What can we do to help insure these wings are preserved?
Bill,
A great forensic analysis. Here is a picture of a flying Siskin III from 1927 :
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These wings are certainly a remarkable engineering dataset. Maybe, unless the structure that houses them is imperilled, they are safe where they are, in the hands of sympathetic, aviation minded folk. The spars are made of corrodible nickel chromium alloy steel, that would unlikely be safe for any future flying. They have lasted eighty odd years, shielded from the scrap man, sleet and snow. The most simple thing to do to preserve them is to attach a sacrificial aluminium or magnesium anode to the continuous steel structure, which would act in the same way as if the steel was sprayed with a zinc primer; a concept easier to grasp but less effective and undesirable from a preservation point of view. Sacrificial zinc anodes are used to preserve the hulls of century old steel ships in floating museums : this is a simple, cheap, effective way to make sure the roof structure will last.
Generally asbestos cement sheet absorbs some moisture and you would expect that the corrodible steel would be in poorer condition from being pressed against this. I wonder if there is some strange circumstance where the galvanic potential of asbestos cement and steel makes the cladding act as a sacrificial anode ? There also seems to be some furnace flue in the building : generally combustion puts a lot of moisture in the air but has the heat of this discouraged condensation on the underside of the roof? Whatever the reason it is amazing to find bits of Siskin III. It is amazing what is still out there.
This roof contains some secrets that could be gleaned without any needing to remove them :
1) Confirmation via metallurgical testing that the spars are DTD54a Nickel Chromium alloy and the bracing struts are 3% Nickel alloy T5 tube and the ribs are DTD98 or DTD99 Nickel Chromium alloy.
2) Confirmation of the gauge of these materials.
3) CAD drafting of the wing assemblies, showing details of assembly/riveting/support structures that may be missing for remnant drawings or be production improvements not detailed in remnant drawings.
A flying Siskin would have to be made from new materials – the fuselage was made from pin jointed T5 tube? At first glance these structures seem complex to an eye more used to monocoque structures, but they lend themselves to simple tools and a patience. Canadians are used to shovelling snow from driveways, so have the mindset! I understand there are a few AS Jaguars floating around – it seems that the plethora of AS Cheetahs can allow a far more simple step into this type than if a Bristol Jupiter were required.
The Canadian Siskin seems to occupy the same place in the history of the RCAF as the Hawker Australian Demon in the RAAF. Both are largely missing in their respective skies and both caught the imagination of their respective populations in prewar air displays. In a time of Depression they were an extravagant spend. By 1940, they were an embarrassment, which is perhaps why they were so readily scrapped by those who had progressed to Mosquitos and Spitfires. A flying Siskin in the UK would be good, but a flying Siskin in Canada would be a profound achievement for Canadian aviation history. So if anybody is going to do it, it might have to be a Canadian.
What’s stopping it is the lost art of strip steel construction : the DTD54a spars, the pin jointed T5 tubes of the fuselage which make it such a different proposition to a timber or monocoque aluminium restoration. When you look at a snow covered driveway it is disheartening. The only way to get to the finish is to just start shovelling ! So here is a hint : the T5 tube of the late 20’s and 30’s has the same characteristics as T45. Ostensibly it was a 50T tube but it never seemed to make this spec and was always regarded by the stressmen as a 45T tube. In order to get a real 50 T tube 3% Nickel alloy tube was developed in the 30’s with a true 50T strength. You can get T45 today so there is enough historical literature to get the concept of a T45 fuselage frame together without controversy. Its all tube with machined joint fittings. Then stick one of your Jaguars on the front and you are on your way ! It seems that there are wing remnants around which, if the custodians were sympathetic, you could survey to start building an understanding of what is required to build the wings. Really you need to find somebody with a coil of DTD54a Nickel Chrome spar material of the correct gauge – so what is the gauge? The coil might be available but a shame if a 1,000 m coil is run and the opportunity to output 100m in a gauge suitable for Siskin is lost, because I doubt it will ever be done again.
Have you seen GR Quick’s superb GA of the Siskin III :
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Thank you. Quite a remarkable document to put into storage – is there some way to verify that it exists and can be accessed ?
I have discussed the matter with someone who interviewed Jim Carmichael (Can Car) on this very topic. When asked what CC&F used for their Hurricane production, his answer was “whatever we could get our hands on”, which turned out to be 4130 as a substitute for the T.50.
A fascinating anecdote which would explain many questions, and of course to find some original documentation to verify this would be gold.
Where in the US or Canada could you buy cold drawn aircraft tube from in 1940-1 ?
Does this mean you’ve tested the piece of centre section spar that I sent to you?
Ron, indeed the section was tested in June and results posted on #23 here :
http://forum.keypublishing.com/showthread.php?129241-Hart-Hind-Bulldog-Wapiti-Atlas-Siskin-Hurricane-amp-others-steel-testing&highlight=
I try and post up results as soon as I can on the forum to make this information available for all – as a simple courtesy I reflect I should have directly contacted you at the time to let you know this information was posted and I am grateful that you sent the sample in. Often I find that testing creates a whole new range of questions and it is this sample that has opened up the material substitution line of query for CCF Hurricane, so a very valuable piece of metal carrying an interesting mystery.
Ed
Ian,
I have access to a Hurricane I Repair & Maintenance AP which predates CCF Hurricane X. In the case of repairs to centre section spars, made from BS S88c nickel chromium alloy, repair patches of S88c or DTD 166 stainless (same material used in the fuselage fish plates) are specified.
I have also tested known CCF Mk X centre section spar remains which report manganese alloy (DTD 138) spar booms, obviously different to the British made aircraft using nickel chromium booms (S88c). Subject to confirmation, the theory is that CCF used local materials for Mk X that were different to materials used in the UK. The link to your question is whether a RCAF AP would specify DTD138 for centre section spar boom repairs, which would be delightful to confirm, or a later RAF AP covering Mk X would do the same.
In thinking through this information I have the following reflections :
Repair & Maintenance APs were practical documents focused on the quick return to air of battle damaged aircraft. Therefore materials reasonably at hand of a repair unit would be specified. The great advantage of DTD 166 was its presentation as sheets of work hardened material with a strength of 50T minimum that could be work hardened to 65T and used to repair a wide scope of the Hurricane structure. I have seen in lists of equipment for Maintenance units dealing with Hart biplanes in the 1930’s in Iraq sheets of DTD 166, and it can be defensible to accept that this practice continued with the Hurricane, as the argument in the buildup to 1939 was there were trained fitters for this type of aircraft and they should be built in preference to the monocoque aluminium Spitfire types. There is no mention of sheets of S88c, which is a corrodible material which can only be supplied as heat treated coil, far less practical to a front line maintenance unit. I draw the conclusion that repairs using S88c where based on salvage material from written off aircraft.
To introduce a new material, DTD 138, into the mix would be an unwelcome complication in procurement and engineering management. It would make more sense for a CCF Mk X to be repairable with DTD 166 or salvaged S88c. They key is the performance values of this material, in that work hardened DTD166 would aquire strength values of 65T, in common with 65T S88c and 65T DTD138.
Where CCF did re-engineer the Mk X Hurricane structure, they would have taken care to meet the same strength values using DTD 138 as the original S88c. In other words spars would be absolutely interchangeable, and there would be no complication in a frontline maintenance unit in blending CCF parts with UK parts. In this respect the simple solution would be to allow the maintenance unit to rely on existing APs, without confusing them with questions about materials. If this is true then no maintenance AP will come to light that specifies DTD 138, though in the literature of the 1930’s DTD 138 is listed as a typical spar material.
I think today, that most folk would not recognise the use of DTD 138 in Hurricane construction. If the logic stands, that it is directly interchangeable with materials more commonly understood to be used in Hurricane construction, then it is largely just a curiosity. It does suggest, however, a considerable effort to re engineer the Hurricane structure in Canada that would be a fruitful body of work to rediscover. Consistent with this are the use of SAE 4130 spar liner tube in the CCF product rather than 3% nickel alloy T50 in the UK product and United States sourced EN 8630 nickel-chrome-moly fuselage tubes in the CCF product rather than 3% nickel alloy T50 in the UK product.
This is an example of wartime substitution which could greatly inform future restoration work concerned with strip steel and pin jointed construction. Clever Canadians.
Wulfie,
You included some extracts of what looks like a history of BP. Is it possible to have a complete copy? Very interesting reading!
One insightful journalist wrote recently that “the 21st Century is falling into place around our heads”. So much as Museums and restoration agendas make sense to children of the 20th Century, so the Museum in one hundred years will reflect the themes of this new century. I can sense the following :
1. The revitalization of Chinese, Indian and Japanese Museums as history becomes a tool justifying current readjustments in global affairs led by the resurgence of China. So as Anglophone Museums may wither, dynamic, New Museums with budgets will draw airframes and well renumerated staff from the Old to reinterpret the New. You may not like the New!
2. The Drone will become the most contentious display of the 21st Century Museum. It represents a failure of Anglophone imagination and thus it will become the principal display in any Museum wanting to diminish Western ideas. “They slaughtered us with These so they could keep Shopping.” Some young person will throw red paint on a drone display in the West and elderly Machine Centric Museum trustees will shake their heads and a further gap will open up between dusty displays and young people choosing to do other things. One rebel Museum in the West with no budget will display a drone with Wikileaks footage showing wedding parties being shredded but there will be queues to get in. I hope drone pilots do this because I already shudder to think about how abandoned they will be by Governments and Us once they wash out. There will be a need for a Truth and Reconciliation Drone Museum to at least help them avoid becoming the 21st Century’s marginalized Vietnam Vet. This Museum might also examine the successful use of airpower in Policing by the RAF in the 1930’s, when leaflets were dropped on Day 1, if no luck after 2 days, crops were set alight, if no luck after 2 days precision strikes were made on hold outs who had one week to get their women and children out of the way. Then the 1930 RAF Policing budget will be compared to the 2015 Drone budget and an Effectiveness analysis made. Do the same for Hitler’s Vengeance drones, the V1 and V2, which were at least honestly described by that government as devices of Terror. So we need a Hawker Hart biplane next to a V1 and Predator Drone and documentary interviews with drone strikers and survivors. A conversation, measured, confronting, indignant, chilling. No Museum will get more press coverage. It’s really about People applying technology, not the technology. Drones are the future, but test your ideas: how do you want your children or grandchildren treated by them in the 21st Century? The drones are coming. So give me a Museum that is about the future.
3. To the unborn, a Defiant, Spitfire, Hurricane, ME 109, BF 190, Mustang and Wildcat, as preposterous as it will be to the 20th Century student of the art, be look-alike monoplanes with dangerous paddles out the front, used in a world war which may have started in 1860 something, or 1933 something or 2002. History tends to compress. You might not know the difference between a 16th Century Portuguese Caravel and an 18th Century Man-o-War; they are all wooden boats with sails, but upon this technology great themes and Empires evolved. So certain aircraft types will travel into the preposterous future : The Spitfire versus the Stuka, the Mustang versus the Zero. Only because biplanes look different the Camel will not be confused with the Hurricane, although the short twenty years between them will invite abbreviation in future conciousness. The Youngsters of the 21st Century may be forced as school children to march through caverns of this stuff in dark Museums peopled by cranky, wrinkly, disapproving creatures. This will be caused by Museums thinking that it is their job to preserve Machines, and that Machines speak for themselves. One or two Museums will adopt Plato’s motto : “He who does not know what has come before him, will forever see the world as a child.” They will accordingly make their displays about People, so a young person can say “ That Person in the Display could be me.” So a display about a Pilot, preferably a young pilot who dies for their country and why, will make the Machine that remains start to speak. Museums will cross promote with Movie Makers, to have Blockbuster displays timed with the release of Movies about People in Machines. These Museums will be 80% storage and restoration, with 20% on display, display 100% rotated every six months based on themes about People. They will use shop display professionals to set these up, not cranky old goats. Really, many Museums are Men’s Sheds, which is not a bad thing, as long as the Men’s Shed doesn’t overawe the Museum. Because Museums are so badly led, they end up being dependant on free labour, being Old Goats, but nothing is free, and the Old Goats can mist over an organisation with other forms of compensation that turn it into a Goat Fiefdom. That’s OK in the storage zone, but the Shop Front and direction must absolutely be the domain of Young Roosters.
4. The day of Gloomy Museums having a monopoly on machines will, thankfully, pass. Modern manufacturing productivity improvements, aged metallurgy and keen people will make things fly, even if there is not an original rivet in it. So the Flying Museum will flourish and the Dark Cavern with Barriers will sink further into the gloom. The Flying Museum will negotiate tax arrangements to make it attractive to donate your aircraft in when you are ready to hang up your helmet. The Flying Museum may be virtual : it may simply be a network of individual aircraft owners who ‘flash mob’ a particular airfield at a given moment. The Flying Museum will offer vocational training courses to young people who leave school early, to teach them about engine rebuilding, welding, the English wheel. The Flying Museum will once a year do cross country flights and beat up small towns and land at a local airfield and set up a tent with displays about People and Machines. It will research ahead and find out that someone, totally forgotten, born in that small town flew in this Machine and died aged 21 in France in 1940. It will offer paid flights and change lives. The first woman on one of Jupiter’s moons will first take her first flight in a Spitfire flown by her great grandmother in a Transport Squadron.
That’s probably enough controversy for one post!!
Wulfie, it’s arrived ! On the custom’s declaration it says “Fragment of crashed aircraft in biscuit tin”. What there is, instead of biscuit, is the Faberge egg of strip steel construction, real B&P spar, something I thought I would never see in my life, remarkable! Thank you. I will subject it to all sorts of metallurgical testing indignities and report back.
Congratulations Matt, a remarkable insight and breakthrough. Probably too obtuse for most to understand, but then I don’t understand dark matter, E=MC2, and why the missus would rather sit on the beach rather than dig through mud for corroded aeroplane parts.
I wonder if you could crowd source more data by making up a downloadable Beermat-o-meter or diagram showing key dimensions that would allow folks on the other side of the planet to feed back ‘apples with apples’ data to support your insight ? Maybe like a stick of a fixed dimension that is laid against the blade root with adjustments for different shank sizes, marks for measuring key blade dimensions and a red letter warning : “Are the magnetos isolated?” Probably also one of those stickers with a human figure getting chopped in half with a prop blade, to avoid litigation, in case a wit becomes a half wit.
Thanks, mate. I will call E today!
No worries – I understand how all this prop stuff is like sailing through mist, blurting on the fog horn, and then suddenly you come out into sunshine, then mist again !
I sense that the nomenclature was overtaken by wartime invention and events, and those that were concerned with these things probably thought they could tidy it all up ‘after the war’. Then jets came in and there was no time or reason to conduct such an exercise, because all you really needed was to consult a chart that showed aircraft and indicated the appropriate prop/blade, why would you need anything else ?
HS certainly invested in a parts numbering system and parts catalogues that are brilliant in their structure, clarity and detail, but not ‘why’ that number.
One way to sort this out is to invent the Beermat-o-meter, the analogue version being a stick with suction cups which allows you to lay it along a blade and pickup key characteristics with cardboard templates at ‘standard’ stations. This will require dealing with stepladders and clucking and disapproving museum folk as you travel the world building up the definitive database of blades. The digital version could be one of those laser scanners that connects to an iPhone, that will allow you to capture blade models from a distance, maybe putting little dots at stations to allow comparisons, the Beermat-o-matic.
I would buy a copy of Beermats Bible, once it is published, the definitive reference source for blades and the aeroplanes they were used on, and why.
Thank you, very much looking forward to it.:eagerness:
While the pattern maker looks at the main wheel I thought I would wander up the back and look at the Mosquito tailwheel assembly.
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Disconcertingly, the whole thing is made out of magnesium. I always thought the tail wheel fork was a steel forging, surely with all that weight bouncing through a cantilevered beam design. But no the whole thing is magnesium, the whole assembly surprisingly light for all the volume of air it displaces.
When you squint at it from a distance the tailwheel assembly looks to be in reasonable condition, but when you peer in close the rot becomes apparent. The surface of the magnesium is pocked with corrosion and could never reliably be used in service. I think is impossible to ever find an airworthy piece of this magnesium assembly. Looks like the pattern maker will be busy.
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I understood that one of the faults of the Mosquito was the failure of the tailwheel hydraulics, in that the tailwheel would not come down and there was no indicator in the cockpit to alert the pilot. To deal with this on operations the tailwheel was left locked by the fitters in the down position at all times. When you look at old photos of Mosquitos in flight, the tailwheel more often then not is swinging in the breeze.
When you look at the hydraulic ram that actuates the tailwheel it is quite small. I would understand if the tailwheel assembly had some steel components that it might prove too hard for this ram to actuate it up, but surely the weight would help to actuate it down ? Now that I can lift a magnesium assembly in my hands it is remarkably light. Perhaps this was just a design fault, with a hydraulic device far from the engine driven pumps, losing pressure through the distance and restriction of supply lines routed from the cockpit selector valve. Without putting a great deal of effort into tracing the valves in the system, I would assume that the valving would favour the mainwheels first, and if there was some loss of pressure from leaky mainwheel rams, then supply would never get to the tailwheel.
Back to magnesium. It seems that the whole Mosquito sits on magnesium hooves. While I wheely don’t want to go round and round deflating folk by rolling over the tyred ground of magnesium in antique aeroplane structures this subject could puncture your enjoyment of historical aircraft or even bring it to a skidding stop….
Here is one little study that deals with stress corrosion factors in magnesium wheels, most often used in racing cars :
https://lra.le.ac.uk/bitstream/2381/8920/1/final.pdf
Interesting on the tail wheel assembly are heat treatment marks and X-Ray inspection marks.
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While it is par for the course today that a new casting is inspected by X-Ray and other processes today in search of porosity and flaws it is interesting to see a confirmation of this process used 70 years ago, either as a manufacturing inspection or part of a service overhaul. While it seems self evident in magnesium casting that these processes would have been followed these evidentiary marks on parts and process descriptions in maintenance publications for British aeroplanes are generally omitted, because, I think, the authors deemed them self evident or unnecessary to know for ‘throwaway’ parts. But these authors and technicians are now gone, and with them the confidence of invention. Children unborn will be dealing these antique structures in thirty years time and that think magnesium is only found in sports drinks. So it’s better to overcompensate with information, methinks.
No wonder the Mosquito burned when it bellied and burned. Not only timber and petrol but big chunks of rubber and magnesium for mainwheels sitting under the engine oil tanks, and a nice chunk of magnesium and rubber for a tailwheel.
Wulfie,
Sidestrand brochure strapped to leg of pigeon winging its way over to you – you have PM
Wulfie, did the beautiful, rare, expensive, original brochure sent in trust for your Museum display arrive ? No PM reply from you!:apologetic:
******** if I know
Matt, I would make the following observations :
a) The missus is quietly relieved that you wake up muttering ‘thickness to chord’ rather than the 23 year old secretary’s name at work !
b) ‘Thrusting Forward’ might be worth chasing up to gain insight into the didactic of blade development. Described as a ‘Detailed account of the development of the Aircraft propeller; published by Hamilton Standard to commemorate their 50th anniversary in the manufacture and development aircraft propellers’.
c) I understand that deHavilland’s were a licensee of HS, and that Mr Hamilton himself was resident in Paris and concluded this arrangement. In the build up to war, the Air Ministry and dH would most likely want to adapt HS systems without becoming bogged down in reinventing parts or systems. From looking at dH Australian manufactured prop parts the part numbers are identical to US HS part numbers, so dH Aust, it seems, entirely adopted the HS parts numbering system. Therefore dH parts are HS parts, therefore design factors are HS design factors. I understand that dH GB, in seeking to describe a whole airscrew system with an ‘Overview’ number, sought to classify this through a separate British 5 number system that made more sense to them rather than adopting the US HS ‘Overview’. I understand you are seeking a logic that connects the dH GB Overview number with a design decision made by a US designer perhaps years before.
My gut feel is you will find some pieces of logic that support your hypothesis, while some drive you to drink. I think the times were so chaotic and urgent that pieces of technology were grabbed and adopted without waiting for the nomenclature to catch up, eg changing over 2 bladed Hurricanes to 3 bladed Hydromatics within ‘weeks’ during the BoB. In my own researches into Mosquito blades I have finally found that the blade selected by those perennial scavengers in the dH design office was originally designed by HS for a radial P&W 1830 engine. So how do you rationally incorporate blade design factor nomenclature for a prewar 1830 radial into a twin V12 design on the other side of the planet ? Probably by going to a pub and throwing a dart onto a board to come up with a number.
Anyway, here are some charts with some data such as ‘Activity Factor’ which I know nothing about, that might start to form some logic threads, maybe….Sorry it’s all Hydromatic :
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Fire in the hole
Anthony,
Don’t know if this is a A27N/106 mounting bracket but here are some pics of an old school Graviner automatic fire extinguishing system :
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Bottle contains methyl bromide which is still used today to fumigate shipping containers. It is basically a very heavy gas that displaces air and ‘suffocates’ fire. The bottle in the photo is actually still full so quite an uncomfortable thing to handle with it’s 70 year old seals. Below is a empty bracket, WW2 vintage.
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The other elements of the system are the flame switch normally situated on the firewall, and an impact or gravity switch which is the analogue equivalent of the modern day impact switch triggering the airbag in your car.
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There are earlier brackets for 1930’s type handheld extinguishers, which were sometimes activated by a cable pull system.