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-   -   Dornier DO 31 (https://www.pprune.org/military-aviation/514043-dornier-do-31-a.html)

althenick 4th May 2013 19:00

Dornier DO 31
 
An interesting way to use Peggy Engines ....


Dornier Do 31 - Wikipedia, the free encyclopedia

I wonder what this Aircraft could have done with the final variant of the Pegusus Engine to power it.

What do you Engineering types think?

LowObservable 4th May 2013 19:23

My guess would be "carry a Smart car 150 nm and deafen everyone for two miles around".

SammySu 4th May 2013 19:59

Or with 4 x 23500lb podded Pegasus rather than 2 x 15500lb versions and 8 4400lb lift jets, much more thrust, much less drag which I think was the technical problem first time around.
Would also benefit from modern FCS technology for simple transitions as per the VAAC Harrier and subsequent F35 control laws.
Wouldn't be Stage iii compliant though :D

Davef68 4th May 2013 21:12

Or the Fairey Rotodyne witrh Pegasus rather than Ellands....

JFZ90 4th May 2013 21:25

i assume another issue was that a single pegasus engine failure was presumably catastrophic in several parts of the flight envelope. just about tolerable with a harrier, but not normally ok with something that could carry pax. i guess the 2 front seats were martin baker?

BEagle 5th May 2013 06:26

I remember seeing (and certainly hearing!) the Do-31 at the 1969 Paris Air Show. That was the 10-engined version which was capable of VTOL flight and it demonstrated its capabilities most impressively!

Visit the Dornier museum at Friedrichshafen and you can see the Do-31, together with many other rare Dornier designs.

But not the Do-217 or Do-335.....:\

Chugalug2 5th May 2013 09:10

This was the one that the MRT Force was waiting for in the 60's. Waiting and waiting...
Armstrong Whitworth AW.681 - Wikipedia, the free encyclopedia

barnstormer1968 6th May 2013 10:06

While we are looking back at old VTOL contenders, or equipping old models with new engines, could we poke the French to making the 'Rafale son of Balzac' (sp)

It was fast and looked good in its original form IMHO

John Farley 7th May 2013 15:54

Sorry chaps the notion that old jet VSTOL contenders failed just because they were short of thrust is too simple. They all had problems with one or other of these things (sometimes both).

1 There was no provision for keeping the hot efflux out of the intakes.

2 The lift systems left little room for anything else.

Putting more thrust in to such designs would not have helped and with some aircraft (D031 for one example) would have made matters worse.

GreenKnight121 7th May 2013 23:17

Or the Breguet Br.1030.
http://www.secretprojects.co.uk/foru...772.0/all.html

Planned test aircraft:
http://i22.photobucket.com/albums/b3...psa29b9132.gif

Intended transport development:
http://i22.photobucket.com/albums/b3...ps61b15d3a.gif
http://i22.photobucket.com/albums/b3...ps78f38844.jpg

Rigex 8th May 2013 09:09

Do-31
 
In addition to Beagles find, there's another (which you can walk through) :) at the Deutsches Museum collection at Oberschleißheim near Munich.

Also look here:

Deutsches Museum: Oberschleissheim Airfield, Information

sisemen 8th May 2013 09:18

Just another one of those crazy ideas that abounded in the aviation world post-war until the design teams started to settle down.

Chugalug2 8th May 2013 10:04

I don't think they were crazy, sisemen, simply trying to satisfy their prospective customers demands. Their customers anticipated a war in which the first targets would be every single runway, military and civil. Bristol Engines and Hawkers came up with a solution, but that created its own re-supply and support problems. These various transport projects sought to satisfy that demand, though I grant with varying degrees of reality.
Did you know that the TSR2 was to be VTOL enabled with a Shorts VTOL airborne aircraft carrier? Now that was crazy!

Engines 8th May 2013 20:28

John,

Nice post as ever.

If any visitors would like to find out more about the various V/STOL ideas tried, a good place to start can be found at Vertical and/or Short Take-Off and Landing (V/STOL), where you can find the quite wonderful 'V/STOL Wheel'. It shows no less than 45 ways of trying to do what Hawkers achieved with the Harrier.

If nothing else, it should give anyone a better appreciation of just how good those designers, engineers and pilots at Kingston (and Bristol) were.

Best Regards as ever

Engines

dead_pan 8th May 2013 22:00


'V/STOL Wheel'
Excellent, although have they missed a few off e.g. stop-rotors?

Didn't know the Rotodyne had tip jets. A bit before my time.

sisemen 9th May 2013 02:08

I guess what I meant by 'crazy' was the 'pushing the envelope' think tank mood which was exploring the options until the inevitable dead end hit them. You only have to look at the list of weird and wonderful projects and prototypes that abounded in the latter stages of WW2 and the immediate post-war period. Once the dead-ends had been sifted and sorted it kind of settled down into a conventional design paradigm with the occasional "outside the square" advance.

althenick 9th May 2013 10:59

Thanks for the link Engines. I never realized just how many VTOL Designs were out there - and also how many of them relied upon Rolls Royce to power them! I'm a big fan (Sorry for the pun) of Not reinventing the wheel and as such I think Rotordyne should be revisited. Whould an updated design of this Aircraft really need Tip - jets?

Al

dead_pan 9th May 2013 19:09

According to Flight a week or two ago, the departing head of Eurocopter predicted a rennaisance in helicopter travel, citing new, faster & lower operating cost developments based on their X3 design, whose lineage you can trace back to the Rotodyne. As always I suppose it was an idea ahead of its time.

Engines 9th May 2013 20:01

Athelnick,

In my view, yes, an updated Rotodyne would still need tip jets, because that gave it the very low weight, zero torque rotor propulsion system it needed. No gearboxes, no transmission shafts - just hot gas ducts from the two turboprops in the wings.

That said, Fairey had big problems with the stainless steel ducts, which had to double as rotor blade spars. The other big issue was noise from the tip jets - but they were a long way down the track of a silencer design.

I actually watched the aircraft land at Battersea Heliport - and it was VERY loud.

Best Regards as ever

Engines

BEagle 9th May 2013 20:13


I'm a big fan (Sorry for the pun) of Not reinventing the wheel and as such I think Rotordyne should be revisited. Whould an updated design of this Aircraft really need Tip - jets?
JF and I disagree (politely) about the Rotodyne, which is often accused of having been 'too noisy'. The first prototype was certainly pretty noisy, but huge advances were made throughout the latter days of the project and considerable noise reduction had been achieved. When it flew to Battersea Heliport, there were NO noise complaints, just a few curious enquiries as to what was going on.

The Rotodyne did not need massive helicopter transmission systems and only operated in tip-jet mode for vertical take-off or landing. For the rest of the flight, the rotor operated in free-wheeling autogyro mode, with additional lift from the stub wings which housed the main engines - another source of programme delay, courtesy of Napiers.

Just as the production version's specification was being signed-off, the much-underrated Rotodyne died under a Conservative government several years before Wilson and his fellow-travellers killed TSR2, HS681 and P1154. A pity; had it been developed than the Rotodyne could perhaps have been a pioneering inter-city airliner and military transport

Nowadays you'd have to find a 'killer application' for the Rotodyne to be resurrected and there simply doesn't seem to be one.

It was certainly more viable than the Do-31.


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