Axial Flow Supercharger
#2651
what type of word processing software do you have?
word perfect?
what about power point??
If not I will print out what i have and send you a letter via your return info from my SS box.
word perfect?
what about power point??
If not I will print out what i have and send you a letter via your return info from my SS box.
#2652
You will probably have to send the letter as RP broke is poor puter and has yet to fix it. There are about 10 pages of this thread, way back somewhere, dedicated to trying to help get his computer fixed haha.
#2653
Hey Richard,
Did you realize that if you get this supercharger running that you partially getting to work what Rolls Royce patented about 10 years ago? (Not that this would get you in trouble by any means, but it's interesting nevertheless.)
They patented an aircraft engine where a rotary engine drives an axial flow compressor and the exhaust gases drive an axial exhaust turbine which drive a fan.
Of course the size of the turbine blades compared to the engine are completly off and the power density of an actual turbofan could never be reached, but it must have been patented by Rolls Royce for some reasons.
Did you realize that if you get this supercharger running that you partially getting to work what Rolls Royce patented about 10 years ago? (Not that this would get you in trouble by any means, but it's interesting nevertheless.)
They patented an aircraft engine where a rotary engine drives an axial flow compressor and the exhaust gases drive an axial exhaust turbine which drive a fan.
Of course the size of the turbine blades compared to the engine are completly off and the power density of an actual turbofan could never be reached, but it must have been patented by Rolls Royce for some reasons.
#2654
Originally Posted by globi
Hey Richard,
Did you realize that if you get this supercharger running that you partially getting to work what Rolls Royce patented about 10 years ago? (Not that this would get you in trouble by any means, but it's interesting nevertheless.)
They patented an aircraft engine where a rotary engine drives an axial flow compressor and the exhaust gases drive an axial exhaust turbine which drive a fan.
Of course the size of the turbine blades compared to the engine are completly off and the power density of an actual turbofan could never be reached, but it must have been patented by Rolls Royce for some reasons.
Did you realize that if you get this supercharger running that you partially getting to work what Rolls Royce patented about 10 years ago? (Not that this would get you in trouble by any means, but it's interesting nevertheless.)
They patented an aircraft engine where a rotary engine drives an axial flow compressor and the exhaust gases drive an axial exhaust turbine which drive a fan.
Of course the size of the turbine blades compared to the engine are completly off and the power density of an actual turbofan could never be reached, but it must have been patented by Rolls Royce for some reasons.
I had not heard of this before. I can't make out how the rotory engine fits inside the turbofan in that drawing but I'd sure like to see the whole paper. How do you get that from the net? If you can.
#2655
Go on:
http://free.patentfetcher.com/Patent-Fetcher-Form.php
Type in the patent number:
5692372
Then click on: Fetch
(Make sure that you have a PDF Reader installed).
http://free.patentfetcher.com/Patent-Fetcher-Form.php
Type in the patent number:
5692372
Then click on: Fetch
(Make sure that you have a PDF Reader installed).
#2659
It is a turbofan engine. It substitutes the combustion chamber with 3 rotary engines to apparently reach higher efficiencies.
If you take off the axial flow turbine and the fan, it's basically a rotary engine with an axial flow compressor. That's why I mentioned it.
Also, if you read the patent you'll notice that NASA apperently worked on a similar concept in the 70's. So it's not a completly new idea.
If you take off the axial flow turbine and the fan, it's basically a rotary engine with an axial flow compressor. That's why I mentioned it.
Also, if you read the patent you'll notice that NASA apperently worked on a similar concept in the 70's. So it's not a completly new idea.
#2660
nice find
depending on the axial compressor would the rotary need to spinn at very high speeds 20000+ RPM.
Thats one of the main things I love about rotary engines there is allmost no max operational limit.
depending on the axial compressor would the rotary need to spinn at very high speeds 20000+ RPM.
Thats one of the main things I love about rotary engines there is allmost no max operational limit.
#2662
I have your study and I must say you spent some time thinking and drawing. I could use that energy myself. Anyway I think you invented the turbocharger except you replaced the shaft with a hydraulic pump and motor.
Yes it could work but would be alot of extra equipment and money.
Hyd pumps are very heavy because they make lots of pressure. Ditto the motor. Cast iron with steel rotors.
If you want to think about something try a high pressure axial flow compressor that lets it fluid expand in a turbine that then drives a centifugal compressor or another AF in series with the first for very high boost applications like tractor pullers. Say 100+ psi or Pr of 7 or more.
Still I like the effort. You might try some of those things on the goverment for a grant. If I could do it right I would present them something. Just have to know the BS to print with it. Read some of the grants they have given and you'll get the idea. How about a spherical piston? Got a patent on it too. How stupid do you have to be??
Yes it could work but would be alot of extra equipment and money.
Hyd pumps are very heavy because they make lots of pressure. Ditto the motor. Cast iron with steel rotors.
If you want to think about something try a high pressure axial flow compressor that lets it fluid expand in a turbine that then drives a centifugal compressor or another AF in series with the first for very high boost applications like tractor pullers. Say 100+ psi or Pr of 7 or more.
Still I like the effort. You might try some of those things on the goverment for a grant. If I could do it right I would present them something. Just have to know the BS to print with it. Read some of the grants they have given and you'll get the idea. How about a spherical piston? Got a patent on it too. How stupid do you have to be??
#2664
Is the axial turbocharger (direct drive shaft from axial expansion turbine to axial compressor turbine) feasible depending on the exhaust turbine material.
Might be worth looking in to in the future.
When I get board at work (R&D) my mind tends to think about these things.
Might be worth looking in to in the future.
When I get board at work (R&D) my mind tends to think about these things.
#2666
Originally Posted by deppenma
Is the axial turbocharger (direct drive shaft from axial expansion turbine to axial compressor turbine) feasible depending on the exhaust turbine material.
Might be worth looking in to in the future.
When I get board at work (R&D) my mind tends to think about these things.
Might be worth looking in to in the future.
When I get board at work (R&D) my mind tends to think about these things.
Yes, it's been done. Sorry. The thing that hasn't been done is the expandable air to start with. Just never gonna get that perpetual motion machine done no matter what I try.
Anyone out there invented the breeder reactor yet? Or cold fusion?
#2669
Originally Posted by deppenma
Is the axial turbocharger (direct drive shaft from axial expansion turbine to axial compressor turbine) feasible depending on the exhaust turbine material. Might be worth looking in to in the future.
And ABB makes turbocharger with axial flow turbines:
#2670
yes axial compressor but the exhaust side looks like the standard designs of today.
I was looking for a turbo like setup but with both sides being an axial flow compressorand axial flow expansion turbine.
I was looking for a turbo like setup but with both sides being an axial flow compressorand axial flow expansion turbine.
#2671
Originally Posted by deppenma
yes axial compressor but the exhaust side looks like the standard designs of today.
Originally Posted by deppenma
I was looking for a turbo like setup but with both sides being an axial flow compressorand axial flow expansion turbine.
With an axial compressor in a turbocharger you'd need several stages in order to reach the same pressure ratio as with a single radial compressor wheel. It would make it more complicated and increase the rotational mass and you'd end up with a giant turbohole.
Last edited by globi; 01-18-2006 at 09:22 PM.
#2673
At least if you read, you don't necessarily end up repeating errors or develop products others came with already.
Besides I don't know whether this is the actual reason why we don't have axial flow compressors in turbochargers. So I can only guess, but this is how I would explain it.
Also last year was the centennial of the turbocharger, so many people probably read about its invention anyway - after all pretty much all ships, trains and trucks are fitted with turbochargers.
Besides I don't know whether this is the actual reason why we don't have axial flow compressors in turbochargers. So I can only guess, but this is how I would explain it.
Also last year was the centennial of the turbocharger, so many people probably read about its invention anyway - after all pretty much all ships, trains and trucks are fitted with turbochargers.
#2674
With the better picture now I see what you were talking about globi.
I thought axial flow compressors were more efficent than a radial compressor wheel. Hence this project to develop an axial flow supercharger.
I thought axial flow compressors were more efficent than a radial compressor wheel. Hence this project to develop an axial flow supercharger.