Search

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 numberTitle of the applicationFiling DateStatus
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
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