Has anyone look at DLC for Diamond-like coatings for aluminum side
plates. I am sure it is expensive but I don not know how it would compare to other
coating particularly silicon nitride flam spraying.
http://www.bekaert.com/bac/Products/Diamond-Like%20Coatings.htm
http://www.bekaert.com/bac/Products/Diamond-like%20coatings/Automotive%20Engine%20Parts.htm
http://www.bekaert.com/bac/Products/Diamond-like%20coatings/Racing%20Engine%20Parts.htm
DYLYN® PLUS VALUES THAT CAN BE OBTAINED
- Coating thickness
varies from 1 to 5 µm
- Deposition
temperature < 180°C / 356°F
|
Coefficient
of friction
|
0,05 - 0,10
|
Steel-ball-on-disc test (dry):
10N, 0.17 m/s, 25°C (77°F), 50% RH
and 100,000 cycles
|
|
Hardness
(GPa)
|
15 - 25
|
Nano indentation
|
|
Adhesion -
Lc2 Value (N)
|
> 25
|
Scratch test: constant load on HSS (M2) substrate
|
|
Adhesion -
HF Value
|
1 - 2
|
Rockwell C on HSS (M2) according to VDI 3198
|
|
E-modulus
(GPa)
|
150 - 250
|
Nano indentation
|
http://www.azom.com/details.asp?ArticleID=623
Properties
of Diamond-Like Coatings
Amorphous (a-C)
and hydrogenated amorphous carbon (a-C:H) films have high hardness, low
friction, electrical insulation, chemical inertness, optical transparency,
biological compatibility, ability to absorb photons selectively, smoothness,
and resistance to wear. For a number of years, these economically and
technologically attractive properties have drawn almost unparalleled interest
towards these coatings. Carbon films with very high hardness, high resistivity,
and dielectric optical properties, are now described as diamond-like carbon or
DLC, table 1.
Table 1. Properties of diamond
and DLC materials.
|
|
|
|
|
|
|
|
|
|
|
|
Crystal Structure
|
Cubic
ao=3.561Å
|
Amorphous
Mixed sp2 and sp3 bonds
|
Amorphous
sp3/sp2
|
Cubic
ao=3.567Å
|
Hexagonal
a=2.47
|
|
Form
|
Faceted crystals
|
Smooth or rough
|
Smooth
|
Faceted crystals
|
|
|
Hardness (Hv)
|
3000-12000
|
1200-3000
|
900-3000
|
7000-10000
|
|
|
Density (g/cm3)
|
2.8-3.5
|
1.6-2.2
|
1.2-2.6
|
3.51
|
2.26
|
|
Refractive Index
|
-
|
1.5-3.1
|
1.6-3.1
|
2.42
|
2.15
|
|
Electrical Resistivity (Ω/cm)
|
>1013
|
>1010
|
106-1014
|
>1016
|
0.4
|
|
Thermal Conductivity (W/m.K)
|
1100
|
-
|
-
|
2000
|
3500
|
|
Chemical Stability
|
Inert
|
Inert
|
Inert
|
Inert
|
Inert
|
|
Hydrogen Content (H/C)
|
-
|
-
|
0.25-1
|
-
|
-
|
|
Growth Rate (µm/hr)
|
~1
|
2
|
5
|
1000 (synthetic)
|
-
|
Engine
Applications
The coatings may
well find their biggest application in enhancing properties of general wear
parts. For example, it was hoped that the coating of cams and cam followers
with DLC in Formula 1 motorbike engines would produce an increase in power of
0.5-1bhp. The resulting power increase was 8bhp, which in racing terms is
enormous.
-----Original Message-----
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On Behalf Of George
Lendich
Sent: Friday, May 13, 2005 5:43 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Aluminum side housings
> George Lendich wrote:
>
> >>We were discussing aluminum side and intermediate housings
a couple of
> >>weeks ago. A figure
of somewhere around 15lbs per housing in weight
> >>savings was thrown out.
The exact figure isn't as important the fact
> >>that several Delta builders have had to stack
approximately that much
> >>weight in the tail to get the proper W&B.
> >>
> >Ernest,
> >Surface treatments are problematic- no real cost effective
treatment as
yet.
> >Composite( aluminium and steel) housings don't save that much
weight, I
> >forget the exact figures but will save about 30 lbs, at best.
A hell of a
> >lot of work ( and cost) to get that 30 lbs.
> >
> >
> >
>
> I tend to agree with you, George, but you have to balance the work
> required to remove 30lbs from the engine against the work required
to
> remove 30lbs from my slim figure*.
I won't even consider aluminum sides
> until I do a (semi) final weight and balance. If it comes down to
> aluminum housings or more junk-n-da-trunk, the debate will be wide
open
> again.
>
> (The humor will be apparent when you get to the email where Ed
tells me
> that I'm a little stout for his RV 8*)
Ernest,
Don't get me wrong I'm actually working on aluminium housings as we
speak -
however the truth of the exercise is fully evident when costs and
weights
are real, rather than anticipated. Machining anything is a hugely
expensive
part of any development and there's a lot of machining in end housings.
Hey I'm on the diet too, but firewall forward weight is my main
concern, for
C of G requirements.
George ( down under)
>> Homepage: http://www.flyrotary.com/
>> Archive:
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