
Amanda Lee Bailey
Examiner (ID: 4785)
| Most Active Art Unit | 3673 |
| Art Unit(s) | 3673 |
| Total Applications | 468 |
| Issued Applications | 245 |
| Pending Applications | 48 |
| Abandoned Applications | 191 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 1190644
[patent_doc_number] => 06729579
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-05-04
[patent_title] => 'Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same'
[patent_app_type] => B1
[patent_app_number] => 09/366533
[patent_app_country] => US
[patent_app_date] => 1999-08-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2005
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/729/06729579.pdf
[firstpage_image] =>[orig_patent_app_number] => 09366533
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/366533 | Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same | Aug 3, 1999 | Issued |
Array
(
[id] => 1439790
[patent_doc_number] => 06334588
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-01-01
[patent_title] => 'Aircraft propulsion unit fan cowls equipped with maintaining and positioning safety elements'
[patent_app_type] => B1
[patent_app_number] => 09/341573
[patent_app_country] => US
[patent_app_date] => 1999-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 4607
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/334/06334588.pdf
[firstpage_image] =>[orig_patent_app_number] => 09341573
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/341573 | Aircraft propulsion unit fan cowls equipped with maintaining and positioning safety elements | Aug 1, 1999 | Issued |
Array
(
[id] => 4257071
[patent_doc_number] => 06279856
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-08-28
[patent_title] => 'Aircraft de-icing system'
[patent_app_type] => 1
[patent_app_number] => 9/364804
[patent_app_country] => US
[patent_app_date] => 1999-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 43
[patent_no_of_words] => 13182
[patent_no_of_claims] => 53
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/279/06279856.pdf
[firstpage_image] =>[orig_patent_app_number] => 364804
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/364804 | Aircraft de-icing system | Jul 29, 1999 | Issued |
Array
(
[id] => 4329087
[patent_doc_number] => 06213426
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-04-10
[patent_title] => 'Monolithic structure with redundant load paths'
[patent_app_type] => 1
[patent_app_number] => 9/351044
[patent_app_country] => US
[patent_app_date] => 1999-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3211
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/213/06213426.pdf
[firstpage_image] =>[orig_patent_app_number] => 351044
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/351044 | Monolithic structure with redundant load paths | Jul 8, 1999 | Issued |
Array
(
[id] => 4351253
[patent_doc_number] => 06286787
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-09-11
[patent_title] => 'Small satellite GEO-to-LEO orbit transfer vehicle'
[patent_app_type] => 1
[patent_app_number] => 9/350813
[patent_app_country] => US
[patent_app_date] => 1999-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2888
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/286/06286787.pdf
[firstpage_image] =>[orig_patent_app_number] => 350813
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/350813 | Small satellite GEO-to-LEO orbit transfer vehicle | Jul 8, 1999 | Issued |
Array
(
[id] => 4226973
[patent_doc_number] => 06135395
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-24
[patent_title] => 'Aircraft wing leading edge high lift device with suction'
[patent_app_type] => 1
[patent_app_number] => 9/349453
[patent_app_country] => US
[patent_app_date] => 1999-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2247
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/135/06135395.pdf
[firstpage_image] =>[orig_patent_app_number] => 349453
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/349453 | Aircraft wing leading edge high lift device with suction | Jul 7, 1999 | Issued |
| 09/284064 | PRESTRESSED STRUCTURE FOR AIRCRAFT AND THE METHOD OF PRODUCING THE SAME | Jul 7, 1999 | Abandoned |
Array
(
[id] => 4217647
[patent_doc_number] => 06142422
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-07
[patent_title] => 'Method to reorient a spacecraft using only initial single axis attitude knowledge'
[patent_app_type] => 1
[patent_app_number] => 9/337078
[patent_app_country] => US
[patent_app_date] => 1999-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 18
[patent_no_of_words] => 5161
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 90
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/142/06142422.pdf
[firstpage_image] =>[orig_patent_app_number] => 337078
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/337078 | Method to reorient a spacecraft using only initial single axis attitude knowledge | Jun 20, 1999 | Issued |
Array
(
[id] => 4276392
[patent_doc_number] => 06196500
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-03-06
[patent_title] => 'Hybrid ice protection system for use on roughness-sensitive airfoils'
[patent_app_type] => 1
[patent_app_number] => 9/330444
[patent_app_country] => US
[patent_app_date] => 1999-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2771
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/196/06196500.pdf
[firstpage_image] =>[orig_patent_app_number] => 330444
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/330444 | Hybrid ice protection system for use on roughness-sensitive airfoils | Jun 10, 1999 | Issued |
Array
(
[id] => 1562701
[patent_doc_number] => 06338455
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-01-15
[patent_title] => 'Heating device with resistive elements for an aerodynamic profile'
[patent_app_type] => B1
[patent_app_number] => 09/318364
[patent_app_country] => US
[patent_app_date] => 1999-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 14
[patent_no_of_words] => 4545
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/338/06338455.pdf
[firstpage_image] =>[orig_patent_app_number] => 09318364
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/318364 | Heating device with resistive elements for an aerodynamic profile | May 24, 1999 | Issued |
Array
(
[id] => 1591030
[patent_doc_number] => 06491259
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-10
[patent_title] => 'Halogenated composites for oxygen systems'
[patent_app_type] => B1
[patent_app_number] => 09/309804
[patent_app_country] => US
[patent_app_date] => 1999-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 5064
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 52
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/491/06491259.pdf
[firstpage_image] =>[orig_patent_app_number] => 09309804
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/309804 | Halogenated composites for oxygen systems | May 10, 1999 | Issued |
Array
(
[id] => 4257045
[patent_doc_number] => 06279854
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-08-28
[patent_title] => 'Combined damper and truck positioner for landing gear'
[patent_app_type] => 1
[patent_app_number] => 9/302233
[patent_app_country] => US
[patent_app_date] => 1999-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5337
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 292
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/279/06279854.pdf
[firstpage_image] =>[orig_patent_app_number] => 302233
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/302233 | Combined damper and truck positioner for landing gear | Apr 28, 1999 | Issued |
Array
(
[id] => 1514361
[patent_doc_number] => 06499691
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-31
[patent_title] => 'Method of rotating aircraft wheels'
[patent_app_type] => B1
[patent_app_number] => 09/299453
[patent_app_country] => US
[patent_app_date] => 1999-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1088
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/499/06499691.pdf
[firstpage_image] =>[orig_patent_app_number] => 09299453
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/299453 | Method of rotating aircraft wheels | Apr 25, 1999 | Issued |
Array
(
[id] => 4389320
[patent_doc_number] => 06270038
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-08-07
[patent_title] => 'Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop'
[patent_app_type] => 1
[patent_app_number] => 9/296624
[patent_app_country] => US
[patent_app_date] => 1999-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 6161
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/270/06270038.pdf
[firstpage_image] =>[orig_patent_app_number] => 296624
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/296624 | Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop | Apr 21, 1999 | Issued |
Array
(
[id] => 4226896
[patent_doc_number] => 06135390
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-10-24
[patent_title] => 'Whole-spacecraft hybrid isolation system for launch vehicles'
[patent_app_type] => 1
[patent_app_number] => 9/277595
[patent_app_country] => US
[patent_app_date] => 1999-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 1285
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/135/06135390.pdf
[firstpage_image] =>[orig_patent_app_number] => 277595
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/277595 | Whole-spacecraft hybrid isolation system for launch vehicles | Mar 25, 1999 | Issued |
Array
(
[id] => 4216178
[patent_doc_number] => 06164598
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-12-26
[patent_title] => 'Adaptive control surface apparatus'
[patent_app_type] => 1
[patent_app_number] => 9/265671
[patent_app_country] => US
[patent_app_date] => 1999-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 15
[patent_no_of_words] => 5016
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/164/06164598.pdf
[firstpage_image] =>[orig_patent_app_number] => 265671
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/265671 | Adaptive control surface apparatus | Mar 9, 1999 | Issued |
Array
(
[id] => 4394258
[patent_doc_number] => 06308913
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-30
[patent_title] => 'Method for reducing wave resistance in airplane'
[patent_app_type] => 1
[patent_app_number] => 9/264894
[patent_app_country] => US
[patent_app_date] => 1999-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 20
[patent_no_of_words] => 7936
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 233
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/308/06308913.pdf
[firstpage_image] =>[orig_patent_app_number] => 264894
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/264894 | Method for reducing wave resistance in airplane | Mar 8, 1999 | Issued |
Array
(
[id] => 4393416
[patent_doc_number] => 06299106
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-09
[patent_title] => 'Thermal insulation utilizing a low profile snap fastener'
[patent_app_type] => 1
[patent_app_number] => 9/264605
[patent_app_country] => US
[patent_app_date] => 1999-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 2514
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/299/06299106.pdf
[firstpage_image] =>[orig_patent_app_number] => 264605
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/264605 | Thermal insulation utilizing a low profile snap fastener | Mar 8, 1999 | Issued |
| 09/264700 | METHOD AND APPARATUS FOR POSITIONING A LOW COST, LONG DURATION HIGH ALTITUDE INSTRUMENT PLATFORM UTILIZING UNMANNED AIRBORNE VEHICLES | Mar 7, 1999 | Abandoned |
Array
(
[id] => 4364500
[patent_doc_number] => 06260804
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-07-17
[patent_title] => 'Functionally and structurally modular parallelogram-shaped spacecraft'
[patent_app_type] => 1
[patent_app_number] => 9/262003
[patent_app_country] => US
[patent_app_date] => 1999-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 18
[patent_no_of_words] => 3244
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/260/06260804.pdf
[firstpage_image] =>[orig_patent_app_number] => 262003
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/262003 | Functionally and structurally modular parallelogram-shaped spacecraft | Mar 3, 1999 | Issued |