From: stealthman@iglou.com
On Thu, 29 Sep 2011 03:12:41 -0400, STEALTHMAN
wrote:
> Page Two, Application 972527 - Continued
> I was short of money, had a job, had two kids
>in college, and did not feel like making a trip, and
>feared running up a bill with the law firm and the
>possibility that I would have had to give them
>part of the invention if I couldn't pay the bill, so
>I began thinking of how to file a "continuation-in-
>part application, rather than try to salvage the
>apparently less than adequate application 972527.
>
> (7)
Page Two, Application 972527 - Continued
18 Fig. 1., in the drawing is a bottom surface of an
arbitrary shape
19 of aircraft lower surface, the outline or perimeter
shape being
20 unimportant as long as the lower surface and
possibly the side and
21 top surface, are constructed with a surface
figure or configuration
22 which conforms to the specifications for configurations
of ultra small
23 reflected pattern beam configurations as described in
this specification.
24 Fig. 2., is an end view of a nominal wing chord with
it's bottom
25 surface conforming to the specified configurations.
26 Fig. 3., is a front or rear view of that chord section
showing the
27 specified radius of curvature of the surface figure.
28 Fig. 4., is an end view of the same wing chord except
that the bottom
29 surface has a slightly different radius of curvature.
30 Fig. 5., is a front or rear view of a similar wing section,
except
31 that it has a different radius of curvature of the surface
figure
32 of the lower surface.
33 Fig. 6., is a view of a cone with the conical surface
having a round
34 profile when viewed from the pointed end, but
the side view shows a
35 modified cone with the surfaces having an arched
concave configuration
36 of specified radius of curvature.
37 Fig. 7., is a side view of a cylindrical structure with
the walls
38 of the cylinder having the straight sides modified
to conform to the
39 specified concave radius of curvature.
40 Fig. 8., shows a side view of a structure which
is a perfect cone.
Page Three, Application 972527 - Continued
01 Fig. 9., shows a perfect cylinder with no modification.
02 Fig. 10., depicts a conical section, of arbitrary shape
and size,
03 which might be either a section of a perfect cone or,
for better
04 avoidance, might have it's straight surface modified
to be a concave
05 arc with a radius of curvature of twice the maximum
operating altitude
06 for aircraft and with a radius of curvature of infinity
for spacecraft.
07 Fig. 11., shows a section of a perfect cylinder, which,
for better
08 avoidance might also have it's straight sides made a
concave arc
09 with a radius of curvature of one to two times the
operating altitude
10 for aircraft and a radius of curvature of infinity for
spacecraft.
11 Combinations of any of the above surfaces may be
combined as long as
12 the unmodified straight lines or the straight lines
after modification
13 are all in the same plane or all being perfectly
parallel to one and
14 the same arbitrary imaginary plane surface so
that the reflected beam
15 from all surfaces falls or is projected as close to
the other reflected
16 beams from the same craft and all covering the
smallest area possible,
17 so that the concept of the invention can be
realized.
(8)
STEALTHMAN
--- SoupGate-Win32 v1.05
* Origin: you cannot sedate... all the things you hate (1:229/2)
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