Difference between revisions of "Consistent design for external limiting factors"

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When designing a product usually one wishes that it poses some resilience to environmental influences.
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When designing a product one usually wishes that it poses some resilience to environmental influences.
 
A few critical delicate components in a mainly robust system can bog down the whole system.
 
A few critical delicate components in a mainly robust system can bog down the whole system.
Those components are the weakest links in the chain and constitute some kind of bottleneck.
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Those components are the weakest links and constitute a bottleneck.
To avoid disproportionate bog-down components should be paired with their resilience ranges,
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that is [[microcomponents]] could be [[microcomponent tagging|tagged]] with links to informations on allowed ranges.
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This way one can design a system consistently for a chosen set of external limiting factors that one requires.
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or maximize certain limiting factors.
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External limiting factors can be: <br>
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To be able to avoid including components that disproportionately bog-down the whole system one should pair components with their resilience ranges.
 +
That is [[microcomponents]] could be [[microcomponent tagging|tagged]] with links to information (stored somewhere else) describing the allowed operational ranges. Just like the usual "absolute maximum ratings" section in datasheets of todays electronic components.
 +
This way one can design a system consistently for a chosen set of the external limiting factors that one requires.
 +
Or maximize for one specific spec (performance parameter).
 +
 
 +
'''Some examples for external limiting factors are:''' <br>
 
temperature '''T''',  
 
temperature '''T''',  
 
radiation  '''I , ..''',  
 
radiation  '''I , ..''',  
 
acceleration '''a''',  
 
acceleration '''a''',  
pressure '''p''', ...
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pressure '''p''', <br>
 +
chemical resilience when exposed to "surface" (pH, redox-potential), ...
 +
 
 +
== Absolute maximum/minimum Temperature ==
  
== absolute maximum/minimum Temperature ==
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The allowed temperature range of a whole system is defined by the intersection of all the allowed temperature ranges of the system components.
 +
This is of course only true when one assumes thermally equilibrium at the size scale of the whole system. Otherwise one could just protect the sensitive parts by thermally isolating them.
  
The allowed temperature range of a whole system (on a thermally equilibrated micro-scale) is defined by the intersection of all the allowed temperature ranges of the system components.
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At and below the microscale thermal equilibrium is almost always present (more or less) due very low levels of thermal isolation which are caused by the [[scaling law]] that surface area per enclosed volume rises with shrinking size.
When using technology of [[brownian technology path]] in e.g. [[technology level III]] either in the process of reaching it or when re-merging after reaching it the machine phase (e.g. [[chemomechanical converters|entropic batteries]]) AP Technology will acquire an accordingly restricted range of allowed operation temperature range especially much of the otherwise down to zero kelvin completely allowed low temperature regime will be cut off.
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It is advisable to keep track off all the allowed temperature ranges for system components (no matter which technology path)
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When one would keep using technology of early steps of the [[incremental path]] to advanced gem-gum technology (that is when one would keep in remnants of the [[bootstrapping]] process) in [[technology level III|advanced gem-gum technology]] then this new technology will be bogged-down to an accordingly restricted allowed range of operation temperature.
and keep the technology path branches (with vastly different allowed temperature ranges) as separate as possible.
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Especially much of the otherwise completely allowed low temperature regime all the way down to zero kelvin will be cut off.
 +
The same happens when one would start using technology of the (with gem-gum technology unrelated) [[brownian technology path]].
  
Diamond is metastable and can turn into graphite at too high temperatures.
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There are likely several cases where one might want to include temperature sensitive parts and accept the implicated severe cuts in thermal resilience.
Other [[diamondoid]] materials like the carbides of the titanium vanadium and chromium group ([//en.wikipedia.org/wiki/Carbide interstitial carbides]) can be used for high temperature applications since they are [http://en.wikipedia.org/wiki/Refractory refractory]. (complete sets of DMEs are needed).
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Some of these could be:
Stability of free or mutual or environmentally contacting passivated surfaces (that are possibly strained) will reduce the allowed temperatures well below the bulk material melting points though. Interstitial diffusion may too be a limiting factor.
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* [[Entropomechanical converter|Entropic batteries]] – They might work better with smaller molecules that are prone to freeze. <br>(In case of an implementation with floppy singly linked chain molecules they likely "feature" high sensitivity to radiation damage beside thermal limits.)
 +
* A situation where thermal capacity bog-down due to integration of thermally sensitive parts does not matter at all are advanced [[medical nanodevices]] since those are embedded in a highly temperature sensitive environment anyway.
 +
* ...
  
4th period:
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The different technology path branches (micro chamber managed [[brownian technology path]] vs late stages of [[incremental path]]) have vastly different allowed temperature ranges. It is probably advisable to keep track off all the allowed temperature ranges for system components and keep the technology path branches as separate as possible.
* [//en.wikipedia.org/wiki/Titanium_carbide TiC] (3,160 °C; 5,720 °F; 3,430 K; abundant elements)
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* [//en.wikipedia.org/wiki/Vanadium_carbide VC] (2810 °C; 9-9.5 Mohs)
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* [//en.wikipedia.org/wiki/Chromium_carbide Cr<sub>3</sub>C<sub>2</sub>; Cr<sub>7</sub>C<sub>3</sub>; Cr<sub>23</sub>C<sub>6</sub>] (1,895 °C; 3,443 °F; 2,168 K; extremely hard; very corrosion resistant)
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5th period:
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* [//en.wikipedia.org/wiki/Zirconium_carbide ZrC] (3532 °C; extremely hard; highly corrosion resistant; very metallic)
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* [http://en.wikipedia.org/wiki/Niobium_carbide Nb<sub>2</sub>C] (3490 °C; extremely hard; highly corrosion resistant)
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* Mo<sub>2</sub>C (2692 °C) [http://tttmetalpowder.com/molybdenum-carbide-powder-303/]; MoC; Mo<sub>3</sub>C<sub>2</sub> [http://en.wikipedia.org/wiki/Carbide]
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6th period:
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* [//en.wikipedia.org/wiki/Hafnium_carbide HfC] (3900 °C; very refractory; low oxidation resistance)
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* [//en.wikipedia.org/wiki/Tantalum_carbide TaC<sub>X</sub>] (3880 °C (TaC)  3327 °C (TaC<sub>0.5</sub>); extremely hard; metallic conductivity)
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* [http://en.wikipedia.org/wiki/Tungsten_carbide WC] (2,870 °C; 5,200 °F; 3,140 K; ~9 on Mohs scale)
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mixed:
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* [//en.wikipedia.org/wiki/Tantalum_hafnium_carbide Ta<sub>4</sub>HfC<sub>5</sub>] (record holder: 4,215 °C; 7,619 °F; 4,488 K)
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Note: Many elements here are neither abundant nor prime targets for [[mechanosynthesis]].
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Potentially thermally weak structures to look out for could be:
 +
* Very strongly strained parts of [[diamondoid molecular elements|crystolecules]] like cylindric shells. Here less thermal energy is required to overcome the remaining energy barrier and break stuff.
 +
* Bistable structures with low energy barriers.
 +
* Close proximity of atoms that like to form low-energy highly volatile compounds. Many nitrogen atoms close together e.g. may tend to form N<sub>2</sub> gas on heating. Also water and carbon dioxide may form in very harsh thermal conditions.
 +
* Diamond is metastable and can turn into graphite at too high temperatures. Other [[refractory materials]] are better suited for high temperature applications.
  
 
[[Category:Technology level III]]
 
[[Category:Technology level III]]

Latest revision as of 19:32, 14 June 2021

When designing a product one usually wishes that it poses some resilience to environmental influences. A few critical delicate components in a mainly robust system can bog down the whole system. Those components are the weakest links and constitute a bottleneck.

To be able to avoid including components that disproportionately bog-down the whole system one should pair components with their resilience ranges. That is microcomponents could be tagged with links to information (stored somewhere else) describing the allowed operational ranges. Just like the usual "absolute maximum ratings" section in datasheets of todays electronic components. This way one can design a system consistently for a chosen set of the external limiting factors that one requires. Or maximize for one specific spec (performance parameter).

Some examples for external limiting factors are:
temperature T, radiation I , .., acceleration a, pressure p,
chemical resilience when exposed to "surface" (pH, redox-potential), ...

Absolute maximum/minimum Temperature

The allowed temperature range of a whole system is defined by the intersection of all the allowed temperature ranges of the system components. This is of course only true when one assumes thermally equilibrium at the size scale of the whole system. Otherwise one could just protect the sensitive parts by thermally isolating them.

At and below the microscale thermal equilibrium is almost always present (more or less) due very low levels of thermal isolation which are caused by the scaling law that surface area per enclosed volume rises with shrinking size.

When one would keep using technology of early steps of the incremental path to advanced gem-gum technology (that is when one would keep in remnants of the bootstrapping process) in advanced gem-gum technology then this new technology will be bogged-down to an accordingly restricted allowed range of operation temperature. Especially much of the otherwise completely allowed low temperature regime all the way down to zero kelvin will be cut off. The same happens when one would start using technology of the (with gem-gum technology unrelated) brownian technology path.

There are likely several cases where one might want to include temperature sensitive parts and accept the implicated severe cuts in thermal resilience. Some of these could be:

  • Entropic batteries – They might work better with smaller molecules that are prone to freeze.
    (In case of an implementation with floppy singly linked chain molecules they likely "feature" high sensitivity to radiation damage beside thermal limits.)
  • A situation where thermal capacity bog-down due to integration of thermally sensitive parts does not matter at all are advanced medical nanodevices since those are embedded in a highly temperature sensitive environment anyway.
  • ...

The different technology path branches (micro chamber managed brownian technology path vs late stages of incremental path) have vastly different allowed temperature ranges. It is probably advisable to keep track off all the allowed temperature ranges for system components and keep the technology path branches as separate as possible.

Potentially thermally weak structures to look out for could be:

  • Very strongly strained parts of crystolecules like cylindric shells. Here less thermal energy is required to overcome the remaining energy barrier and break stuff.
  • Bistable structures with low energy barriers.
  • Close proximity of atoms that like to form low-energy highly volatile compounds. Many nitrogen atoms close together e.g. may tend to form N2 gas on heating. Also water and carbon dioxide may form in very harsh thermal conditions.
  • Diamond is metastable and can turn into graphite at too high temperatures. Other refractory materials are better suited for high temperature applications.