R
Runge_Kutta
Guest
First, the downside - Berylliosis
http://www.healthatoz.com/healthatoz/Atoz/ency/berylliosis.jsp
http://www.eh.doe.gov/health/beryllium/communicating.pdf
Now, the upside
From ( www.tsgc.utexas.edu/archive/subsystems/structures.pdf Pages 10-15)
=================
Beryllium
With a density approximately 60% of aluminum and a stiffness to weight ratio six
times better than aluminum or titanium, this material has many potential
applications. Being stiffer than other materials it can be useful in avoiding resonant
frequencies that may occur between a satellite and its booster during launch. It is
non-magnetic, has a high elastic modulus (44 Msi), and a high yield strength. Using
beryllium instead of aluminum can reduce weight significantly, and its high
thermal conductivity makes it an excellent choice for components that will conduct
heat. It is also non-reactive with hydrogen.
However, beryllium is extremely anisotropic and sensitive to damage, and is twice
as brittle as aluminum. Its relatively low fracture toughness at cryogenic
temperatures is a potential drawback, but development of beryllium-aluminum
alloys may improve this. It also needs special facilities and tools for machining due
to the toxicity of its dust, and is thus very expensive.
=================
From ( http://www.ccdott.org/hss_volume2/07_loads,_materials_&_structures.pdf See Table 1)
=================
Beryllium-aluminum alloys containing greater than 60 percent (by weight)
beryllium are favorable materials for applications that require light weight and high
stiffness. These alloys have 22 percent lower density than aluminum with three times the
elastic modulus and a 40 percent lower coefficient of thermal expansion. Some
aluminum-beryllium alloys have been developed for aerospace applications. The
AlBeMet series of alloys was initially selected for a folding fin on the SR-71 Blackbird.
The properties of some of the beryllium-aluminum alloys are presented in Table 2.
AlBemet 162 is a promising alloy with a high cycle fatigue limit of 10 million
cycles at 30.5 ksi. It is immune to stress-corrosion cracking at 90 percent of
yield stress in saltwater at 65 degrees C for 169 hours and in salt at 315 degrees
C for 100 hours.
=================
Here are some properties:
=================
http://www.geocities.com/pganio/materials.html (AM 162 makes titanium look cheap!!)
http://www.matweb.com/search/SpecificMaterial.asp?bassnum=NBB002
http://www.asminternational.org/Tem...ate=Ecommerce/FileDisplay.cfm&file=ACF7E2.pdf
=================
So, where is beryllium used?
=================
http://www.pureluckdesign.com/ferrari/f1engine/ (Pistons)
http://www.clevelandclinicmeded.com/diseasemanagement/pulmonary/occlung/table1.htm
http://www.thalesgroup-optronics.com/pdf/Beryllium.pdf
http://nautilus.fis.uc.pt/st2.5/scenes-e/elem/e00410.html
http://www.focal.tm.fr/gb/instal/images/cahiertekgube.pdf
http://www.reade.com/ezine/vol1issue6/reade0106_en_4.shtml
http://www.jobwerx.com/news/Archives/aerospace_materials_advances_news_id_102703.html (AM 140)
=================
The primary American producer of Beryllium appears to be Brush-Wellman
http://www.berylliumproducts.com/web/bpdweb.nsf
For weight loss in Corvette applications, one is probably mostly interested
in alloys of beryllium and aluminum. The alloy which is 62% beryllium and
38% aluminum looks like a good choice ALuminumBErylliumMETAL162 = AlBeMet162
http://www.reade.com/Products/Alloys/aluminum_beryllium_alloy_al_be.html
One can also apply beryllium-aluminum alloys to engine bearings:
===========================
http://patft.uspto.gov/netacgi/nph-...0&d=PTXT&p=1&S1=6308680&OS=6308680&RS=6308680
GM Patent, Engine block crankshaft bearings, 6,308,680
An internal combustion engine comprises an aluminum alloy engine block housing
pistons in cylinders and having a lower face including an upper semi-circular
bearing surface. A lower bearing support has a lower semi-circular bearing
surface to complement the upper semi-circular bearing surface in the engine
block to define a crankshaft bore to rotatably support a ferrous crankshaft.
The lower bearing support is formed of a single beryllium-aluminum alloy having
a coefficient of thermal expansion comparable to the ferrous crankshaft to
promote a consistent clearance between the lower bearing support and the
crankshaft. Such a beryllium-aluminum alloy may be comprised of approximately
60-65% by weight beryllium and the balance is aluminum.
===========================
Here's an informative patent on beryllium-aluminum alloys
===========================
6,312,534 High strength cast aluminum-beryllium alloys containing magnesium
http://patft.uspto.gov/netacgi/nph-...1=AND&d=ptxt&s1=6312534&OS=6312534&RS=6312534
===========================
Also:
6,656,421 Aluminum-beryllium-silicon based alloy
While there are also beryllium-copper alloys, I doubt they have much
application in the mechanical part of a Corvette except the valve
seat in the heads.
http://www.brushwellman.com/alloy/tech_lit/GuideToCopperBeryllium.pdf
Here's some random stuff:
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/berylmcs96.pdf
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/100495.pdf ($275/pound for Be powderin 1995)
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/100498.pdf ($385/pound for Be powderin 1998)
Compare Beryllium-Aluminum (AM162) to traditional Aluminum-Silicon alloys
used for pistons. The LS1/LS6 and presumably LS2/LS7 use a Mahle alloy
M142. Here's something relatively close.
http://www.spba.net/pdf/alsi356.pdf
http://www.healthatoz.com/healthatoz/Atoz/ency/berylliosis.jsp
http://www.eh.doe.gov/health/beryllium/communicating.pdf
Now, the upside
From ( www.tsgc.utexas.edu/archive/subsystems/structures.pdf Pages 10-15)
=================
Beryllium
With a density approximately 60% of aluminum and a stiffness to weight ratio six
times better than aluminum or titanium, this material has many potential
applications. Being stiffer than other materials it can be useful in avoiding resonant
frequencies that may occur between a satellite and its booster during launch. It is
non-magnetic, has a high elastic modulus (44 Msi), and a high yield strength. Using
beryllium instead of aluminum can reduce weight significantly, and its high
thermal conductivity makes it an excellent choice for components that will conduct
heat. It is also non-reactive with hydrogen.
However, beryllium is extremely anisotropic and sensitive to damage, and is twice
as brittle as aluminum. Its relatively low fracture toughness at cryogenic
temperatures is a potential drawback, but development of beryllium-aluminum
alloys may improve this. It also needs special facilities and tools for machining due
to the toxicity of its dust, and is thus very expensive.
=================
From ( http://www.ccdott.org/hss_volume2/07_loads,_materials_&_structures.pdf See Table 1)
=================
Beryllium-aluminum alloys containing greater than 60 percent (by weight)
beryllium are favorable materials for applications that require light weight and high
stiffness. These alloys have 22 percent lower density than aluminum with three times the
elastic modulus and a 40 percent lower coefficient of thermal expansion. Some
aluminum-beryllium alloys have been developed for aerospace applications. The
AlBeMet series of alloys was initially selected for a folding fin on the SR-71 Blackbird.
The properties of some of the beryllium-aluminum alloys are presented in Table 2.
AlBemet 162 is a promising alloy with a high cycle fatigue limit of 10 million
cycles at 30.5 ksi. It is immune to stress-corrosion cracking at 90 percent of
yield stress in saltwater at 65 degrees C for 169 hours and in salt at 315 degrees
C for 100 hours.
=================
Here are some properties:
=================
http://www.geocities.com/pganio/materials.html (AM 162 makes titanium look cheap!!)
http://www.matweb.com/search/SpecificMaterial.asp?bassnum=NBB002
http://www.asminternational.org/Tem...ate=Ecommerce/FileDisplay.cfm&file=ACF7E2.pdf
=================
So, where is beryllium used?
=================
http://www.pureluckdesign.com/ferrari/f1engine/ (Pistons)
http://www.clevelandclinicmeded.com/diseasemanagement/pulmonary/occlung/table1.htm
http://www.thalesgroup-optronics.com/pdf/Beryllium.pdf
http://nautilus.fis.uc.pt/st2.5/scenes-e/elem/e00410.html
http://www.focal.tm.fr/gb/instal/images/cahiertekgube.pdf
http://www.reade.com/ezine/vol1issue6/reade0106_en_4.shtml
http://www.jobwerx.com/news/Archives/aerospace_materials_advances_news_id_102703.html (AM 140)
=================
The primary American producer of Beryllium appears to be Brush-Wellman
http://www.berylliumproducts.com/web/bpdweb.nsf
For weight loss in Corvette applications, one is probably mostly interested
in alloys of beryllium and aluminum. The alloy which is 62% beryllium and
38% aluminum looks like a good choice ALuminumBErylliumMETAL162 = AlBeMet162
http://www.reade.com/Products/Alloys/aluminum_beryllium_alloy_al_be.html
One can also apply beryllium-aluminum alloys to engine bearings:
===========================
http://patft.uspto.gov/netacgi/nph-...0&d=PTXT&p=1&S1=6308680&OS=6308680&RS=6308680
GM Patent, Engine block crankshaft bearings, 6,308,680
An internal combustion engine comprises an aluminum alloy engine block housing
pistons in cylinders and having a lower face including an upper semi-circular
bearing surface. A lower bearing support has a lower semi-circular bearing
surface to complement the upper semi-circular bearing surface in the engine
block to define a crankshaft bore to rotatably support a ferrous crankshaft.
The lower bearing support is formed of a single beryllium-aluminum alloy having
a coefficient of thermal expansion comparable to the ferrous crankshaft to
promote a consistent clearance between the lower bearing support and the
crankshaft. Such a beryllium-aluminum alloy may be comprised of approximately
60-65% by weight beryllium and the balance is aluminum.
===========================
Here's an informative patent on beryllium-aluminum alloys
===========================
6,312,534 High strength cast aluminum-beryllium alloys containing magnesium
http://patft.uspto.gov/netacgi/nph-...1=AND&d=ptxt&s1=6312534&OS=6312534&RS=6312534
===========================
Also:
6,656,421 Aluminum-beryllium-silicon based alloy
While there are also beryllium-copper alloys, I doubt they have much
application in the mechanical part of a Corvette except the valve
seat in the heads.
http://www.brushwellman.com/alloy/tech_lit/GuideToCopperBeryllium.pdf
Here's some random stuff:
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/berylmcs96.pdf
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/100495.pdf ($275/pound for Be powderin 1995)
http://minerals.usgs.gov/minerals/pubs/commodity/beryllium/100498.pdf ($385/pound for Be powderin 1998)
Compare Beryllium-Aluminum (AM162) to traditional Aluminum-Silicon alloys
used for pistons. The LS1/LS6 and presumably LS2/LS7 use a Mahle alloy
M142. Here's something relatively close.
http://www.spba.net/pdf/alsi356.pdf