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Patent 2362624 Summary

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Claims and Abstract availability

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(12) Patent Application: (11) CA 2362624
(54) English Title: AERODYNAMIC FLAG AND ADVERTISER
(54) French Title: BANNIERE PUBLICITAIRE AERODYNAMIQUE
Status: Deemed Abandoned and Beyond the Period of Reinstatement - Pending Response to Notice of Disregarded Communication
Bibliographic Data
(51) International Patent Classification (IPC):
  • G09F 7/00 (2006.01)
  • G09F 13/00 (2006.01)
  • G09F 17/00 (2006.01)
  • G09F 19/02 (2006.01)
  • G09F 21/04 (2006.01)
(72) Inventors :
  • CADAVIS, GONZALO A. (Canada)
(73) Owners :
  • GONZALO A. CADAVIS
(71) Applicants :
  • GONZALO A. CADAVIS (Canada)
(74) Agent:
(74) Associate agent:
(45) Issued:
(22) Filed Date: 2001-11-05
(41) Open to Public Inspection: 2003-05-05
Examination requested: 2006-09-21
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): No

(30) Application Priority Data: None

Abstracts

English Abstract


The Invention is aerodynamically constructed and designed
structure with pair of wings or sets of winglets on both sides and
streamlined panel resulting to aerodynamic function created by wind
velocity and direction thereby creating lifting effect on the structure.
The aerodynamics on wings or winglets and the streaming
effect of the wind on display panel on vertical axis sustains lifting
capability to stay aerial and stability without wind beating and flapping
effects that normally results to the disintegration and ultimately the
destruction of flags, outdoor signs and the like.
The Invention may be illuminated from outside power source to
display images placed on display surface i.e. flag, advertising or
announcements during darkness.
The display panel is made of clear durable plastics to allow non-
obstructed view of display and illumination. It is lightweight to stay
aerial, and durable to hold the structure together withstanding weather
elements on all seasons.


Claims

Note: Claims are shown in the official language in which they were submitted.


-11-
IV-CLAIMS:
The Embodiments of the Invention in which an exclusive
property or privilege is claimed are defined as follows:
1. An Aerodynamics Flag and Advertiser for the purpose but not
limited to outdoor signs and display including flags, color, banners,
symbolic colors, advertising signs and the like, and illuminated or not
illuminated.
2. An Aerodynamics Flag and Advertiser design and construction as
recited in Claim#1, whose measurements, sizes or weight are
variables but rather (Fig. 1) is designed and constructed in direct
proportion accordingly, in order to arrive at a working product.
3. An Aerodynamics Flag and Advertiser as recited in Claim#1 and
Claim#2, are constructed and designed with pair of wings (Fig.1.1)
and or several numbers sets of winglets (Fig.5.19) as creator for, but
not limited to, wind lift, dampener or streamer.
4. An Aerodynamics Flag and Advertiser as recited in Claim#1,
Claim#2, and Claim#3 the purpose of which are various, but not
limited to, can installed on a ground level, buildings, mobile transport
including vehicles and the like, aircraft on the ground and public or
private.

-12-
5. An Aerodynamics Flag and Advertiser as recited in Claim#4,
(Fig.1.2) the shell is constructed and designed, but not limited to, in
solid core in aluminum alloy encompassing the metallic panel
including the spike (Fig.1.2a) but excluding; post or stand (Fig.1.4),
display panel (Fig.1.3) and wings (Fig.1.1).
6. An Aerodynamics Flag and Advertiser as recited in Claim#4
(Fig.4.16) the angle of attack adjuster is constructed and designed, but
not limited to, allow adjustments for the correct angle of attack into
the blowing wind to create lifting effect on the aft side of the panel
(Fig.1) resulting to the second leg effect.
7. An Aerodynamics Flag and Advertiser as recited in Claim#4,
(Fig. 4.17) the wing joint sealer is constructed and designed, but not
limited to, seals the joint between the wing side and shell side and on
both wings and are made of soft metal alloy, copper and the like to
seal the joints (Fig.4.17) airtight inside out and strong enough to
withstand pressure difference along the wings joints.
8. An Aerodynamics Flag and Advertiser as recited in Claim#4, and
described in (Fig.4.18) the wing adjuster guide is constructed and
designed, but not limited to, make certain the adjustments are
correctly calibrated to the correct angle of attack coinciding the
calibration with the wing on the opposite side (Fig.4.1).

Description

Note: Descriptions are shown in the official language in which they were submitted.


CA 02362624 2003-02-05
-2-
II - DESCRIPTION:
II-A. BACKGROUND OF TH _F. INVENTION:
Whereas, the demand for the business community to get public
attention to promote or sell respective products has increased the demand
for outdoor advertising, radio, television, print, audio (telephone) and
recently, the Internet Web.
Every businesses that has products to sell or promote wants the
primetime spot to get noticed and public exposure in any media possible,
as evidenced in the recently concluded Super Bowl last January 2003, in
San Diego, CA. Well-known products paid millions of dollars to get the
primetime spot of the year's biggest public exposure for a matter of
seconds or a minute of airtime or in a skimpy banner in a matter of
hours.
Henceforth, the advertising business is thriving simply because
of the basic law of economics, "the law of supply and demand ", wherein
the demand has outgrown the supply.
'Therefore, it is in the interest of the Advertising industry and
the Business companies public and private that the Invention was
conceived. To "Get Noticed", the primetime way.
The Invention, Aerodynamic Flag and Advertiser, as the name
implies, is an outdoor attention-drawer. It draws the attention in a form
of a flag, a banner or simply an aerial advertiser. It draws attention in a
day or nighttime by its illumination, all seasons, any weather, 365 days a
year.

CA 02362624 2003-02-05
-3-
II-B. DESCRIPTION OF PRIOR ART:
It is a known fact that outdoor advertising has been with the
Advertising industry since marketing was conceived. It has develop from
a simple Outdoor Billboard advertising to the neon lighted signs,
billboard and lately to Digitized Illuminated Outdoor Signs. Though,
most of them are fixed in a rigid stand or buildings, some are mobile due
transported and carried along by public or private conveyances, few are
rotational on vertical axis and seldom are rotational and lighted at the
same time.
To mentioned few of those prior Arts;
1. Canadian Patent# CA02010947 issued to Michael Laprise of
Canada filed in 1990 which presented Advertising sign in a fxed/rigid
stand model.
2. Canadian Patent# CA608070 issued to Greg Huey filed in 1960
(country unknown) which presented Rotatable Advertising Sign. It was
constructed to rotate its signs from its adjustable holders from the base
and designed with practical purpose to get noticed for being mobile to
the observer.
All of which are an early predecessor in Advertising signs in each
field, as rigid or mobile category.

CA 02362624 2003-02-05
- 4-
II-C. SUMMARY OF THF.' INVEN710N:
The Invention was conceptualized to develop the outdoor
Advertising industry through "get noticed" mentality and get notice well
in day or night, rain or shine or in short words, in all seasons.
Through the years, the development of rotational and illuminated
signs are limited due to technical difficulties and high cost of
maintenance.
The Invention is a revolutionized development from the rigid stand
and rotational illuminated outdoor signs combined. It works primarily
based on the basic principles of aerodynamics and principally the same
principles why airplanes fly (Fig. l ) and Fig.2 (B). The only difference is
that airplanes fly and moves from point A to point B. The Invention
never moves from point A to point B, except that it rotates around point
A, in all directions (360 degrees) on its vertical axis but never moves out
of point A. The wings are located at the aft point, (Fig. l . l ), as the wind
blows it creates pressure difference on the lower and upper surface of the
wings. The result of the pressure difference due to wing design is that the
lower surface is always stronger against the upper surface (Fig.2 (B) and
you have a lifting effect on the aft side of the structure (Fig.l.2b). The
stronger wind blowing, the better
Its construction is rigid from its vertical stand up to a point to
maintain strength on its vertical axis to counter the strength of the
strongest wind velocity. On the same note, the display panel with its
wings (Fig. l . I ) or winglets (Fig.S. l 9) will aerodynamically respond with
the wind velocity and direction that instead of counter acting the wind,
the invention will face into the direction of the wind and utilizes wind
speeds and direction to create lift on the display panel on the aft side
creating aerial effect (Fig.l.2b) . . . . .(over)

CA 02362624 2003-02-05
- 5 -
The Invention is cost effective due most of earlier rotational and
illuminated models spend most of its electricity on its rotational power
especially if its built top heavy and with so much vertical surface area
that during strong winds it has to counter the high wind velocity by
consuming more electricity to overcome and rotate its vertical axis.
It is cost effective because the construction is simplified with few
moving parts for easy maintenance and repair but strongly built to
withstand strong winds and the harshest Canadian weather.
Most importantly, except for the wings construction and
application on the aft side of the display panel, (Fig.l.l), most features
built-in have been for a while existing technologies incorporated into
other products but have been improved and revised application to work
with this Invention.

CA 02362624 2003-02-05
_6_
I1-D DESCRIPTION OF DRAWINGS:
Fig.l.l, the pair of w~ or winglets (Fig.5.19) is the main
feature of this invention. The design and construction is similar to
aircraft's wings, the function of which is to provide lift of aircraft in
flight. In this invention the wings derive its lifting force through the
passing of wind on top and the bottom. The pressure difference created
by wind velocity creates resultant positive force acting upward against
the lower surface (Fig.2B), creating lift. Lift translates another vertical
support acting on the aft side, as a second leg (Fig.l.2b). Wings are
designed and patterned from NACA airfoil design. As researched and
evaluated, NACA 4415 and NACA 4412 are the most suitable and
adaptable for this Invention, Fig.2(B). The wings (Fig. l . l ) have no
define measurement in this document due they are the variables but are
always in direct proportion with its load structure. In the same manner,
aircraft design is always in direct proportion to its body and designed
payload.
Fig.1.2, the shell holds the display structure together including
the wings, display surfaces and into its rigid stand or post, (Fig.1.4). The
shell is made of aluminum alloy designed to withstand extreme (hot or
cold) outdoor weather. It is constructed strong enough to withstand wind
beating and flapping and heavy rainfall in the unforgiving outdoors. It is
streamlined designed to allow wind passing smoothly without resisting
the wind blowing through its surface, (Fig.4A). In aircraft construction
and design, it is the vertical rudder. The shell construction is solid core
aluminum alloy around the metal structure except; the wings (Fig. l . l ),
the display panel (Fig.1.3), and stand or post (Fig.1.4). . .(over)

CA 02362624 2003-02-05
- 7 -
> The whole panel (Figl) is constructed watertight to prevent rain and
moisture inside but allows a breather to release pressure build-up
especially during winter when heat is allowed to build up to defrost the
whole structure and prevent ice build-up anywhere in the structure,
especially on the wings and display surfaces.
Fig.1.2a, the spike is the third leg of the structure. (As in the
tail of the Kangaroo). It allows its weight to rest on it when wind
velocity is between 0 to 5 mph (calm wind). When the wind is blowing,
its wings act as the second leg on the aft side {Fig.1.2b) due to its lifting
force on its lower surface acting upwards. The spike (Fig.l.2a) takes
over as the alternative leg to support its weight during calm wind
conditions. It is made of aluminum alloy and is an integral part of the
shell (Fig.l.2) structure. The spike extends two-thirds (2/3) from its post,
(Fig. 1.4), towards the aft side and curving and phasing out, (Fig.1.2a).
Fig.l.3, the dispdaY surfaces on both sides of the structure
allows the display of images, i.e., advertisements, flag, color or a banner,
on both sides of its surface. The images are replaceable from its display,
periodically as possible. Similar to replacing regular ads signs, slip it
inside and pull it out. Except that, in this invention, either you climb in
mechanical ladder or bring down the structure for replacements and or
maintenance, as shown in (Fig.3) and (Fig.5.20) for the removal of
plastic display (Fig.l.3). The display surface is made of clear Acrylic
plastics that allow clear view of images on the display and is compose of
two (2) layers. The outer layer which is a clear Acrylic plastic to allow
clear view of display and protector from the outdoor elements including
breakage. The inner layer is a translucent Acrylic plastic to diffuse and
even distribution of illumination to the display. And in-between, is the
slip in/out materials for the images; ads, flag, color, banner and the like.>
. . (over please)

CA 02362624 2003-02-05
g
Fig. 1.4, the stand is the first support or the first leg of the
structure. The entire weight of the structure is supported on this stand
when the wind is calm (less than 5 knots) and subsequently becomes on
the aft side (Fig.5.2b) lighter as wind blows greater than 5 knots. Until it
literally floats as wind blows stronger because of the lifting effects of its
wings, (Fig.l.l) and the streamlining of its shell, (Fig.l.2). The stand
may be constructed rigidly on stand-alone post, Fig.l.4) or mobile in
automobiles. And may be also be constructed in a folding post, similar to
airport's windcone stand. Which allows maintenance by folding it down
opened the ground level. The post has to be constructed on strong
materials like steel to support its all up weight of the panel structure and
considering its continuous exposure to all outdoor elements.
Fig.2.6, the trusses support the upper and lower curvature of the
wing structure. It reinforces the horizontal plane of the wing without it,
the wing structure will crumple. Trusses are made from Aluminum alloy
and are lightweight and strong and do not corrode easily.
Fig.2.7, the ribs are the longitudinal reinforcer of the wing
structure. It connects the trusses together from the shell side (Fig.4.2) to
the last set of truss. It is an aluminum alloy wire. Most metals in the
display panel structure are made of aluminum alloy for strength and
lightweight. The wing interior is hollow to allow heat circulation during
winter and prevent ice formations anywhere on its surface. During
summer months, natwal airflow on its surfaces will provide self cooling
effect to prevent overheating when lights are on.
Fig.2(8), the camberline will determine the correct angle attack
settings of the wings thereby creating the maximum lifting effect
necessary for each wing. (over please). . >

CA 02362624 2003-02-05
-9-
Fig.3.9, the acrylic plastic ribs, reinforces the display panel and
are glued together to the inner side of the clear acrylic plastic. It
strengthens the display panel during wind streaming along its display
surfaces (Fig.4.3) and (Fig.1.3) from the crunching effect of the blowing
wind. The exact number of plastic ribs and dimensions (Fig.3.9) is
proportionate to the size and weight of the display panel placed on each
side.
Fig.3.10, the Fluorescent bulbs are the illuminator of the display
panel at both sides. The bulbs are placed vertically to allow maximum
illumination to the display and easy maintenance and are spaced
accordingly. Proper wattage and length of bulbs are determined with
respective size of display panel, (Fig.1.3).
Fig.3.l 1, the sealed bearin s are the pivotal point on its vertical
axis. It allows unimpeded rotation at all directions (360 degrees) on its
vertical post (Fig.1.4), its first leg. Bearings are located at top and bottom
to restrict its vertical movement (play). Bearings allow rotational
movement on its vertical axis but confine the movement to maintain
stability when rotating.
Fig.3. l2, the slip rims are the mobile contact points that are
attached permanently from its post or stand (Fig.l.4). It is the point of
contact from the main power source to the display panel (Fig.l.3). The
Inventor cannot over emphasize enough the significance of insulation
layer and correct wire gauge at this point and onwards to the last
electrical connection (not shown).
Fig.3.13, the brushes are the contact point relay of the
electrical power from the post (Fig.l.4), to the display panel (Fig.l.3),
which are mobile on the vertical axis. Electrical power supply from this
point is dependent on the brushes. Correct contact pressure is essential
between these points, the brushes and the slip rings (Fig.3.12). . (over) >

CA 02362624 2003-02-05
- l~ -
Fig.3.14, the s rin s make sure that the proper contact
pressure is applied to allow needed electricity across from the slip rings
(Fig.3.12) to the brushes (Fig.3.13). Springs are set to the correct
elasticity to maintain correct pressure contact every time and have to be
replaced at first sign of dissipating elasticity.
Fig.3.15, the connectors are the power lines to the panels
(Fig.1.3) electrical supply and other electrical outlets (not shown).
Fig.4.16, the angle o~'attack adjuster, allows adjustment for
the correct angle of attack into the blowing wind. The correct angle of
attack is essential for the aft side of the display panel (Fig.l.3) and
(Fig.4.3) to create lifting effect for correct aerial position resulting to
second leg effect in the aft position (Fig.l.2b). Adjustments are
introduced from the inside the shell (Fig.l .2) and (Fig.4.2) just between
the joints of both wings.
Fig.4.17, the wings point sealer, seals the joint between the
wing side and shell side and on both wings. (Fig.4.17) Sealers are made
of soft metal alloy copper, or the like, that allows being airtight but
strong enough to withstand the pressure difference (flapping effect) on
the upper and lower surface of the wings (Fig.4.1 ).
Fig.4. I 8, the wing ad buster guide, will make sure the
adjustments are correctly calibrated to the correct angle of attack with its
guided calibration and coincide with the other wing (Fig.4.1 ). Both
wings have to be calibrated exactly at the same moment to ensure wing
stability.

Representative Drawing

Sorry, the representative drawing for patent document number 2362624 was not found.

Administrative Status

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Please note that "Inactive:" events refers to events no longer in use in our new back-office solution.

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Event History

Description Date
Time Limit for Reversal Expired 2012-02-06
Application Not Reinstated by Deadline 2012-02-06
Inactive: Office letter 2011-12-13
Inactive: Office letter 2011-12-12
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2011-11-07
Inactive: Adhoc Request Documented 2011-08-08
Inactive: Office letter 2011-07-04
Inactive: Delete abandonment 2011-03-14
Inactive: Office letter 2011-03-14
Inactive: Payment - Insufficient fee 2011-03-14
Inactive: Abandoned - No reply to s.30(2) Rules requisition 2011-01-13
Inactive: Payment - Insufficient fee 2011-01-04
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2010-11-05
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2010-11-05
Inactive: S.30(2) Rules - Examiner requisition 2010-07-13
Inactive: S.30(2) Rules - Examiner requisition 2010-07-13
Amendment Received - Voluntary Amendment 2010-02-22
Inactive: S.30(2) Rules - Examiner requisition 2009-09-24
Amendment Received - Voluntary Amendment 2009-04-30
Inactive: S.30(2) Rules - Examiner requisition 2008-11-06
Amendment Received - Voluntary Amendment 2008-08-11
Inactive: S.30(2) Rules - Examiner requisition 2008-02-14
Amendment Received - Voluntary Amendment 2007-10-18
Inactive: S.30(2) Rules - Examiner requisition 2007-04-27
Letter Sent 2006-09-29
All Requirements for Examination Determined Compliant 2006-09-21
Request for Examination Received 2006-09-21
Request for Examination Requirements Determined Compliant 2006-09-21
Letter Sent 2006-05-09
Reinstatement Requirements Deemed Compliant for All Abandonment Reasons 2006-04-25
Inactive: Office letter 2005-11-22
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2005-11-07
Change of Address Requirements Determined Compliant 2003-11-07
Inactive: Office letter 2003-11-07
Change of Address or Method of Correspondence Request Received 2003-10-27
Application Published (Open to Public Inspection) 2003-05-05
Inactive: Cover page published 2003-05-04
Inactive: Correspondence - Formalities 2003-02-05
Change of Address Requirements Determined Compliant 2002-04-03
Inactive: Office letter 2002-04-03
Change of Address or Method of Correspondence Request Received 2002-04-01
Inactive: IPC assigned 2002-01-24
Inactive: IPC assigned 2002-01-24
Inactive: IPC assigned 2002-01-24
Inactive: IPC assigned 2002-01-24
Inactive: First IPC assigned 2002-01-24
Inactive: Inventor deleted 2002-01-11
Inactive: Filing certificate - No RFE (English) 2002-01-11
Inactive: Applicant deleted 2002-01-11
Filing Requirements Determined Compliant 2001-12-07
Inactive: Filing certificate - No RFE (English) 2001-12-07
Application Received - Regular National 2001-12-06
Small Entity Declaration Determined Compliant 2001-11-05

Abandonment History

Abandonment Date Reason Reinstatement Date
2011-11-07
2010-11-05
2010-11-05
2005-11-07

Maintenance Fee

The last payment was received on 2009-10-13

Note : If the full payment has not been received on or before the date indicated, a further fee may be required which may be one of the following

  • the reinstatement fee;
  • the late payment fee; or
  • additional fee to reverse deemed expiry.

Please refer to the CIPO Patent Fees web page to see all current fee amounts.

Fee History

Fee Type Anniversary Year Due Date Paid Date
Application fee - small 2001-11-05
MF (application, 2nd anniv.) - small 02 2003-11-05 2003-10-27
MF (application, 3rd anniv.) - small 03 2004-11-05 2004-11-03
MF (application, 4th anniv.) - small 04 2005-11-07 2005-11-10
Reinstatement 2006-04-25
Request for examination - small 2006-09-21
MF (application, 5th anniv.) - small 05 2006-11-06 2006-10-27
MF (application, 6th anniv.) - small 06 2007-11-05 2007-10-22
MF (application, 7th anniv.) - small 07 2008-11-05 2008-10-23
MF (application, 8th anniv.) - small 08 2009-11-05 2009-10-13
Extension of time 2011-11-07
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
GONZALO A. CADAVIS
Past Owners on Record
None
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Description 2003-02-05 9 366
Abstract 2003-02-05 1 30
Claims 2003-02-05 2 67
Drawings 2003-02-05 5 106
Cover Page 2003-04-23 1 33
Description 2001-11-05 2 62
Description 2007-10-18 12 429
Abstract 2007-10-18 1 28
Claims 2007-10-18 2 57
Description 2008-08-11 13 463
Claims 2008-08-11 2 56
Claims 2009-04-30 2 45
Claims 2010-02-22 2 47
Filing Certificate (English) 2001-12-07 1 163
Filing Certificate (English) 2002-01-11 1 164
Notice: Maintenance Fee Reminder 2003-08-06 1 115
Notice: Maintenance Fee Reminder 2004-08-09 1 119
Notice: Maintenance Fee Reminder 2005-08-08 1 117
Courtesy - Abandonment Letter (Maintenance Fee) 2005-11-22 1 176
Second Notice: Maintenance Fee Reminder 2006-05-08 1 127
Notice of Reinstatement 2006-05-09 1 165
Reminder - Request for Examination 2006-07-06 1 116
Notice: Maintenance Fee Reminder 2006-08-08 1 119
Acknowledgement of Request for Examination 2006-09-29 1 176
Notice: Maintenance Fee Reminder 2007-08-07 1 121
Notice: Maintenance Fee Reminder 2008-08-06 1 122
Notice: Maintenance Fee Reminder 2009-08-06 1 128
Notice: Maintenance Fee Reminder 2010-08-09 1 123
Notice of Insufficient fee payment (English) 2011-01-04 1 93
Courtesy - Abandonment Letter (R30(2)) 2011-04-18 1 165
Second Notice: Maintenance Fee Reminder 2011-07-04 1 121
Courtesy - Abandonment Letter (Maintenance Fee) 2011-06-30 1 173
Notice: Maintenance Fee Reminder 2011-08-08 1 121
Courtesy - Abandonment Letter (Maintenance Fee) 2012-01-03 1 172
Correspondence 2001-12-07 2 40
Correspondence 2002-01-10 1 41
Correspondence 2002-04-01 1 22
Correspondence 2002-04-03 1 17
Correspondence 2003-02-05 19 615
Correspondence 2003-10-27 1 74
Correspondence 2003-11-07 1 14
Fees 2003-10-27 1 74
Fees 2004-11-03 2 53
Correspondence 2005-11-22 1 20
Fees 2005-11-10 1 25
Fees 2006-04-25 1 35
Fees 2006-10-27 2 141
Fees 2008-10-23 1 30
Fees 2009-10-13 1 24
Fees 2010-11-05 4 172
Fees 2010-11-05 4 172
Correspondence 2011-03-14 2 18
Fees 2011-03-03 1 25
Correspondence 2011-07-04 1 22
Fees 2011-06-29 3 133
Correspondence 2011-12-12 2 47
Correspondence 2011-12-13 2 52
Fees 2011-11-07 1 21