Note: Descriptions are shown in the official language in which they were submitted.
CA 02358484 2001-09-19
Background of the Invention: The invention relates to add-on aerodynamic air
deflectors for the rear surface of a transport trailer. Inflatable drag
reducers have been
described (e. g. McDonald ( 1977) U. S Patent No. 4,006,932, Ryan { 1998) U.
S. Patent
No. 5,823,610), and are more practical than rigid versions (e.g. Lechner
(1994) U.S.
Patent No. 5,375,903, Switlik (1996) U.S. Patent No. 5,498,059, Boivin (2001)
U.S
Patent No. 6,257,654 B 1), because inflatables are light-weight and
collapsible to a very
thin state so as not to interfere with complete trailer door opening which is
important
because there is limited room to maneuver at most loading docks. However,
given that
the standard long-haul trailer in North America is a double door
configuration, this
requires that the drag reducer have two separate halves meeting medially along
a planar
surface when inflated. The external surfaces over which the airstream passes
should also
be planar for minimum turbulence creation and maximum drag reduction.
Inflatables
naturally tend towards a spherical shape without an internal means of
controlling the
position of the surface. The present invention describes a novel configuration
of internal
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CA 02358484 2001-09-19
cords that allows the two bags to meet neatly along a common. plane, while
having
grossly flat external surfaces that are held firmly in place even in heavy
crosswinds.
To achieve auto-inflation the present invention employs a flexible air-scoop
extending
above the roofline from each bag to capture air pressure from the over-passing
air stream.
Similar such means have been used for inflation purposes in prior art (e.g.
McDonald
(1977) U.S. Patent No. 4,006,932, Needy (1979) U.S. Patent :loo. 4,142,755,
Lechner
(1994) U.S. Patent No. 5,375,903).
To achieve bag stability and avoid surface flailing during inflation and
deflation, an
elastic cord oriented in a circular fashion on the medial surface of each bag
is employed
as disclosed in Andrus (1993) U.S. Patent No. 5,236,347. The present
disclosure further
teaches that the placement of such an elastic cord for a double; bag
configuration is best
on the medial surface of each bag thereby drawing the bags together and away
from
traffic during conditions of partial inflation.
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CA 02358484 2001-09-19
summary of the Invention: The invention solves the problem of creating an
aerodynamically optimal shape with flat surfaces from a soft inflatable
material, as well
as the problem of the inherent lateral instability of a double bag
configuration. The novel
aspect disclosed herein is a network of internal cords consisting of a
radially oriented
array of horizontal cords that stabilize and flatten the lateral surfaces of
the bags, and a
parallel array of vertical cords that flatten the upper and lower surfaces.
Brief description of the drawings: Figure I is a side view of a trailer with
the invention
mounted. Figure 2 is a face-on view showing the internal cordls. Figure 3 is a
top view
showing the 5 columns of horizontal cords splaying out radially, and the I O
vertical cards
per bag end-on. Figure 4 shows the medial surface of ane half' of the
invention with the
elastic recoil system exposed.
Detailed description of the preferred embodiment: Each h,~lf of the invention
is a
fully enclosed bag 10 mounted permanently onto each of the o-ear doors I I of
the trailer.
A flexible rubber air-scoop I Z feeds air into each bag to provide inflation
pressure with
trailer motion. A circular series of outside patches 13 on the medial side I4
of each bag
I O pauses an elastic cord 15 that functions to draw the bags 1 ~0 together by
contracting
when inflation is only partial, thereby maintaining stability and preventing
lateral flailing
of the bags. An array of horizontal inelastic cards I6 originate from the
medial edge I7
of the base 18 and splay out to insert at equally spaced points on the inner
surface of the
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CA 02358484 2001-09-19
lateral side 19 and trailing surface 20. There are twenty-seven horizontal
cords 16 per bag
10, twenty-four on the lateral side 19 and three on the trailing surface 20.
An array of
vertical inelastic cords 21 connects the upper surface 22 and lower surface 23
of each bag
10, and intersects with the horizontal cords 16. The horizontal cords 16 and
the vertical
cords 2I are attached to inside patches 24 that are heat sealed to the inside
surface of the
bags 10. A rubber tube 25 that easily disconnects in its middle feeds air from
one bag to
the other in the event of partial air scoop l2 failure or a significant
surface hole in one
bag so as to maintain relatively equal bag pressure and thereby symmetry of
drag reducer
shape. Each bag has a zipper 2~ which can be undane to allow rapid deflation
at the
loading dock. Air leakage through the closed zippers 2fi during operation also
serves to
bleed unnecessary pressure from the bags so that the seams and attachment
points are not
unduly loaded. At 60 mph airspeed, the available static head of air pressure
is about 2.5
inches of water or 0.1 psi. half of which is lost through the closed zippers
2b leaving
about O.OS psi. 'The bag's surface tension will overcome the tension of the
elastic cord 1~
and allow full inflation as iow as 0.025 psi. At 0.05 psi (typical highway
operating
conditions), each of the inelastic cords is loaded with about 7 pounds
tension.
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