impact resistant composite materials f.or casfi in transit git … · impact resistant composite...

1
Impa Resistant Composite Materials For Casfi In Transit GIT Securi Boxes Aim: Define a suitable composite material to be adopted in the development of the new Cash In Transit box at Spinnaker International Limited Produce a full size model of the outer sheII of the CIT box with the selected laminate Define potential fibre reinforcement architecture Source Laminate properties of the selected reinforcement MINIUM F:M• 4 •OMONIN� C$WIYlll(R �4 "' lVCtU (IIN , 1Z +0,w,i RUltlR tHCl aM:1 IHIANO NI IO ,_. UOCGlAlt . ...-_.., n 10,0 O •O, . , 0.1ћ •n ,_ •n ,_ '" 0.1 0.1 ,_ 1111 ,o cn,,,o C-••- (ltl 2. •N l'11:t.H•N ·�- =·"--. :• . . . . - . - - --- - . I --I __ 1 : Define potential laminate stacking sequence J /�. ., . ,, . .. , . ., " . ,_ ou,,so - llC(LI . . . . . ·- . - 1 UO(GIAtl J UO(I 4 UOUHAII I UOCOVU I UOOIAH UOUIlt I UOCOVtl -- ,-·-·· +_,_ ... Implement Properties and stacking sequence in LAP ·- 49 o. -n ··- - o.-n ,.-n 49 . . - ··- .. , .-n - - Computational simulation of laminates adopting estimated impact loads ' -r L- " - Define a suitable laminate layup for the test samples , ' = _,__ _.� .. -- -�== = Contact suppliers to source high impact resistant constituents Define laminates to be manufactured for the test samples ' -- COMΠOSITES WITH PLMOUTH UNl¥ERS1T¥ -- Estimate forces produced by the impact testing I ___ ,,, I estimation of drop weight forces I I IE , I 1: I Iii 1: 1 .. - ,� , Source suitable constituents in the ACMC lab at the UoP in relation to the laminate layup defined through LAP ; -- . -- - ------- Carry out a cost and weight analysis to ensure compliance to specification = ,_ - - ,- --- --- e� t Produce a curved test sample to monitor the impact behaviour of the laminate struct ure t Define a suitable composite laminate for the implementation in the new cash in transit outer shell --- -- Implement the results achieved in an evaluation matrix Analyse failure modes induced by impact testing Carry out impact testing on specimens Manufacture test samples by resin infusion under flexible tooling 11 --� _ _ _ ·- :-- : -- ·� f --- . ·---- -= __ __ M - - - ·--- - - - ·- •-·-· =·:, ·:::= -=-· - ====-===- --=--- -=-- - .. ·--- - ·--- - t . -- ::;:.= -- _::: - - - - ·-· _·- • .:.. ·· .. t. . i t. t_ ;_ t .. ·--- - ·--- - · t Analyse load-deflection curves to define laminate flexural properties ' Load deflection cur\'CS from thrcc�1>oint b\•1ulin - ·- ·- ·- •= ·- - - - - , ICSI ' HI 1, ..... , .... _,_) I -A? ! -.,:: -,,:_) -o:_, -,, :_: -o:_, -,:, -,.:: -u, _,_, n -1: ,-- Carry out three-point bending test on specimens Joseph Barnaby, Stage 4 Mechanical Engineering with Composites Universtiy Plymouth (26th April 2012) PRME304 - Honours Project Open Day

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Page 1: Impact Resistant Composite Materials F.or Casfi In Transit GIT … · Impact Resistant Composite Materials F.or Casfi In Transit GIT Security Boxes i'I Aim: Define a suitable composite

Impact Resistant Composite Materials

F.or Casfi In Transit GIT Security Boxes

i'I Aim: Define a suitable composite material to be adopted in the development of the new Cash In Transit box at Spinnaker International Limited Produce a full size model

of the outer she I I of the CIT box with the selected laminate

..

Define potential fibre reinforcement architecture

Source Laminate properties of the selected reinforcement

MINIUM 70:M• 4 •OMONIN� C$WIP0'-Ylll(R ll�49'f:"OX'I' "' "1ll.VCtUl'l ll(IIN ,vi: ,.0- 190 110,w,i RUltlR tHCl aM:10"5 IHIANO NI CMIOl't ,_...,. UOCGlAlt . ... -_.., .......... .uJ:

lfn 1....,0,0 Ott 9"o•O, ... , 0.11115

•n ,_ •n ,_

'" 0.001 •• 0.001

,_.., 1111 :i.,o. cn,,:»oo,o. C-••- (ltl 2. .. •N l'.111:t.H•N

·�- =�·�"�

--.-,-.--� :.•

. . . . -. �

-- --- -

. --

I -- I

:,-:: __

1

:

Define potential laminate stacking sequence

J /�. ., . ,, . .. ,;, .

., " .

•• • ••

,_

ou.u,,so -llC(LIM,

. . . .. . .

·- ... -• • 1 UO(GIAtl J UO(llV,.II 4 UOUHAII I UOCOV.U I UOO:OIAH I' UOUIV\lt I UOCOV.tl

--,-·--··· 11_,_ ........

Implement Properties

and stacking sequence in

LAP

·- 49 o.-n to ··- -o.-n • ,.-n 49 .. - ..··- .. ,•.-n •

-·­........... -

Computational simulation of laminates adopting

estimated impact loads

' -r

ill:.

L..=...-

"-

Define a suitable laminate layup for the test

samples

,.

'

-,

= _,..__ _ .... � .. _,_... .. -------�== =

Contact suppliers to source high impact resistant constituents

Define laminates to be manufactured

for the test samples

'

--

COMPiOSITES WITH PL'fiMOUTH UNl¥ERS1T¥

--

Estimate forces produced by the impact testing

I ___ ,,., I

estimation of drop weight forces I

I# I IE @;,.;;:.._ I 1:

I&: Iii 1:.. 1r,,

.... -

,� , ..

Source suitable constituents in the ACMC lab at the UoP in relation to the laminate layup defined through LAP

1t

":;

-­. ----- -

----------=--=-

Carry out a cost and weight analysis to ensure compliance to specification

= ,.__ --,-

------

e�

t Produce a curved test sample to monitor the impact behaviour of the laminate structure

t Define a suitable composite laminate for the implementation in the new cash in transit outer shell

--­::---

Implement the results

achieved in an evaluation

matrix

Analyse failure modes induced by impact testing

Carry out impact testing on specimens

Manufacture test samples by resin infusion under flexible tooling

11 ;:--� _-l= _ __.i=._ !-·- :-- :"-'!'... --l=-----

·�f -c

l-

--- .!"::..""::. ·-::...-...=.:.-.=-- -==- ("�-:--!'!':' .. __ .. __ M---·--- ---;:::.,-·-

•-·-;:...-:=-· =·.::.:, -===-··::::.:=.:.."' -=-· -..:.:- ====-===- ---==--- --====--

-..

·--­-

·--­-

t ...

... --=- ::;:.:-.= .:...-=;:: -===-=-==-- _:.:::.:::.:. ... _i-

- - -

·-· _,-·- • .• :.... !_,·· c: .. t.. i t.. t_ ;_ t ..

·--­-

·--­-

-·· t

• •

... Analyse load-deflection curves to define laminate flexural properties

'

Load deflection cur\'CS from thrcc�1>oint b\•1ulin,::

-·-·-·-•=·-----

,

ICSI

' HI 1, ....... , .... _,_)

I

-A? ......... !

-.,:_,....:

-,,:_.,..) -o:_..,..,

-,,:_:

-o:_,

-,:........,,

-,.:._...:

-u.......,,

_,_...,, n .. -1..,,...:

,....,--......,., Carry out three-point bending test on specimens

Joseph Barnaby, Stage 4 Mechanical Engineering with Composites Universtiy Plymouth (26th April 2012)

PRME304 - Honours Project Open Day