail at about 100 miles per hour.
The tiret passenger aircraft had a epsed of eoee 60 m.p.h. and
today it is iuite comonplace to travel by air at epeets of about
600 m.p.h.
These three modes of travel have each improved in speed by sees
tenfold.
Although passenger carrying ships have al so increased in speed,
the fastest liner today travels at only
35 knots und it appears that
farther improvemete are not poesibhi, and
a barrier to increased epàsI
cxi etc at around about 30 knot e.
There is a very ftzndaziental
reason for this M this is the
hich water drag for dipiaeement vessels.
IDENQ. i.
-2-The first slide shows very sicply the relationship between
the resistance of a typical displaceient vessel and its forward
speed.
The lower curvi thaws the wave resistance due
to the
prea?ures exerted unoa the water surtac.; this we see is negligibi.
at low speed, but increases very rapid].y with thoreau
in speed.
The difference between the two curves is skin resistance, which to
the first order is :'roportional to the
squars of the speed.
The
figure illustrates where cargo ahipc operate for
onz lisuecunc
and
how far up the rerj.qtanca curve the Atl&ntie
liner operates, athough
it obta1n
a very
fnererent in speed.
This then was the rroblen of a few years back - how can this
meres-o of renpt9nce vrth reed be overcorne
to ezabl, craft to
operate at high
eed
eccnciieaiiy en the water 'urface?
By
:loytn
the Hovercraft -rinciple, the skin friction
is
virtually &t1:inated, by st%ftaining
a cuhicn of air beneath the craft.
In tercis of the previous
11de, the increase of resistance with
sneed t' reduced to e very et'ì fraction
of that of th dizniaoemcnt
craft. In fact the Fvercreft toes further
thc.n this; becauss of the
air cushion the water pressure acting on the craft iS independent of
speed.
Por the same Prcpu.siye
rower the speed can be increased by a
factor of 4, as shown in the cttagrexn and Vie only liIsitatiQfl is the
aerodynaz,ic drag.
(SLIDEO. 2).
Lot us r.oiider vey briefly
the case for a new tye of veMole
frofl the
oorat1oni roint
f view.
To ¡irìke a cose for a new vehici.
we ut a'c the -uestion "are
existine vehcies enrabie of carrying
out
atifactoriy rl the trs»ort work
required.
(SLIDE NO.
3).
-3-This next slide shows the
weight
versus speed envelope forexistinj; cosercal viclea wl4oh operate over water. In the top
left-hand -ide there are reitively low speed ships whose weight can be as nuch as lOC,OOC tons. In the bottom right-hand aids there ars the aircraft, both fixed ìr.d rotar' wing, which have a weight lizdtation
of little nere than lOO tons. The present trend of aircraft develoent indicate that they wilt, in th, next decade or so, fill the dotted
area.
Between the two :-iajor types of vehicle there are a few
srecialised craft, which pernte in cparatively ssaU mwbcra.
These are the hydrofoil artd hydroplaning craft. At the present t1 thaca
two
foras of vehicle do not neki a significantcontrtbutjoa to oercia. transport arid, tren the diagrszzi, we can see that the real choice lies between the ship, which carries a large payload at a low speed, and the aireroft, which carries a snail load at high speed.
In
this central area the case te ubsitted that a Hovercraft operating at interacdiate speeds earrying payloads of internedjatsize will fill this very significant gap in the overeater transport eyatea.
There are seveal nethods f sustaining
an
air cushion, each p,.thod having its own tartiaular applicstton.
.IDE NO. 4. shows the three nethods.
Air Bearing:
This eiplyu Vicus effects arid needs relatively flat surfaces
with a very a11 clearer.ce.
A high pres'ure euply is used to produca
a cushfo
hetween
the rad andIts
bearing surface,it is only of use
with
tr2ri.-ort ystsrs e'ioyirg rails or flattrack..
(The Por4LevansA ute' this idea for a railway 'ystem).
Plenw Qiber:
Air lea&
arounA tnt- jerihori with tht
fern.
Th
tota
prezauzrioe th the fon aot
onthe underside
of the
lenu ch.aabert
lift the craft until eiltriun ta
tablihed. The
power reured doenda on the 1eake rate of thern
air aLld
grtdr clearancestre re4uired than
with theLevapad, so
that a pLiun ohanber craft will rile oez-
oLtd o'ostaclea.
This
nethd i
auitable for low speeds over rough ground,
Staple Curtain:
This is the Hovercraft concept
a reri.heral curtain of air.
The jet ini;ialli r,rocluceo a positive
rea rwe ua1er the crft,
hi.h
then dcfleeta th.
eùrtan outwrta to
a seal for the cushion air.
Atre'eit
'ono 4O
.ess rower i
rei.irtd to btin the aae ground
eleors'ce, or hoverheiht, than a rienun chanber craft.
That 1oes this
cushionof air do for the craft? It provides th. greater
speed oaability. It makes a con'iderable contribution to the
behaviour in ru&a seas in reducind the re»orse of the craft in
pitch
ari heave,
provi'es
asseners 'th n ¡roze corf,rtnb1e ride.
It also provides a truly anrhibious craft and dispenses
with the
need for docks or berthing facilities.
There is, of course, a price to pay for all this and
this is
in the power required to lift it aboye the surface.
And the next
løvoì:pai.:t should be concentrated
onreducing the power required,
Several proposals for this are xentioned in
the
nextpart of the
lectw.,Pow the stage has been reached v.here the
various annufaeturere
are either ready,
r soon wi be in a poattion, to offer custoners
nell aud ;diun sized craft at least for cv: ution and route rroving.
L the aae te, de1IA.r
'are wcrkth
n
che. ea for considersb]y
larger and oore so-hi.ticated craft for
;'rtder range of
operations.¡iv on the pzib1eaa coneit cf refining the original
ooacot to .iuet the vAriou5 seds, size. and
oAtiguztions and
pyzioai oparationa]. coditiuna iii.eiy to b. posed by potential
ou s t ers, vho
ill wait aoun
and ec ìn.i. orbit.
jwITh
Oi?t sIr4
CE 2 hRESISTANCE
OTYPICAL DISPLACEMENÍ CRAFT
o O 0 I 2 F' I I Fi ) i
il iii
VICIfRsAnM5tRo,dG5 ARCRAPt) LTD. SOU!H MARSTON WORK
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SPEED WEIGHT
ENVELO
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CIVIL CRAFI OPERATING OVER WATER
r I I) O laC) LIO li):) 00 a
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SIMPLE AIR BEARING
SINGLI ANNULAR JET
HOVERCRAFTALTERNATIVE AIR
CUSHIONS
L-PLENUM CHAMBER
A
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VIc&8..SThO11GS (ANGxN3) u'z
VAPT
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12 (B)
(B)
¡ziicwi
01 flOYFCRAPTCD(EThG
A LSCJR TO
BÌ PRESI*IThDfl
BODAM BY UR. (. C. K
Lect. 12.
LIZ? OF corrm
i
DE3Inmoso
2.
MEcHANICAL DIG
laI#t
Lyout
Strsogth
Water Impact
.3.PESfT
Arr
-1 i
V. A. -i
V.A. .2
V. A.-3
4.
FUflBK AFT
De1oped Air Curtains
Ict. 12 (B)
LIST OP SLD
Pt. I Wet,jht analysis
i6. 2
Suctaze d1aon
Ptg. 3 Source of resistance to tioa
Pig. 4 Water inpect loading cases without rotaon
P*.g,. 5 Wat.r tect loading caece wi rotetion
71g. 6 Sl-II ovar oater Pig. 7 V.L.-1 water trials
Pig. 8
V. A. -2 traaspartioa 000nta
Pig. 9
Y. e -3 geteyal -angecentPig.IO
Driver's controls Y.&.3
71g.11
Coaponenta V.A.-,
Ptg.I2
Y.A.-3 cobb 1aloe
Pig.
13Spss of
øov.r..tt aircurtains
Plg.14 Actuation
of
flazible øoverottecture 12
IGII
nosoI1a
The first question - what is a hovercraft? ¿t i.
essest.
i.Uy s ourf.oe vehicle lassonch that it relus upon thefus
ionedistclj bassath it for it. support. The hovercraft is unique "iig.t surface vehicles however, top la its basto esafigurstion at liest, it doss ont cons is ooat.et with the suface ovu which it operates.There ore s usher cf problema associatedwith craft et
th
rps, pu'tioul.ply ibas opusted ovei water, and it has been considered dosirabi. to¿saLgo
and asaotue a onli
craft, for their investigation.ofinj5g Hovercraft groud-olsasano, performance ther is a direct interchange betessu all-up
wsight
and haves-height ovar s rangs of values. An st.logous imitation toon
aircraft does apply la the abili, or otherwise,
of
the Haver-craft to olear wavsa of s given height3 operation in partial contact with water gives an increased fuel oonsunpticn and s reduced radius of operation.Thus, is the dov.lojinsnt of these craft, control
of
weight bas been carefully considered, balanced 'g-4-t the desire for, los proction coats Tb. structure has bess
considered on s mii Leva weight basis cospatibló with the
usi of ectabi 1'hod sauf acturing facilities
There material sises bave bees datarained r the strength required, airsr,ft
stressing
practise has been said.Xn the ¿saLgo and manufacture stage certain practices have been
adoptedu-The quaii' of estensi. processes, and workmanship,
havi been maintained to a
at.ndasd
determined ' thenatur, of th. structure - whether pnimax, or second.a... and the atrsa level the
atructue is
szpeet.d te support.
Corrosion protection la provided either by the
choice of compatible esterials, ky the use
of
In the absenos at recognised acceptance standards, the deai materiale and components used in the hovercraft have been specified Vickers-Armstzongs (gineers) Limit.d,
baa ed upon mom- years experience of sireraf t strengthand
safety rquiremcnta, suitablj modified and having dus rsgezd to the iàtrinsio safety of the hovercraft.
A great deal of dvenae scheming has been done at Vickers-Arustronga (gineera) Limited, on hovercraft eap.ble of opeieting over open seas For the type of seas likely to be encountered on unprotected waters hóvercref t
sizes from 100 to 1,000 tons should be considered. Such siseo are dictated r two teeters.
Firat].y tar open water operation .1.1 tough the year,
the wave coditions require longer craft, with greater hover height. This io to keep the struotcral loads and power requirements to reasonable values. The second factor,
which erives rrcm the relationship of cushion area to perimeter, leads to improved econoi' et operation in terms of ton miles per borse power installed. This la due to the relative saving in power and the greater disposable load
n the larger craft. Thus the larger ranges requiÑd for open sea journeys become economie in terms of fuel to payload
rat io.
The structure of a hovercraft is largely dictated LG' the
impact boda In the first designs, adequate clearance was
provided ty hoving higher powered lift systems, since the structural penalties in designing for greater impact are prohibitive.
In general the development work being carried out on
hovercraft is c,imed primarily at two things:-(a) reduction in capital cost of the craft
(bj reduction in ins tailed power and fuel oonaumpt ion
In the f itt problen, an attempt is being made to get away from expensive aircraft methods of construction, which were and are currently cieing used in order to achieve a
New asterial. are being considered end in particular the use of tetis-tabu etrasterie is receiving attention.
On the question of installed power there
is
a traaendoa coop. for novel ideas Theniiti1.i
3St p. of curtejo aequiros less litt power and ease flow than th. plonu. obsaber typ. of cushion, yet the power requirexaast. suggest that thistype of craft vili not bay, general application, but will be restricted to ap.oi.lia.d fields, transportation. What anat be borne ta atad however is that the curtain doca no wort and nature bu cot no liait on the reduction in power that night b. sohieved.
Lec
i2
1*'QIMIci1L DESIGN
The toro 'Usvercrat' was that giver by Coakerall to his
invention of te sn...&1nr jot
ahoin thsae firee oad
develop-miata at it.
M-tfect nachin', a tore iod piøularly
by the AiMna, inoledea all 4r cushion croft.
'The none
liovszsft' baa ace b.e
adopted se the Registered Trade.
f or H1L aed
ir aasoQte5.
Sisas te pocer reçti:ì i: 1re1y ajnicnt on tbe Uft
?rovi(1.ed cad honco o
tio tottJ. ;;i;ht of the craft, it foUo
that the ratio ei:
j10
to totoi (
2-"-7o!.t)
e a oaee
of eftiotsuo
ua rfecto tho cgt of opraticr aíì1ficantly.
flamee centcl cr
i ceratuUy assessed aM balanced ainat
the doirq roe le.. pct..oi cots.
At the pto.ct ote, eod layct.t, cozotuliy iolecteil aM
oate'icod opÛ.3tioa
r
.tronenta, s, the choice at the
correct pOvez'/weht ratioo
u.n oI..l resuit in I...r-e wei1it aaviDßs.
Thess foatorsa aLU not cost enytMn sad vili te fact redues
the first cost or the cre? t. Th' can, !oov.r, only be eoath»ellsd
la the epeciftonUoc tant initial pro..ct staee, sthlto
to date
ioate that L'1b. I is s typical wctht bresdin.
Ltycii' i
Fis. 2
ivoa 1taarrat1r
vicos of a ty:1cai Hovororm2t
lauont.
The 1er d.tau.'
phasisoa t:o
eaentiai foab.zres at
tJ
ßovercrqjt, viz, a ztatic air cua.zion boncath
o oratt o?
prosawe higher ')wa to:"r!.c ml !al
fr
zrtr5n which tices
Pror the orart to Je Ot
« it1
otiic cruft's
yeriphery.
Thu ai cTtfl ?.ttfl..' t
prcsu'o and
seals It Iroin tLí.
tcrr, h
t
.whiei
pro-vidse most of
tìia
r!vt 1if. Ia tLt. çft ti.. air £,r the
ctains is t&cn ints t
craft tzow
intaloas iii the upper
stu1ee, enert.i by
of tan oentrjfuai f tai au ducted
ctt to the edre et' thu craft.
The farl3 are driven b;' pceer uidts
a oua.d buoyamey taz
. o:c't to .bat
OuIituL WA neoaas%ry.
In the upper diagran, superitructure and control surfaces
arc addsdj the latter are for steering the craft and waking it stable. An aireczew provides propulsion force. The crow arc aoo'o4.t.d
la
the treat of thecroft sed
the poyload, which nay be ¡*ss.ng.r. erfreit, te
carriedta
the centro.Poer:
e p
.c.a o? 71-.3 is
tu
tiiu?tr..te tivrtou 'urcc
et ronirtco to the motic.n .f Hove'uzaf t. For i croft operating ovar t hard aurfce there are three ounIronte of re2lstance on drag aM s fourth cowponnt eben
oieratin
aver yielding ,urfs000 cueb se vetar.The ne radynanic 'rof11e drrj' te te rcsietucs incurred by any
body aviu tuh air ani'. trkes the fz
f ¡.rrue
tcrtt
surface
end rhearii
force
u, t:
fz4et1i.. The 's tiLe dr.' irsaooieted 'ith the uses of tr túen tnti the ertt to the air
curtains. Tb. air is speeded up tre rest to the speed of the crcf%
bsfors o3seted with subetoatially equal velocity
la
all direction.. This speeding up of the air baa a dreg force reactionca
the intabas.The cuahios drag is due tu resisting the novenent of thi cushion tbrcu the *i,, As far as the free stroan is concerned, it resistu nation of the air cu!hion i. it would a solid body.
The catar drag is associated with wave-caking
and
cones about due to slops of the water beneath the craft. It is easy te see how a resi.tanco io exerted on the aircushion by the
water because the torse nore'. t th' surfac. has a renrward couponciit, but It is ot snay ta se.how the
water drod
nd the urtte drse; transaitt,j
to the croft.In
effect
both
1 1.he. Lrug cor'nnntstru to ioke
t!t. er*ft twe rore-upatt.itnde
n,1 then th
craft ha..
dreg, for the
resutiunof the air
eusijiun
iadsr.iafr,oe
th!1.rt
jTíijfl4
'..gis.wL.rù:'.If
heat.ttue of the oì.aift,t
I'.e:.t hrtaa.nta'. h .n :. :'"riate oontr].movenent then th penalty i' neyed in a different way. In thi, cose cene
of the
front curtain flows to the rear of the craft - it is netthan
naking s/iubstantial
subqVntiol contributios to llStinj the enti sad is sttostiv.]
a
loas of power or s z,dussd hover h.it. Not. that the Hovsa'onaft sia
be tilt.d, io
helicopterfashion, to obtain s toros la 007 direstia* st
the
pricest redooed hover heidt.
e cue- co.i4ered
vs bees fron 4r.nft nstiss a
fors the
bsis r r
i.sftu4 :r wiUah
vil Heverassit, Vr sisisfl
t2;s.aont tio o.itt ie
000ai44z'sd1* a maker of ropre..nt.tivs
ccd ¿o s
ibriia ador
aìppll4loada aM roa.tivs
Tity gid inertia lo&4s.
The
zssl usccelo-t. op.rstia
soaditiam.pro,1d
bsals ;
eijJ.ii
ani .toseiig to the onr
liait at 5h. ostentai.
It L envi,e,d t.at
io .v:zss Gporatla4, oesiittas. s vuai.5 wateriMbet*.'1tl. v;purts ractivs fczcat aLU osor.
Is tos
ooahisi-borne eM1ticn this 3atsi st torsos
3. sddttiv, to the stam
satt sir
ani
tj lcade.
The; cisbbami bid. an 4a
to saver s.srnq
conditie tus to
'gta
or oo.tni tailors, etac
it I. stotlati.sllj
laprobabt. that adveras vater
sanditica.and
g1or isatrol tai1oz
sou1 sri,
It
s awl presti.. to dsi
to lou.r
faster. la eaergen sonditiona.
The proof and ultiost. tasto,. assisi
lap
that all a.trtsl used for strsss.d parts is to s rscopd..d 5tal4.4
apsei(icst ice,
Lu confbr.ity with sJronstt pne.tis., the
sass. for
trengtb sr tesesent are ba&ed, u1.s.
othsnwi.
stated,
ea lindi oonditiossi.e. eritin
ihich a's ¿sonad to bs et weh ssv.nit
that thq sosar
bot -c.roir.
The ehc,ie cf such critions.uat nssisaarUjr be sonswbst
arbi t rtr3- at thia ttee et Hceercrart expirions. and celt lapa7 sposi
aftd,/or
irat,r rount st lixitetis it theb.hejou. t the matt abos, this
to b. iesc:cax.
The footers provided
on 'lisiS' condition.are:- Prost fasto,
10,
An ultinate factor of1.5 is used in all saies zs.pt
crash eases.
Lest. 12,
Loodin: n's f n
tn
,vhibioup
Hoverorafti Water and around inrcct.Ccllieion asid *aerpen Ittohing. Beftohing, 3aakl.ng and eltning.
Towing and mooring.
Leoni and general
waterru
rures on the hull plating.Control ey.t.. loada.
Tb. sore inportant of the aboye ass now dieeueed ii
detail.
Vtcr t.-set:
The following id.&iis.d water iss»aet conditions ars
considered to
cover
.11 sasse of watr in,a.t. Thessconditions will arias fron the relative vertisal and horisantal
velocities between the craft arid tne water wñea slighting it
high speed,
or incountering waves in adveres oenditjona.Cases without rotation:
Casi 1: A water fores of twic. tb. weight of
the craft is
applied to a
local area verti.allybelow the C.G., toCether with cerresroodia inertia
retetion-. flise are eoobined with a steady curbion
lift ha
flclflt'
thew,lrht
of the nrnft. The totalunfactor.d inertia force on each nasa le thus thr,.
tines it. weight. This case gives rise tu lortgitud.tnal
ens! tr'taver,e 'Pojri
berdiflE.
Cas. 2; Two 'rater forces, togeter oqúvl
ti twio.
the weight cf the craft, ars
ap'-lied
to local areas,one at the bow curtain and the other et the et.rn
curtain, togetner with correa)on(ling inertia reactions.
This case gives rise t, lcr.tudt.
'agin' bending.
Cc.. 3g Tw water force,, together equal te twice th.
weight of the
craft, xe arpli.d to beniareas,
one attea bow cn! the other at the stern curtains, and inclined to the vertical, up and aft, togetherwith corresponding 5nertia
reactions.
These are combined
with the eteadyvertical
ciashion lift balancing th. weicht. Ø depese is the in&titjopi of the streight lie. oinjn, the bow impact
noi.itjon with the C.(. to the vertical tbrou th. C.c.
Caes 1z Two water forces, together eaual to twice th.
weight of th. craft are applied along the id.walla.
Case 5 Two water
foro., are inclined
to the vertical upand aidewcys, to.etber with corresponding in.rtig raaotlonna. These are
oombtne,d with the
stekdy cuckiv* lift balcaetá.g thecoi ht. This caes
4vee ris.
o
atte amd vertical bede osthe eacees. dsp... is the tncl.tnatton of the straight
line j4ning the sidewall impact oaltio with the C.G,
relative te tEL. vertical,
Cases with rotation of the craft:
Case li A ver-tisai water
tier-ca iii
uçplied to theforward curtain iet such maitud.
as to g.ivs a vertical
&cceberatje or
8 g tediat.1y above the fores. The reacti,. verticalforo, on
a mass imnediat.iy abovethe
force ja eight tines its weight, and elsewhere the veztjsa_1
reactive force cay be obt-iaed.
A.ditionl tore ar4 aft torees on th ..arse: n'y a;iee e to Uz Lortzcnta:
conpoient
cf
tk rotation&]. ixaortia.The above leeds er. combined with steady cushion litt balancing the weight of the craft.
Case 2 A? for Cas, i ece.t that the
inpi.ot
force is tp!iod te the reer curtain,Cace 5; A vertical .iter- Çoioe
i
a.tljed
crito
a.Lgs1 the furoei4
aft contrs-ljne of thecraft,
bett,
thaforward ai4
roer cuz-tgjn,Caee J: A vertice,' 1irce
ir
r:!f.cd along one cde
of .uoh as to ivo a v.rtjoal aoceleratjos
f 4
d1.toy above tb 'crce. The izspi.ot toro. a4resetlone are
bined
itb
cushion litt ¿nd weight.C iin :'
aeren
ditohtn:Ia tIse event of the craft hitting qusya, Jetties, or
obstacisa at the aes wbie t b,ih speed, or, slt.rmstivily, ersih is the shore, the aafctj of the pa.aenr. sad orsw is of ;rtse isportence. Tb, d.ei of the sects sad equipuast support etrgeture within th. o.bi is each tI*t the resulting
bi aceelerftionS in different treetione 5$)' be witbatsed. rs sc!Mtio,
psrticulsr
attentios baa bees paid to the supS ofheavy na,se, erteraal tv t, cabio, -rhieb
sight cause isjuzp itthey break boa, in a crash 1&4g. The inertia terses in teisa antilat, eeoelorstio ore
z-+
!uir
tu
¿t':
':' ! ;
i:i,.Li :'."ñtt '
Lt. i
12? cflJLFr
T firrt rtou. L r In ::it. ii
1je
F5B,
jut fj:.tr c1 .;hen C.zriIere-R3. ori o.i;iijo:ie4 y .he
tlstioi.1 Zc arci Duvel1.. :t Cr:jr..Lfl
tc
d.-tn ¿v aLLnufctuz.sa eoii-vt'i raiinod Hov3ror ft. Th or:ft i;e.red in lun, 1959
eni. as t,iutai the S-l. 6
;h,;-.
tc
uwtsr
t slu f Tt,ht. Ti:.- i aecs:.. It t;erforae&
orieb1y
.i ofu1 'asearch ve1cle.Psrhse it iu .ohiey,we,i
w.. t,
rijì
of the ehi.nn..ì frCalais to Dover.
Thi: v-1 t. ?s 'ei.
-1f.3
-i.
57.e'11
i:lt first
c;er.sta! fcr rs.'qrch r' :.'
T': lt
te
-l. waft
&! it bees. 25 ft. AL 'vis I.,o.ide Lelieoçter ins dsiiviing
435 i..i. rOtd.s litt. At it .riral wet;bt of 7,500 lb. it achl.vs4
o c kotr. and a hover
cf 3i"n. T. wsght ha. been ¿cubiM
with odifietjø nd !ts hover hplht has b.en rodue.d
to about 1
It now he
rtst1
'.le; Vlre- e-.Jne f.,r rrc-iul.j3n and hasachived
-&out 70 'oiot, over water.
rtef rvt.w of Viok.rs ara%; V,A,-1. R.seareM Vnicl.:
Now with trr; yeaz-
opartic,n
a.1iady behind it, thisseau ver.irile (Pig.
7)
t. con tict4 of wood endfibrejla..
sn ) ri,tol SUdney
psy Major engin 4riviag two oentrifupi. tans
t1 provide lift. The propulejo unit i.
a
35
h.p. 1ru
en,ine hirivin a f ixed-'itøh tw.-b1ad. airaorew.0pereti; _th "atiepi. autin*
*.ikt of .,3C0 lb. a.&&
a how-p. "ei-ht of 4 ins., en xte!pjya
ro're of test.
was ooepl.t.g.
Iveptl,.tj eover.dcontrol and etability
probiere end drag LsIsureerate and j.rvid.4 sea. insigbt
La.t. 12,
the prob1.. of Hvu.r ft
000trol
over laM ia siaM
epasci. Over outer a Iyet.a of rprr defl.otica
.s
üVal.psl. 0p.ratio La t h. radia
of
Map apeM rk's4
sa pr.4istM loatability; tbt. e ovsrqous v
zat of the bm.
Lateas mdiLiaatign. to the s
I5hioa
azoabetter litt ai1GsataUoa. ithaut di.stubiij the litt
plipui.- iaatallstioa, the herir height via laersaaM
to3 io..
at the w.igbt 4' 4,600 lb. t Cotivi3ta.1 agI of 130 b.j. va. fittsl t., prupsld.a.
Aoe&.ezstioa tbra,k the p z.gio vta laprorel eM apsel. t 35 t. 40
t. wars
rosolai. Ths vehiel. is cow fittil with fleu4.hi bv_
sai
par.t.a st a w.it of 5,750 lb.V,&..2, Hsvearatti
tI. logisal ousess. to V..-i., it La
4'
tl't1ias ais. aM plaifaxs (vi1, 8) but baastzustcr, to jv. o hiM st v'iejçbt ratio.
Th. V..-2., whiab ta currently &ìgogo4
orar lna4 talais
is a
5-ciat voIlais
of
about 3 tone 1O.4a1 w.lkt.,It ertdosa at 40 kaotz, 6 Loabas oboy. th. suifs, aM i.. poversi
Coatincita. pistoo eng1uius - two fu' litt aM oca for propulai
which a total of about .5O h.p.
Tb. coat iat.resttj tssturs of the V.À.-2. is that it can b. trtnipertM by ajj'eavf% aM is iotsnl.t for
operstina tkreujbt the veriL, ?: transçort purpc.as, t1 si&e f the croft uro
rosovabis soi tha
bo
orna b. z-&Luocd to aiy 8 ft.Tb. craft is iit.oiai ¡rivarU.y for osontz'tj
work, but it oou1
?°e
a u!efu1 personnel traneL'ort
riblais over abuterai water, It h*r tve rstxuotebli
v:h.eli which ¡vi lt eziol1o$ over]oni
coaeourrsbility.
V.!, -3, HQvsrcratt:
This i the Vio av .trQne (V,A.-3. 9) ihiqb arrlad p.eoasr! betxeen 7a11rieey and EI'1 this urer. It
sarrtei 24
aar1era1 weihz 12 t9
at 60 ote aniis
4k(gjs
to hover with it. nain boij about12 lanhea .bov. the
urfPö.
Pour
Bristol Side1q Turinan
taz'bios"g4"ea5 tas
f' Ïitt azd tie fOr
rou1aton, prc'wiis the pasz.'ft. dis of
the 'eft ebos
as bi on the
iainjs41.
that eoul4 op.ratawith rsa:ouabl. opaxttona1 effieieç. The nain urp..e of the
sraft was to
ovUe U3stnl infirsatios on epsrsltuj sapabilitisi
tsr use on lnrr .rsft, but it in b.inj dsvolap.I fats
s
IV51lk
wihisli fa its sin riht.
!.*,.i. Paaasnsr Perri:
Tb. prlàdpls
sryiag the iosiga
eisstrijet ton
bIss issit with aM eons ft
south. of oprsttes
hey.m
s1ete
In the ffxgt trials cf en .C.V,
as
ith s
Vokicls
hoaspetsutialitisa ax' sot f011y
oon, priority znact b. ivon to
qua3itative tsrtin.,
iviw as wy !ruuninS houra
a ;oaiibl
earljr in the life of t.e 'ehislo to onb1s the 4riv.r-t.
obt,i.a bandita1
saperienwi, aM te ieteet any sajsr unrs istthaut delay. Quantitetiwsasasnlsaent. airs sai. on V.A..-3,, but air. not allowi t. diley
the
pr.ee. of the
t.eit. 8ubeert1y, the
ehids has opirotsion a
trial seisercial rout ivin s noheauld pas rsngeri.carry1sg serviesover n 19 efe route ii sea contjtjo
near the 1it. et the vehie1spotentiel.
Ai eses out of conf.zt was taksa frs.
psassax' sents.
This su'vq oovers*t operation when eMir
tut, incluting ditsbis
taiog, and wave inpast,
Tb. general
aungex' rsation to the rUs
aleo compared to other paeeensr-oixryisg Isbiol..; scat of the
psassar. tosod the ails. the 'scoi' a, s traiw sai 'bstt.
t
s ¿asbl*4sak bas, bat opinica was ¿iwidsL ca whathsx the rids ass.
tbè 'ais. a's esa. Is.
l'4''
aaa33rats St paaaissr
is.at1ca'h,. fris the
1 t.
asziis, ace' 3.000 replIes
hey. bis* .t44 caverai 10 trips
er 16 iiar..
ta tú. survq
fammi the jouzs
aaooth 4
ssc.ptabls sei l
ecacafbatabis,
Ths V.i..3. is ais st Sast
astca sei baTh,. isrriag ist
a
als.nied sp.zstil. tasis it is t. bi solitSad t.
dv. lt s
assh - -
i.sas ibais is Pg. 10.
All soatrols ars dsel4 ti aplaste la their astersi usos,
s.s. ]att aillai tuia the sasSi ta pert. Whew the .i.ft is
he'si.a stattisU, it is f
to b. very .uss.ptabl. ta ulM
sasreat., sei lt ever 1, t. grsdista.
The controls saw ¿4.al
t. SSistS2It the$S.iftiSita u
pggjja bat lIròMr.i
causa of
heats, it ii .nsssesu' to head
the sraft ints ojal sei
asisteis posits with tbias,l
thz'gat.
Wha5 the lift heleas sue roiaet fas
speed increases;
the enti biiao t. lift oft
at a cantata faa opee
This speed
is lasrsa.e4 atea the cr3tt
is
n, hestZjr 14.d. Piinthez raiol.a
st the levers ivu jasrascad
stati. havsa height,
Triisiag st ib.
sasSi is pite
is a.hje,ei b; &tfotcutja.
use cat these levez..
i
ipalstio 1 the (pzepelisz.)
tig'uat lever. ent (ctcs f aireo)
eastasi
-kiel oauces the irait to
ao, away in the tesized ¿tzostiim,
Havarie5 st speeds belw l heats (heap drag upset)
over catai,
the üpreaaia
is the aster sutaee beesath
the croft ¡iv.. a
et
'k.t1' stfeat arricting Li over,1.fli .0. Ipift.
niioeuvrin
over .rntor at 51ew ep.cd fe bt øUÍri
sut t
rs4iad.n
ho?er hiht. In thir coitton the ej'sft oSli rts
ik10
convontioruti boat, aoutro1 betn osbteM a1Tost .nttve3
os the rud3.er
a-d uro of ij!far,ntid thsut.
Traveflie
t high isc4 the ratei' .uWss t'. ralattvsly
umiitnbe
sit4 the
o1 .ff.ot i. set pveunt. ui.st. t bus
sind. eust bi eoitrofle* b7 use of tb
?srati'4 fias, but is sitz
saies it usy be nese..ar' to yaw the erift at. the eLM te
latsts
s Iaafre& track.
Whoa ao1d.n
a turs OTS? retir the .ruSt sill veapu te
*ar.
st1utiøn, bet uaLag fro. the .uk of salar bui,
exiSt sill
bugS.s t, sk.i4 *l4swsyà alng the oridasi trssk,
Operctios et the f crward fLua 4sirsss. tM. tsaâuq aM fair7 lar
raliva tersa are sa4s witheut .kU&tai.
In as sserguuq
i...
avoSdases of saUsa ob,trustiou, zapiL ruth
et twn sra ¡ossLb1i ist
1'urm3
i.PTLet us consider now bow Hoieorstt
eon be mod. onas
off ioiont. Th.z. ars two major eqs of riduSili the¡owes required to maintain the
cuabionz-(s)
developedair
curtains (bi mechanical curtainsRecircuistion
la
a po.sibl. emsif
obt&inthg $ more efficient sir cushion. Developed sir curtaInssmplq-thg reoirsulstion are shown in Pig. 13. This omoo.$
la
to use the curtain more then once before it la allowedto rice into the atmosphere. The air or .q not be
re-energised before final dis Ohazge. Por the price of
complication ja dust. deaii substantial reduotion in power
i be achieved.
More r i.sing than developing the air curtains is the
approach of reducing the area of the sir certain however.
The most simple insana of doing this is to
port'y
seal thecushion vith solid mechera Of course, the members t b.
introduced so that thv do not incur large loads upon the
ore! t. One exemple of this mechanical sealing a to Introduce
sidewall. which project downwards at the sides if tb.:orift
below the surface level. On euch a craft
power is
requiredmerely t) maintain
the sir curtain
st the front and rearif
th vehicle, but the price one pqs istas
loss of tb.ciph4bioue oapabiliy end also the speed is rsatrict.d some
45 knots. Above this speed the dro'nanio drsg sssoeistd
with dragging the sidewall, through the water exceeds the
power caving dus to the redaced curtain area.
Por general applications over all surfaces the curtain area is beat reduced the use of flexible members. These have the
advantage that the resistance to water and iapat loada associated with the flexible members striking the aurisos are halted.
Pig. 14 sunnarises the different wys in which flexibili
cuy be used.
The general problem is to intodue members manuf.ag
if
flexible materials or members flexibly meimted an the craft's naln
body which readily respond to waves or rough countly.
The coving - iq be psrauM to rsapond t
G the'e . Tb. first 'cup of flmxibl. Hoveresofft.4 .b.
Whiah ers aotaatsd osotsoting tbs suIsse over hiah th* ipust..
TN.
p. bas bun u..dso
s nusber st craft aitbaugh t i. tifl, roso for da1.p.mit, It Sa ost esacatial for isoLai. bcvazaz.ft to contait the surfas. buever ter the aeviog parts of thecraft bi situated cushion pusu. s. illustrated io to.
escoed pioturs. This ps of craft consist. of a snober of o'r'°
os cella sro the peripb.zi of the eilt sod each fleztb1 mted. The coin craft Weight
is
ta ' the central osahionthe outer calla onrsly actuate the f1wth1. parta.
At hidhar speeds ontion of the flexible parts Vili tend to lag behind the waves resulting
is on
increased seen gap between the craft
the surf ace.
Por the fissible parta to closely follow the surface at higher speeds it is necessary for thea to base highsoosjustjan_s
to
receive warning of app osMng waves. To do this the flsb1. part.
mast be powered as illustrated in the leau figure.
105 such s areft
a sensing device and servo qeteu are ssp1red.
Putu hovercraft ciploying single er isiti-stage
flexibility will require s fraction of the installed peau of
that of rigid bovercrsft.
The introduction of flexible neobers permits a pestar desigu height for the nain bc4y of the craft the 1arsr
*dronsmjc -t loada encountered
lOr riglA bawsrusItctrifrig waves are no longera proales. Local impacts and
abras ion are not berne
the sain structur. but Iy the fissible
components,
We chill now consider what future bovepøaft coy look liho. Fig 15 ta an artist's i.pronsjon
of s boverurmjt projeotsa at Vtch Armstrong. end d*siate4 VA-4.
It is a high speed over water craft with an amphibious
oapabiiiy sad is a logical folles-on from the basic concept o hovercraft ac* th. early developeent craft. 1pica,l data for a craft of this e-pe is as followszw
I
A11Wtght
-
100 tons
Total installed pawir
-
15,000 N. P.
Pqìoad
-
£comnodstian tez' 240
panangere , 2
oars
0ve'all disione
-
140' z 50'
Speed
-
80 mots
iwaven up to 4.tt.
Scheduled service would
continue in ness of wave
height
6 - 7 feet.
uoh a croft would hive an operating coat of the
name order
I
as coipetitive vehicles.
Lt enploya ilexible members and would
operate in coastal or iheltered waters.
It could tor atpIe, speiste
ver the English Channel in spring and early suer, but in winter
menthe it would find that there would be too
as
days on which
operation would not be safe.
Nevertheless, there would be a number
of placen in the world where it could offer
a car and passenger
terry service with a substantial tine saving on existing vehicles
and at competitive fares.
Lecture 12
't
1
bD
BUOYANCY
TANK
FA NPROPULSION
UNIT
AND
CONTROL SURFACES
STRUCTURE
DIAGRAM
INTAKE
FAN POWER UNIT
(3
Case 1.
Caae 3.
Si4e Kieviition
C4.
2w
Case 5.
Water Impsot Iadin
Csaes Without Rotati.
Caae 2.
S ido
EleyBtjGfl
+
Water Impeot Losdlng CMO5 with Rottj.
d E1evatjo
Csse
3.
-4-Ca80 4.
I
1Ca.e 2.
*
j')
j
f
VAI
9' -\'r'?.t "
Frg.'7 V.A-I WATER TRIALS
'
S
'
L- 7A
1ll
"..',.
-,
4.,'---".c
4.'
frfig.? VA-3 CABIN INTERIOR
r
s44$
t
j
j
i:NON - £NE2c, ISE,o
RECieji. A 7?OA/
¿/vEecLs10
RE
TYPES
O F HO VERC
RAFT A/
C URTA I/vs
S/M
PL.EC.L'e7A lAI
t
t
'y?
VgcBMT
LRCTUR
12 (C)
VISARMßThOflGS (mns) Lm
(C)
sccs op oiic« op iii
A LBCT.x TO B PRES
IN RODAI 3!
.. OC. KN
Lsct. 12
LIST OP cozrai's
PLaCE D ThE T}tA1J'.T SYS
Sp» 7BCTS
4...
DICT OP1ATD(G- CC3TS
F14. I
LIS? OF LIDES
Sp.
ijt nve1ope of civil craft
operati
o,er water (with ilovereraft)
Traaspog-t systeme
- Jourxy tje
?raogrt y5te!. Fare.
- ata8e leathoveraf t direct nperetin coota a33ptjon.
liovercrat Y.
'L-3 direct operatin& costa Siz.e a4 coot of craft.Place in the ?anaport
.yetou
We
retunt
now to a tigore shown earlier,
i... the apoed/
weight envelope of civil
craft epatj
over water.
Placed on
the graph now in addition
to the existing
vehicles are the
pos-sible over water A.C.V'
or Hovercraft of the futuro,
The Hovercrett
are divided into three main cluses.
(i)
At the low speed end
there is what
maybe called 'river
Hovercraft'.
Thon. have an a.1vantae
over existing river
craft both in fast ocrront
and in akmflow watoe.
Sono
of these may be nf the
iznnersed sidewall type.
It is
thought that the speed
rango might be up to
a m,tn of
60 knots, but
probably
30to 40 knots depending
upon bende
and other traf tic,
and the weight will
cbab1y be between
1G tons and 1,OOC
tono.
(2)
'basic Hovsrcrsft
axe the conventj] sheltared
nod
open water craft.
It b thought that t
would have a
ma.zicus speed of 150 knots
end there te not onch point
in going below 50
knot..
The wsight of the craft may very
trou
.ii craft weighing a few toas carryii
a few people
te something approechieg
10,000 tons in the case of the
Open mater craft.
(3)
A third clase
et
craft tensed 'high speed Hovercraft' in
the graph could
cono*iveb].y go beyond 200
knots in speed
atri would probably be
rather large vehicles,
Thsoe
would
not be oonventjo
Hovorcxatt in the
sense of having a
static air cushion boigided
by an air ctrtaj
Instead
tho front air curtain
would be 'switched oft' at high
speed and the dnomic bead
or ti
free a treno used to
o5!tbuto to cnshion
pxesn..
It 13 rather significant that
al though Hovercraft
ciìi
conceivably occu
a large area on the graph, this area does
not overlap tae oporatin
erwelopes c' the aircrs.ft
and the
ahip.
-1-Speed ffeota:
Iitting thehi& speed Heveru f t'fez the present, two
essentially
different classes of craf t, the "imeeroed sidewall',and the 'free-of-the...'
craft previde two speed rouges. In
tsms
of
craft output the irsed
e idewall is the mootatact-ive it ¿isla gatact-ives the *m*liest capital, outlay
par craft and the lo,est fares. )owever, the economic
comparison zeast be
in a intien with the operational
features present. valua can be put on the speed superiority of A. C. V's.
icaca-aed sidmj.1 has
a 2j to I advantage over equivalentdisplacement
ahipa. The 'free-cf-the-ewtace craft has a Ij toI advantegs over the aidevali.
Rather then speed, "convenience" is probably the
e powerful attraction to the intenjjn
pasaewger; bez's convenience 1moludee a meazwe of speed
as it
sifects the block time between
the two pointa the passenger viches to travel as compared with the alterimtive means of
It is in the context of
convenience that the smphlbiou5 property
of
the frei of-the. w'fece' A. C. V.gains compared with lb. imeersod sidewall craft.
A route cay be operated not other-wise poasible by reason of ehallow water, obstacles etc. There is e choice in the positienjag of
terminals and such ter'dnels mey be con.truct
at a lover cost than those requfred by non-smpk4biou_. craft. Aise s'ter turn round
times should be po.-.
aib].. Development
of
the itaeersed sidewall craft will give it
a limited
aMpl4hjog5
qnality, say slip-way capability, without
changing
the essentiel moteof
the waf t.There iU than
be a vider choice of termical location..Pigiwe 2 illustrate. the order
of
the fares gap otilensnot be offset with the greater oonveniez
off eremi by the
A.C.V.
Other things
being equal fer routea of 50 miles or lesathe isotareed sidewall offer,
a Substantial speed increase with little
or
no izoroase in fare. Over longer routes the fares of all A,C.V.a are
coasideraL.jy in excesO o. ahips axtd thecraft with the ¿as.xizxm
spet1 capabiliy will
prove to be mars
atfractjv..
These ocesideratJons
are quite apart
fres themettere of routes, taXInh1l.1A
etc.
Fares:
The estimated paaaen_g,x fare thet would be eborged on the
100 ton A.. C.V. is canpared,
in Pig. 3 with typical fazes
charged
for ships and etrerart
The fare ja. given in terms
of pence
por passenger mile aid la plotted
against the stage length of
the Jowney In nautical
miles.
As the operating cost
per nile
reduces consIderably with inea.se in stage length, operators
are able to offer lor taxes for
the longer joinsrs.
Con-aidoriag the ship, we can see f rem the fares quoted for
the
Isle at ¿iglzt and
ae1 bosta
that
there can bea conaiderabi.
variation, The ninj
faze
chez'ged onboats is about
44 anIcan apply for journys of 20
n.s. a.id above.
The afroratt, although it
can
otter oareble tarea to
th. ship at
stagslengths of a few hred nautical
edles aid
above,cannot compete at stage lengths
up to 100 nautical ailes.
100 ton A. C.V. i. expected to
otter a ocaparable tore
to the ship aid the aircraft,
but the
stagelengths over which
these fares apply are about 50
nautical ailes
and abo,s. Theo1msjens we sdght
drawtras this graph axe
:-(i)
At 2cv ntae lengths
say up to 25 n. miles the
A.C.V. tare. are in excess of the ship.
The
at-tractions
of the Hovoreraf t are its
speed and
rdiacod loading aid unloading times duc
to its
anpbibiaua nature.(ii)
Betvesn 50 n,n, and 25G
n.a. the A.C,V. really
omca into ita ona nith ita attctivg
apoad cal
competitivo fares.(iu)
Above 250 n.m. the caso for the
airca'att is very
strong and the chance of the
Hovercraft would
appear slim on these f
iwea,
-3-It should be borne in mind
however, that the tarea quoted for the 100 ton A. C.V. aroby no na eatabliahea_,
The
par-iouler oral t taken ha s lind ted applications,
. waves up to ore 6 feet significant
he
ijbt, but on the other band
develop-nient 01'
the
craft night ienkeit
moe's attractive than the graph
iiLioat.s.
Dfreet
Ctir:t.t.g
CostaWith the introduction of a' new term er tromaportation, the items of prime importano. to a pro8pec tive opErator
are the sise of payload whioh can be carried, the cent of
cerr.yisg this
peload, and the initial coot of the craft. Another oonsidrat..
ion is the development tireo
required before economical operation
can be established,,
At the present ti.iø hoveroi'af
t are being Ceastruotod based on aircraft type etrurturca and
power instaUatjon, and using
atand,arì aircraft onto riais. In view of this
the estimation
of direct operating cot baa been based on the cerrt
method
of esttj'tatj' aircraft
operating costa, The reference for estimating costs has been the S. n.A. C standard method;
in a few instances the formula, have been a&juated to suit the Hovercraft requirmeonts. A typical set
of
aastiona is shown
in Pig, 4. aM timas have been used in øbtin1ngcrative
costs for various craft discussed in this paper. Pig. 5 presenta
a coot amalysis for a smell amt t.
Comparing the direct
oper-nun« cesta
of
tarions iraf t using the some standardsof
en-gineering construction and
development, although the operating Conditiea are not identical, the
variation of craft size and coat readi3j be soon. The trenda due to sono of these parameters are iliustrat-' in Pis. 6.
-?-101
lo,
Io
.1SPEED! WEIGNT ENVELOPE
OF CIVIL CRAFT
OPERATING OVER VATER
r- -
sI
g%BISBI
' 'SPICO
I
' Basic
,'
HOVER ______________I-,
HOVEl
'
ICIAFT #
s CRAFTi
I
i
,
SlivEl
VA.5
1ROVERCRAFT$
sV.A.4,e
I
/
OIL..
s s/
4V.A.2
I
T
10
20
50
40 50
100200
¡00 400 500
SPIElKNOTS
JOURNEY TIME
(HOURS)
3
2
i
o
50
100
150
200
G.'STAGE LENGTH (NAUTICAL
MILES)
a'
NJ
TRANSPORT SYSTEMS-JOURNEY
20
16
FARE
(PENCE PER
12
PASSENGER MILE)
N
.,
N
A.C.V. s
50
AIRCRAFT
HOVERCRAFT
ISIDE
WALLCRAFT
I I IFERRIES
100
150
STAGE
LENGTH (NAUTICAL MILES)
200
TRANSPORT SYSTEMS- FARES.»'
HOVERCRAFT DIRECT OPERATING COST ASSUMPTIONS I. ANNUAL COST Amoetization
-10 years Utilization -2,000 hours/year Spare8 -10% first cost Insurance -3%first cost
Interest on investment -4%first cost
MAINTENANCE AND OVERHAUL COST
Labour cost
-7 shillings per hour
Engine overhaul
-Annually
Fan and transmission overhaul
-Annually
FLYING COST
Crew
LI per man hour
Fuel cost
-20 pence per gallon
Berthing fee
-£3 per hour
TOTAL DIRECT COST
DIPCT OFFRATI'
COSTS!.
ANNUAL COSTSL
perhar
-
19.9
3
2,
MADT!!iWC AND OV9AUL COSTS
L
perhour
-
9.5
2Q43.
FLI1G COST
£
per hour
-
23.5
4.. TOTAL DIRFOP COST
L
per hour
5.
PAC'T
CJD! S
COST P SEAT ThE
HOV'RCRJFT V ft -3