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powerandpassion

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  • in reply to: Just how rare are Merlin engines? #1012755
    powerandpassion
    Participant

    FAA approvals do necessarily mean they can be used on CAA permit aircraft.

    Product liability….. releasing drawings and that part failing and causing deaths would come back up haunt you..

    Take Rolls Royce as an example as they built the Merlin, they no longer produce piston engines, they have moved on, why on earth would a company as such release drawings for parts that are no longer made, for engines where their expertise no longer lies, where their core business isn’t, because as the Design Authority they would be culpable? If anything went wrong, it would open them up to future litigation. Remember in the scheme of things there would be no advantage to them, financial or otherwise, just lots of risk. And in this day, an age of bad publicity and the effect on a companies share price, you can totally understand it.

    Hence why without the likes of Royce’s, Marshalls and BAe onboard as Design Authorities, the Vulcan would still be sitting at Bruntingthorpe, as one would imagine the CAA would have said no chance. I’m still suprised they got onboard as it must have been a risk for the companies.

    TonyT,

    I apologize for reacting viscerally to your post. It is not personal. I am a Dreamer. All your points are valid and grounded in reality. I have a friend who I debate with who calls reality the “Big R”. Our debates are never won. At a distance to any particular debate, I reflect that the Big R and Dreaming are wound around each other like a helix, in any healthy state of human affairs. If one is more preponderant over the other, bad things can happen. In respect of aviation there is no progress without Dreaming, and things don’t fly without the Big R.

    I sense that in historical aviation there is a shrill, protesting element to the Big R. It resents Dreamers doing things that it can’t get a handle on and pigeon hole. It’s visceral urge is to shut things down. It’s like a lorry driver looking at an upturned truck of chickens squawking and scattering over the road.

    Fundamentally things in historical aviation are driven by Dreamers, who turn scrap into angels, fanatics who grind, smash and shortcut their way to the top of impossible summits. If they don’t fly headlong over a cliff they eventually tire out the “Big R”, which begrudgingly accomodates them into an expanded version of Reality. So the Big R, which swore 40 years ago that a warbird would never fly, now tolerates this. In the end the simple fact that 70 year old engine spare parts supply cannot sustain the present reality will mean that the idea of remanufacture will have to be an unremarkable reality.

    How could we get there ? Let’s accept that the taxpayer funded and sustained the aerospace industry as an intrinsic feature of the industry. Without the taxpayer the industry would have failed many times over. I am impressed, in going through libraries, how many publications were funded by old industrial conglemerates, in a tacit acknowledgment of mutuality. These days it is called being a good corporate citizen. I can understand that it is not the job of a harassed manager in a modern corporation in the midst of a global recession to accomodate requests for archived engineering information and the unrenumerative supervision of some Dreamer in a garage working on an antique product. Perhaps the Dreamers should become more sophisticated in their approach? Use the tangible accounting factor of ‘good corporate citizenship’ to propose a transaction which is digestible.

    One thing to do is to setup a non profit, incorporated entity to take anything to do with antique products off corporate balance sheet, off products liability exposure and off the current budget. At the same time set up a constitution for the non profit, incorporated entity that captures the essence of what it is for : making children see and hear V12s flying through the air, to be proud of their country and perhaps want to become engineers. No doubt such an entity would want products liability insurance and professional indemnity insurance for its officers. These things would cost money. Therefore it would have to charge cost recovery to any party wanting to use its archives, conditional on accepting inspection of works completed in accordance with archived procedures, again at cost. In other words a mini CAA, made up of semi retired folk, skilled in the art, excited more by a participation than a paypacket.

    Properly constituted, such an entity could act as a circuit breaker between a modern conglomerate, modern inspection and approval authorities and Dreamers.

    Another aspect is revitalising a collectivist ethic. As a complex mechanism aircraft and engines were products of original collectivisation, between metallurgists, metal suppliers, forges, casters, cork gasket folk, magneto folk, bakelite magneto distributor cover folk, platinum depositors on distributor breaker point folk, breaker point spring folk etc, etc. In some way responsible Dreamers must become collectivist. If you know you need 20 distributor breaker points, make 1000, get them approved by the previously described non profit incorporated entity, then make them available to the wider community. For the sake of collectivism, fix the profit on cost at 30%, as the government fixed the profit originally. The advent of the internet makes it feasible for the cork manufacturer in Portugal to make 1,000 sets of rocker cover gaskets, the engine bearing manufacturer in Australia to make 1,000 sets of big end bearings, the crankshaft forge in India (!) to make 500 crankshaft blanks and the CNC machinist in the UK to finish 1,000 fuel pump gears and be on one database. Rather than one Dreamer make 500 individual pieces over 25 years, make 500 repetitions of one part in one year and buy/trade the other 499.

    As I say I am a Dreamer !

    My understanding with forging crankshafts is that the skillsets/experience to forge from billet as per original method is scarce. Theoretically a forged crankshaft may be stronger on paper but the skillset to work economical numbers of ‘accepts’ is not there, whereas CNC from a billet of proven, modern metallurgy gets a result. To say that there has been no progess in steel metallurgy, viz, alloy composition, may be correct, but this does a disservice to method of manufacture. In other words the capability to produce grain structures of predictable and superior characteristics is much improved (unless it is a chuck on a Chinese manufactured drill, when it may have asphalt road inclusions). It is not strength which is wanted, more predictablity.

    I do like the old engineers, they were Dreamers :

    “An important feature from the design aspect is that if it is desired to use material of different characteristics, or if new metals become available, no re-design is necessary-(in respect of tubing)-merley an alteration to the gauge of the tubing.”
    from Air Annual of the British Empire 1933-4 -Hawker system of Construction pg 342

    God Save the Queen ! God Save the Merlin ! Sigh for a Merlin !

    in reply to: Rolls Royce "R" Engine #1012938
    powerandpassion
    Participant

    Come on where is the rest of the engine stop teasing !!!!!!!

    Mike E

    http://www.whirlwindfighterproject.org

    Engine was melted and made into a Ford Escort gearbox assembly, subsequently remelted and made into 280 Chinese manufactured toasters….
    Just like the latest fad is to trace your ancestry via DNA to some angry Viking or randy Spaniard I wonder if radio carbon dating alloy components within metallurgical analyses will indicate some provenance….I probably have a toaster that was originally Excalibur and part of Baders tin leg !

    in reply to: Rolls Royce "R" Engine #1012947
    powerandpassion
    Participant

    Brain frying

    I also have this firing order plate which I think is RR Vulture?
    Can anyone confirm this?

    [ATTACH=CONFIG]221595[/ATTACH]

    I have reached the limit of my thin competence on this one ! No doubt an X engine, looks very much like a RR Vulture, but someone with a mind that looks like an enlarged, inflatable dinghy growing out of their head will need to confirm the mathematics and engine balance probabilities to back up the punt. Or look in the AP.

    in reply to: Is this a Boost gauge? #1012955
    powerandpassion
    Participant

    Maybe breach air pressure

    Thank you all, the pressure range is what worried me…could it be part of a calibration or test rig ?
    Regards Mike

    Left field thought : maybe air pressure gauge for breech loading mechanism for Anson ? I cannot see the scale being realistic for Boost pressure. Later Ansons had similar gauge scale with more modern gauge by Dunlop. Perhaps breech loading mechanism had the capacity to form a vacuum in the reservoir once the gun got going ? It would alert the ground service crew to ‘reverse vent’ the air bottle before fixing compressed air line to bottle to recharge the system. Taking a punt.

    in reply to: Just how rare are Merlin engines? #931808
    powerandpassion
    Participant

    Never give up, never give up, never give up.

    Err I think the technologies involved would prohibit it simply on cost, one would doubt many companies have the facilities to do this at all, and that includes RRoyce. Indeed some of the machines that could have produced parts to such critical dimensions no longer exist either and haven’t for many a year, so you would be spending tens of millions simply getting the infrastructure up and running before you knocked out a single washer.
    Top that off with the only people that hold the drawings are never going to ever release them and you are on a hiding to nothing.. Rocket science would be relatively easy in comparison.

    Tony,
    I’m gonna have a crack at you ! In order to find solace from this post modern paradigm of self defeatist, cold water pouring, lily livered, gormless, authoratative denunciation of dreaming that has assisted in seeing industry dismantled, manufacturing jobs lost and capabilities flushed down the toilet I turn to old aviation literature, which is infused with an entirely different spirit. While you hose down your neighborhood the Chinese government is doing the opposite and rapidly building up the mentality of its engineers and entrepreneurs. Go pull out your old “Bridges of England” or Aircraft Engineering to see what goals grandpa kicked with one eightieth of the resources at your disposal !

    I understand that there was only one forge capable of turning out Merlin crankshafts in the UK prior to the Battle of Britain, proving conclusively that in the United Kingdom there were not “many companies (with) the facilities to do this at all”, so the UK should have just turned over and died in 1940. Today, I reckon there would be more than one machine shop capable of CNC’g a crankshaft out of modern 4130 and then heat treating it using usual techniques to come up with a short run of crankshafts equal to 1940’s forged specs. Block ? Shoot, where the city of London can come up with exchange traded derivatives, collaterised debt obligations and other algebraic financial confections then complexity is still within the wit of modern Britain. I reckon Old Harry can still put together a block casting down the road.

    Can’t get drawings ? Why ? Why would the proudest manufacture of a nation be hidden ? What would it do for a younger generation to be drawn in to an OEM supervised short run ? Perhaps get them excited about engineering ? About excellence ?

    The can’t be done attitude makes me want to reverse engineer a DB 605, to absolutely prove a Merlin can never be done !

    I do like the boat. That’s the spirit ! I don’t have the bling or the babes to carry off a snort to Calais in a unit like that. Controls would need to be in Russian so buyers could understand which console the cocaine was stored in.

    Really if you had not spent all that time hosing down dreams it should not be fitted with a 70 year old engine design. It should convert the hydrogen in seawater to generate rocket thrust at higher power to weight ratios than a crusty ‘ol IC engine.

    I have just finished Nevil Shutes “Slide Rule”, a person who started Airspeed on nothing more than excitement, and he provides some considered reflections on his career in aviation development : R101 & R100, government v private industry in innovation and especially what made innovation work in the 1930’s, in the teeth of a Depression. Astonishingly, he put this down to a class of Boris Johnson like upper class twits with money, who, on the basis of real estate derived wealth, were willing to punt on high risk, new technology start ups. Death taxes wiped out this segment, and I guess this is coincidental with the decay of UK industry. It is an unusual, though not illogical observation. All that seems to be left is defeat, defeat, defeat.

    I shall now retire to my drawing room to listen to some Winston Churchill broadcast recordings, as a tonic.

    in reply to: Technote Vickers Potts Oil Cooler #931819
    powerandpassion
    Participant

    Destructive tests

    Some destructive test findings, so you don’t have to repeat them !

    Fabrication is made of two shell pressings, top shell and bottom shell (larger circumference)
    Shell pressings appear to be hot dipped in high temperature (hypothesis) solder, as inner and outer surfaces are evenly coated with thin solder, and this would be impossible to accomplish after rivetting of shells together, as solder could not drain out.

    (Hypothesis) Electro chemical corrosion between aluminium spacer rings & brass fins in an assembly subject to water spray would be aggressive, as fins and spacer rings are designed for metal to metal contact.Therefore dip coating is zinc rich, as zinc is relatively passive to aluminium. Central steel oil distribution pipe is not in fact in direct contact with brass fins, so another potential source of electro chemical corrosion is avoided. The original designers have been thoughtful in combining dissimilar metals prone to attack each other.

    Each copper rivet has a brass (B6) spacer. Spacers are in three sizes – large, medium, small. All rivets, including short rivets that from outward appearance show the shell pressings kissing each other, have a small spacer. Spacers soldered onto bottom shell to fix in place. All rivets have a copper seating washer under top and tail. All rivets have a blob of solder over top and tail. Cross section shows this solder penetrating down the shank of the rivet, well sealed.

    Each shell pressing is B12, fully annealed brass. Bottom shell with larger circumference is turned over at edge to form a bead over the top shell. Bead is flooded with solder to assist seal, cross section shows solder sneaking into the folds of the bead, well sealed. This bead is even around the circular edge of the fabrication – no crinkling, splits or deformation to this bead around the circle.

    Most commercial grades of brass sheet used for modern pressing in half hard condition. Very difficult to replicate the even beading around the circumference in half hard material. Very hard to achieve with Jenny wheel. Perhaps this is why a fully annealed material was specified, in combination with a “low skilled labour” method of mechanical beading.

    (Hypothesis) Order of manufacture for fin assembly :
    1. Bottom shell, with rivet openings, was pressed with outer edge turned up 90 degrees, top shell pressed to snuggle in to top shell, both shells zinc dipped.
    2. Copper spacers soldered to bottom shell fixed in jig with standing pins used to locate copper spacers.
    3. Top shell placed over bottom shell in assembly jig, progressively riveted.
    4. Circumference beaded.
    5. Circumference and rivet top & tails slobbed with low temperature solder.

    Have completed autocad drawings, will output as .dxf files to send to the toolmaker. Seems like a relatively straightforward pattern to CNC from a dxf file. Have found an old press tool to cannabilize to make up shell pressings. Brass sheet suppliers all scratching their heads as they only have half hard sheet on the shelf, and the last of the Mohicans still manufacturing things happy with that. May need to special order fully annealed material. Better open a beer while I think about that.

    in reply to: Rolls Royce "R" Engine #931861
    powerandpassion
    Participant

    Firing up

    This raises a point that interests me. How many different firing orders ware there for V12s. I know that there are only two common ones for a straight four though other than the most common 1342 I cannot remember the other one.

    The following data has been translated from the French “gauche” = B (LH side from pilot’s view), “droit” = A (RHS) from Hispano Suiza manual for
    Hispano Suiza 12 X engine (1930’s)
    RH Tractor : 1A, 6B, 4A, 3B, 2A, 5B, 6A, 1B, 3A, 4B, 5A, 2B (Same as RR practice)

    The following data has been translated assuming “left”= B, right =A from Curtiss manual for
    Curtiss D12 engine (late 1920’s)

    1B, 6A ,5B ,2A ,3B ,4A ,6B ,1A ,2B ,5A ,4B ,3A (Curtiss D12) refer below
    1A, 2B, 5A, 4B, 3A, 1B, 6A, 5B, 2A, 3B, 4A, 6B (RR Eagle, RH tractor)

    Which cylinder fires first is immaterial, I guess the British chose 1A at the top of the list while the Americans chose 1B, but ultimately the pattern matches.
    So, at least in this random sample, British, French and US engine makers chose the same protocol for firing order, probably limited by the balancing requirements of V12 geometry. If this is right then German DB 600 firing order should be the same ? Achtung ! Was is das gersplutterblitzenorder DB 600, bitte?

    In respect of HT leads I have noticed small, numbered bakelite grommets on RR Kestrel and Bristol Jupiter HT leads that would help connect things up the right way. A lot of the simplicity depended on the arrangement of leads or looms from the magneto to the plugs. Old photos show elegant looms while modern practice sometimes looks like a bowl of upturned spaghetti.

    in reply to: Rolls Royce "R" Engine #931900
    powerandpassion
    Participant

    Peregrine

    Does anyone know the Perigrine firing order?

    RR Eagle (1917, planetary reduction gear) propellor RH tractor firing order is 1A,2B,5A,4B,3A,1B,6A,5B,2A,3B,4A,6B

    This is the same firing order reproduced on your suspect Peregrine engine plaque, so no doubt, as per previous correspondence, this comes from a RR engine.
    I understand the Peregrine was a development of the Kestrel, but also came in RH and LH tractor, to allow contra rotating propellors.

    By font and style, the plaque looks “1940’s”, certainly not RR Eagle
    So,you no doubt have a Peregrine engine plaque !

    Now, where have you put the rest of the engine !?

    in reply to: Can someone explain the process to "reply" to posts? #935313
    powerandpassion
    Participant

    Time out

    Hello:

    Thank you to those who have replied to my thread in the historic aviation section yesterday. Although I am a registered user and I do “log in” before attempting to reply to posts, this site has rebuffed all attempts I’ve made at replying. The FAQs section is of no help. Every time I try to just reply by typing my message and clicking “reply”, I receive an error message stating…”You do not have permission to perform this action. Refresh your page and log in”. But I am logged in! The FAQs section is of no help. And the site has no “contact us” link to talk with the folks who run this site, to obtain assistance! So I’m hoping someone can share with me whatever black magic one must know to successfully “reply” to existing posts on this site.

    Thank you in advance to anyone who responds with helpful hints to this inquiry. It’s not at all clear I’ll be able to convey thanks in reply to any information you provide.

    Swifter

    The computer servers hosting forums typically ‘time out’ at a predetermined period. Imagine if you are posting your reply then your kid comes up to you and complains that “all you do is sit in front of the computer on that bl*#dy forum”. So you get up to have a jump on the trampoline with your kid, then your foot goes through the springs and you go head over and snap your collarbone. The kid calls the ambulance and you go to hospital. Three days later you return to your place at the computer to complete your message. If the hosting server did not time out it would have kept a link open to your computer for three days, denying a link to other computers, or effectively slowing down the serving of information to other computers. The geek servicing the host computer reckons it takes three minutes to type a normal post, so allows three minutes of link before timing out your connection. The geek types at 234 words per minute while eating pizza, while the average forumite types 3 words a minute with their thumbs while being pecked on the back by kids or partners, so once you hit “post” you are typically no longer linked in and you get the prompt to log in again.

    Because each post I do is like Michaelangelo painting the ceiling of the Sistine chapel, I copy the text before hitting “post”, understanding that I have probably timed out while I have been squinting at and re editing my creation, and, even if the hosting server is set up to save or cache my unposted text while I go through the re-logging procedure, SOMETIMES IT DOESN’T, particularly with high bandwith items like attached photos.

    So, what works is :

    Reply to post
    Copy text using copy/paste function [highlight text with mouse then press Ctrl C (Copy)] before posting
    Try and post, you may be lucky and not timed out.
    If timed out, follow the prompt to log in again
    You may be lucky and the server has cached (saved) your post, go for it !
    If not Ctrl V (Paste) your text and post again.

    Often I have timed out and been grateful as it has prevented me from posting mad, bad and dangerous replies, so it’s not always a bad thing !

    Good luck and good posting !

    in reply to: Technote Vickers Potts Oil Cooler #936210
    powerandpassion
    Participant

    Oil cooler inlet & outlet tees

    Vickers Potts Oil Cooler inlet and outlet tee pieces are die cast aluminium components common to coolers used on Hart biplanes and Ansons.

    Does anybody have spare tees in a box?

    At this stage a low production run of tees can be accomplished via CNC milling from billet (no tooling) or single tool die cast, more work, more fun.

    in reply to: Technote Vickers Potts Oil Cooler #936226
    powerandpassion
    Participant

    Oil Cooler material specs

    Material specs for oil cooler

    Sources :
    [1] Vickers drawings 1927 via Pat 1968
    [2] Materials of Aircraft Construction FT Hill 1934
    [3] RAAF Fitters IIE 1943
    [4] Destructive test

    Brass fin pressings made from B12 [1] being Brass sheet, annealed, very soft for intricate pressings [2], 26 SWG [3], 18-24 tons max stress per sq inch [2] Cross section photo below shows pure copper rivets [1,4] used to join fin halves, bottom half larger than top half, bottom half lapped over and sealed with solder. Need to do oven tests to determine if this is Grade A (180 degrees C melt point), Grade B (205 degrees C) or Grade C 225 degrees C). Brass fin copper rivet heads sealed by additional solder. Whole assembly appears to be dipped in solder.

    Intermediate spacing rings made from L1 [1], being Duralumin, 17 – 25 tons max stress per sq inch [2].
    Proposed modern material 2024 T3

    NB – all joints between fins and spacers are metal to metal [3,4], no sealing compounds. Old coolers subject to brass ageing which will frustrate sealing as hardened metals will not seat into each other as effectively. Modern use of aged components may require modern seals for previously metal to metal contact surfaces.

    Connecting tubes given as mild steel [1,3] but tungum listed in oil cooler application in Tungum advertising in Aircraft Engineering. More logical than mild steel as Tungum has lower electro chemical corrosion potential than ms. Oil Cooler assembly of ms, aluminium and brass has large differences in electro chemical potential, setting up corrosion in the long term

    in reply to: Technote Vickers Potts Oil Cooler #936241
    powerandpassion
    Participant

    Avro Anson VP Oil cooler

    Avro Anson Vickers Potts Oil Cooler images attached.

    Hart biplane cooler (Air Ministry Type A 325 – 25 psi test pressure)
    Anson cooler (Air Ministry Type 802 or 826 – 90 psi test pressure)

    Data source RAAF Fitters IIE 1943

    in reply to: Some parts to ID please #939748
    powerandpassion
    Participant

    Big plug is ground services plug ? Holes around the circumference allow finger holds to pull plug out rapidly, when parafrags are dropping. HT and LT stand for High Tension and Low Tension for ignition system – would there be additional booster coils in a ground services cart ? British Beaufighter ?

    in reply to: Rolls Royce "R" Engine #939758
    powerandpassion
    Participant

    Best guess

    Hi all

    I would be most grateful if anyone could advise the firing order of the above engine as used on the Supermarine S6 racing aircraft please.

    Many thanks

    Best guess based on Flight Global ( great ,wonderful, generous people for digitizing historical publications free of copyright, thank you !) :

    Flight, Oct 2nd 1931, pg 989 – “the Rolls Royce Racing Engines” – description of R Engine in S6, establishing that Buzzard developed from R, photo shows S6 with airscrew shaft with RH tractor after drinking one or two beers, correct me if I am wrong.
    Flight, Nov 15th 1934, pg 1222 – “Rolls Royce Ltd” – description of Buzzard, Goshawk, Kestrel family, same family of engines as R was developed from Buzzard.

    R featured BTH SC 12 magnetos, same magnetos on Kestrel V, alternatively Watford (Rotax) SP 12 magnetos used, same firing order as BTH (hypothesis, but how could it possibly be different ?)

    RR Kestrel Handbook Series XXX October 1939 Fig 1. Diagrammatic layout of Ignition system where –
    Starboard (from rear) = A side
    Port = B side

    and

    (op cit) engine is RH tractor

    and

    Newnes Aero Engineering Vol III Kestrel V maintenance and overhaul :

    A1, 6B, 4A, 3B, 2A, 5B, 6A, 1B, 3A, 4B, 5A, 2B

    but

    RR Eagle & Falcon Engine manual Dec 1917 LH tractor firing order the same, A1, 6B, 4A, 3B, 2A, 5B, 6A, 1B, 3A, 4B, 5A, 2B
    (typo, should this be RH tractor or does RR Eagle planetary gear arrangement mean crankshaft RH tractor, airscrew shaft LH tractor?)

    and

    RR Merlin 32 Running notes 1942, airscrew shaft RH tractor (like S6), crankshaft LH tractor, firing order the same :
    A1, 6B, 4A, 3B, 2A, 5B, 6A, 1B, 3A, 4B, 5A, 2B

    Therefore hypothesis is that all RR V12 Eagle to Merlin, incl R engine, by virtue of V12 geometry and balance and RR workshop practice are the same.

    I note that in (a) collecting this information, (b) worse, knowing where I have filed it (c) being interested in recalling it and going through it to create the above correspondence I have now officially transformed into a propellorhead gunzl-tragic.

    Time to lop the cap off another beer.

    in reply to: Warbird Work Experience #943887
    powerandpassion
    Participant

    Welcome

    [QUOTE=jhoole94;2067608]Hello All!

    I’ve been a long time stalker of this forum, and have finally decided to take the jump and get stuck in!

    Josh, a great post and fantastic to see your energy getting injected into historic aviation.

    Like an old fashioned painter patiently copying an old master in a gallery to learn the art there are some mind numbingly boring things that you could do that might position you for the future :

    1. Metallurgy.
    Most historical aircraft performance development was driven by developments in metallurgy – stronger alloys to contain and direct more engine horsepower and lightweight airframe structures. You would find heat treatment shops and metal casting surprised and grateful to have interested labour in the shop. Rather than free work experience you might get paid to schlep in these environments but you will end up knowing more than most in historic aviation about what makes things work. Your career will develop at a time when replicas, by intent or the circumstance of originals shedding corroded DNA – airframes and engines- will constitute the only safe way for historic aviation to be in the sky. A good practical knowledge of metallurgy will allow you to navigate through future technical challenges. From my reading of aviation literature from 1918 – 1950, the dynamic metals industry always worked closely with aeroplane and engine designers to propose new possibilities and interpretations of aviation theory. The same dynamic will be necessary for reverse engineering antique components in the future.

    2. CAD drafting.
    The more fluent you are with something like solid works the more fluently you will merge into the industry. No doubt this is part of your course, but it will end up being more useful to you over future decades than anything else. To have a conversation and then output a technical drawing from it is an unsurpassed asset. You could thoroughly blow away crusty old types by showing them how to reverse engineer and rapid prototype casting molds for parts using 3D scanning, CAD software and stereo laser lithography or rapidly evolving 3D printers. To avoid egg on your face, your previous experience in a casting shop would make you understanding shrinkage factors in metal and what a useable casting pattern looks like.

    3. Preservation of technical drawings.
    The mind numbing task ordering boxes of old technical drawings, passing bits of paper through a scanner, labelling and indexing files is something you could do immediately that will be useful for decades to come. Both museums and collectors have boxes of stuff that will be ‘sorted some day’ but ends up inaccessible or lost. In performing this task you will find doors will open for you, but more importantly you will gain an understanding of a complete aircraft bolt by bolt and absorb by osmosis design philosophies and thought processes that put you in the mind of Geoffrey DeHavilland or Barnwell or Pollard who are the folk you really need to get to know. Do article searches on these type of names or the names on drawings you find on the Flight Global database and you will enjoy some of the greatest conversations across time, that will also inform your skills navigating through modern engineering problems in your day job. Get infected with their spirit and you will help sort out space tourism, sentient drones the size of a bee and maybe segue 1920’s aeroplane brake concepts into lightweight polymer electric vehicles.

    4. Be generous. Be the opposite of everything that frustrates you. Don’t give up.

    Hey, I have a job for you ! I am in Australia. I need someone in the UK to organise, collate and scan thousands of antique aviation drawings. Something to do during a semester break. It might take a few years, a few odd weeks per year. You need to walk in with a large flatbed scanner and scan. You need to be ‘in love’ with what you are scanning because otherwise the job is like breaking stones in a prison. If you are not in love with it, your curiosity will not drive you to ‘go the extra mile’ and unearth things that less excited folk say ‘don’t exist’ as code for ‘ I can’t be bothered’. It is amazing what is out there, it just needs a good digger. I will pay you a fish and chip shop holiday wage to do this, $20 Australian dollars per hour. You set up an Australian bank account under your control, email timesheets and I will pay into the Australian account. Timesheets don’t include travel time on the bus, and if you really amortized total time it’s better to get work in a garment shop in the subcontinent…there is a limited budget and this is really learning for you ! The reason for setting up an Australian account is that it works administratively here (business deduction) and that it will force you one day to come to Australia, spend the money, try and drown at a beach, get bitten by something, lager up and have a good time. Am I selling this to you ? PM for more.

Viewing 15 posts - 1,141 through 1,155 (of 1,241 total)