![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#12
|
|||
|
|||
![]()
Recently, Larry Dighera posted:
On Tue, 07 Aug 2007 17:51:27 GMT, "Neil Gould" wrote in : Recently, Larry Dighera posted: [...] I'm thinking there would be necessity for some means of conducting the heat from the engine to a remote heat exchanger, and the resulting complexity and weight increase would negatively impact the potential advantages of a Stirling aviation engine. In any event, in addition to the Stirling engine and its fuel, a heat exchanger of some type needs to factored into the weight, cost, performance, and efficiency equations. Of course, but I don't see a lot of reason why that couldn't be incorporated into the overall design. My point is that heat exchangers need not be heavy, and could probably double as structural and/or aerodynamic components, further reducing (and possibly enhancing) their impact. How would you get the heat from the Stirling engine to the heat sink? If you use liquid coolant, it would be heavy and prone to leaks. I'm not a Stirling engine designer, so I can't answer that factually. I have been reading up on it a bit since the article was referenced in this thread, but I haven't seen such things as the required rate of dissipation for the engine to work efficiently. If the heat sink needs to be large and close to the engine, perhaps a design where the engine is mounted on or even incorporated into the wing is a way to go. There might be one advantage to using Sterling external combustion engines for aviation: the use of atomic energy as a fuel source if the weight of the lead shielding were not too great. Imagine an aircraft that effectively never runs out of fuel! There'd be no more fuel exhaustion mishaps. One downside would be the hazardous materials that could be dispersed in a crash. There are a lot of down sides to atomic power, but NASA uses it to power Stirling engines in space. Understandable, but their expectation is that catastrophic destruction would disperse the nuclear material harmlessly. That can't be presumed for light aircraft. If the rocket detonated in the atmosphere, it might not be so harmless. I don't see why it would be nearly as bad as a "dirty bomb" would be, as the material would be dispersed over a pretty large area. I would guess the reactor is jacketed with sufficient strength to preclude its destruction. My guess is that NASA et al are just hoping for good fortune. Having a reactor land from orbit intact in the middle of a city wouldn't be all that desirable. ;-) So, my bet is on there being no good plan for dealing with such a catastrophe *other* than wide dispersal of the nuclear material or the luck of landing in the ocean. Not that *that* outcome is desirable either... Neil |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Electrically Powered Ultralight Aircraft | Larry Dighera | Piloting | 178 | December 31st 07 08:53 PM |
Solar powered aircraft. Was: Can Aircraft Be Far Behind? | Jim Logajan | Piloting | 4 | February 9th 07 01:11 PM |
World's First Certified Electrically Propelled Aircraft? | Larry Dighera | Piloting | 2 | September 22nd 06 01:50 AM |
Powered gliders = powered aircraft for 91.205 | Mark James Boyd | Soaring | 2 | December 12th 04 03:28 AM |
Help! 2motors propelled ultralight aircraft | [email protected] | Home Built | 3 | July 9th 03 01:02 AM |