
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] => 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
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[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
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[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
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[patent_no_of_words] => 2409
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[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
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[patent_no_of_words] => 1748
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |