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] => 4087350 [patent_doc_number] => 06065718 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-23 [patent_title] => 'Universal VTOL power and rotor system module' [patent_app_type] => 1 [patent_app_number] => 9/045991 [patent_app_country] => US [patent_app_date] => 1998-03-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3052 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/065/06065718.pdf [firstpage_image] =>[orig_patent_app_number] => 045991 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/045991
Universal VTOL power and rotor system module Mar 22, 1998 Issued
Array ( [id] => 4226881 [patent_doc_number] => 06135389 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-10-24 [patent_title] => 'Subterranean target steering strategy' [patent_app_type] => 1 [patent_app_number] => 9/039883 [patent_app_country] => US [patent_app_date] => 1998-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5215 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/135/06135389.pdf [firstpage_image] =>[orig_patent_app_number] => 039883 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/039883
Subterranean target steering strategy Mar 15, 1998 Issued
Array ( [id] => 4204746 [patent_doc_number] => 06039290 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-03-21 [patent_title] => 'Robust singularity avoidance in satellite attitude control' [patent_app_type] => 1 [patent_app_number] => 9/039959 [patent_app_country] => US [patent_app_date] => 1998-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1490 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/039/06039290.pdf [firstpage_image] =>[orig_patent_app_number] => 039959 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/039959
Robust singularity avoidance in satellite attitude control Mar 15, 1998 Issued
Array ( [id] => 4083522 [patent_doc_number] => 06098923 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-08-08 [patent_title] => 'Aircraft structure to improve directional stability' [patent_app_type] => 1 [patent_app_number] => 9/042278 [patent_app_country] => US [patent_app_date] => 1998-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 5161 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/098/06098923.pdf [firstpage_image] =>[orig_patent_app_number] => 042278 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/042278
Aircraft structure to improve directional stability Mar 12, 1998 Issued
Array ( [id] => 4155396 [patent_doc_number] => 06082667 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-07-04 [patent_title] => 'Inflated wing' [patent_app_type] => 1 [patent_app_number] => 9/041161 [patent_app_country] => US [patent_app_date] => 1998-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 859 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/082/06082667.pdf [firstpage_image] =>[orig_patent_app_number] => 041161 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/041161
Inflated wing Mar 11, 1998 Issued
Array ( [id] => 6885820 [patent_doc_number] => 20010019089 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2001-09-06 [patent_title] => 'AVIATION CRASH SENSOR' [patent_app_type] => new [patent_app_number] => 09/041338 [patent_app_country] => US [patent_app_date] => 1998-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4164 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0019/20010019089.pdf [firstpage_image] =>[orig_patent_app_number] => 09041338 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/041338
Aviation crash sensor Mar 11, 1998 Issued
Array ( [id] => 4267803 [patent_doc_number] => 06209825 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-03 [patent_title] => 'Low power loss electro hydraulic actuator' [patent_app_type] => 1 [patent_app_number] => 9/031985 [patent_app_country] => US [patent_app_date] => 1998-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3441 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 252 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/209/06209825.pdf [firstpage_image] =>[orig_patent_app_number] => 031985 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/031985
Low power loss electro hydraulic actuator Feb 26, 1998 Issued
Array ( [id] => 4166353 [patent_doc_number] => 06158691 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-12-12 [patent_title] => 'Process for preventing turning over during the landing of an aircraft or spacecraft' [patent_app_type] => 1 [patent_app_number] => 9/032280 [patent_app_country] => US [patent_app_date] => 1998-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 2333 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/158/06158691.pdf [firstpage_image] =>[orig_patent_app_number] => 032280 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/032280
Process for preventing turning over during the landing of an aircraft or spacecraft Feb 26, 1998 Issued
Array ( [id] => 4192850 [patent_doc_number] => 06027078 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-02-22 [patent_title] => 'Method and apparatus using localized heating for laminar flow' [patent_app_type] => 1 [patent_app_number] => 9/032185 [patent_app_country] => US [patent_app_date] => 1998-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 3957 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/027/06027078.pdf [firstpage_image] =>[orig_patent_app_number] => 032185 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/032185
Method and apparatus using localized heating for laminar flow Feb 26, 1998 Issued
Array ( [id] => 4409771 [patent_doc_number] => 06176450 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-01-23 [patent_title] => 'Protective mat' [patent_app_type] => 1 [patent_app_number] => 9/032498 [patent_app_country] => US [patent_app_date] => 1998-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 1611 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/176/06176450.pdf [firstpage_image] =>[orig_patent_app_number] => 032498 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/032498
Protective mat Feb 25, 1998 Issued
Array ( [id] => 4114243 [patent_doc_number] => 06032903 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-03-07 [patent_title] => 'Cooperative control structures and methods for satellite spin axis control' [patent_app_type] => 1 [patent_app_number] => 9/022991 [patent_app_country] => US [patent_app_date] => 1998-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 6894 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/032/06032903.pdf [firstpage_image] =>[orig_patent_app_number] => 022991 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/022991
Cooperative control structures and methods for satellite spin axis control Feb 11, 1998 Issued
Array ( [id] => 4273859 [patent_doc_number] => 06179251 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-01-30 [patent_title] => 'Thin inlet lip design for low drag and reduced nacelle size' [patent_app_type] => 1 [patent_app_number] => 9/020081 [patent_app_country] => US [patent_app_date] => 1998-02-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2698 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/179/06179251.pdf [firstpage_image] =>[orig_patent_app_number] => 020081 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/020081
Thin inlet lip design for low drag and reduced nacelle size Feb 5, 1998 Issued
Array ( [id] => 4137574 [patent_doc_number] => 06113036 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-09-05 [patent_title] => 'Boundary layer control system' [patent_app_type] => 1 [patent_app_number] => 9/018689 [patent_app_country] => US [patent_app_date] => 1998-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2409 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 203 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/113/06113036.pdf [firstpage_image] =>[orig_patent_app_number] => 018689 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/018689
Boundary layer control system Feb 3, 1998 Issued
Array ( [id] => 4184225 [patent_doc_number] => 06012678 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-01-11 [patent_title] => 'Galley vacuum waste disposal system' [patent_app_type] => 1 [patent_app_number] => 9/013386 [patent_app_country] => US [patent_app_date] => 1998-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1748 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 216 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/012/06012678.pdf [firstpage_image] =>[orig_patent_app_number] => 013386 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/013386
Galley vacuum waste disposal system Jan 25, 1998 Issued
Array ( [id] => 4178856 [patent_doc_number] => 06129314 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-10-10 [patent_title] => 'Hybrid deicer with element sequence' [patent_app_type] => 1 [patent_app_number] => 9/010379 [patent_app_country] => US [patent_app_date] => 1998-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 10436 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/129/06129314.pdf [firstpage_image] =>[orig_patent_app_number] => 010379 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/010379
Hybrid deicer with element sequence Jan 20, 1998 Issued
Array ( [id] => 4128427 [patent_doc_number] => 06062509 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-16 [patent_title] => 'Retrofit centerline luggage bin assemblies compatible with existing aircraft bin supports' [patent_app_type] => 1 [patent_app_number] => 9/009756 [patent_app_country] => US [patent_app_date] => 1998-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1734 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/062/06062509.pdf [firstpage_image] =>[orig_patent_app_number] => 009756 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/009756
Retrofit centerline luggage bin assemblies compatible with existing aircraft bin supports Jan 19, 1998 Issued
Array ( [id] => 4166368 [patent_doc_number] => 06158692 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-12-12 [patent_title] => 'Main deck cargo door electric lock system' [patent_app_type] => 1 [patent_app_number] => 9/008279 [patent_app_country] => US [patent_app_date] => 1998-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 1811 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/158/06158692.pdf [firstpage_image] =>[orig_patent_app_number] => 008279 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/008279
Main deck cargo door electric lock system Jan 15, 1998 Issued
Array ( [id] => 3914988 [patent_doc_number] => 05938147 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-08-17 [patent_title] => 'Safety pitot tube cover' [patent_app_type] => 1 [patent_app_number] => 9/005785 [patent_app_country] => US [patent_app_date] => 1998-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 2866 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/938/05938147.pdf [firstpage_image] =>[orig_patent_app_number] => 005785 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/005785
Safety pitot tube cover Jan 11, 1998 Issued
Array ( [id] => 4232178 [patent_doc_number] => 06206329 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-03-27 [patent_title] => 'Process and device for the control of the rudder of an aircraft' [patent_app_type] => 1 [patent_app_number] => 9/003890 [patent_app_country] => US [patent_app_date] => 1998-01-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 5621 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/206/06206329.pdf [firstpage_image] =>[orig_patent_app_number] => 003890 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/003890
Process and device for the control of the rudder of an aircraft Jan 6, 1998 Issued
Array ( [id] => 4094603 [patent_doc_number] => 06021976 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-02-08 [patent_title] => 'Operation of a helicopter' [patent_app_type] => 1 [patent_app_number] => 8/981888 [patent_app_country] => US [patent_app_date] => 1998-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2474 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/021/06021976.pdf [firstpage_image] =>[orig_patent_app_number] => 981888 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/981888
Operation of a helicopter Jan 4, 1998 Issued
Menu