
Anne Bidwell
Examiner (ID: 184)
| Most Active Art Unit | 3105 |
| Art Unit(s) | 3105, 3107 |
| Total Applications | 344 |
| Issued Applications | 320 |
| Pending Applications | 0 |
| Abandoned Applications | 24 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2836590
[patent_doc_number] => 05088665
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-18
[patent_title] => 'Serrated trailing edges for improving lift and drag characteristics of lifting surfaces'
[patent_app_type] => 1
[patent_app_number] => 7/429516
[patent_app_country] => US
[patent_app_date] => 1989-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 17
[patent_no_of_words] => 2979
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 10
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/088/05088665.pdf
[firstpage_image] =>[orig_patent_app_number] => 429516
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/429516 | Serrated trailing edges for improving lift and drag characteristics of lifting surfaces | Oct 30, 1989 | Issued |
Array
(
[id] => 2838868
[patent_doc_number] => 05112012
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-12
[patent_title] => 'Tilting momentum wheel for spacecraft'
[patent_app_type] => 1
[patent_app_number] => 7/427675
[patent_app_country] => US
[patent_app_date] => 1989-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 21
[patent_no_of_words] => 3996
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/112/05112012.pdf
[firstpage_image] =>[orig_patent_app_number] => 427675
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/427675 | Tilting momentum wheel for spacecraft | Oct 25, 1989 | Issued |
Array
(
[id] => 2680796
[patent_doc_number] => 04989809
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-02-05
[patent_title] => 'Removable aircraft floor structure-reinforcing strongback'
[patent_app_type] => 1
[patent_app_number] => 7/427978
[patent_app_country] => US
[patent_app_date] => 1989-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2256
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/989/04989809.pdf
[firstpage_image] =>[orig_patent_app_number] => 427978
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/427978 | Removable aircraft floor structure-reinforcing strongback | Oct 24, 1989 | Issued |
Array
(
[id] => 2865203
[patent_doc_number] => 05108050
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-28
[patent_title] => 'Autonomous orbit control method and system for a geostationary satellite'
[patent_app_type] => 1
[patent_app_number] => 7/416694
[patent_app_country] => US
[patent_app_date] => 1989-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3395
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 219
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/108/05108050.pdf
[firstpage_image] =>[orig_patent_app_number] => 416694
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/416694 | Autonomous orbit control method and system for a geostationary satellite | Oct 2, 1989 | Issued |
Array
(
[id] => 2659703
[patent_doc_number] => 05072894
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-17
[patent_title] => 'Apparatus and method for increasing the angle of attack operating range of an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/415676
[patent_app_country] => US
[patent_app_date] => 1989-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2059
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/072/05072894.pdf
[firstpage_image] =>[orig_patent_app_number] => 415676
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/415676 | Apparatus and method for increasing the angle of attack operating range of an aircraft | Oct 1, 1989 | Issued |
Array
(
[id] => 2656670
[patent_doc_number] => 05033697
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-23
[patent_title] => 'Pilot head support apparatus'
[patent_app_type] => 1
[patent_app_number] => 7/415695
[patent_app_country] => US
[patent_app_date] => 1989-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2267
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/033/05033697.pdf
[firstpage_image] =>[orig_patent_app_number] => 415695
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/415695 | Pilot head support apparatus | Oct 1, 1989 | Issued |
Array
(
[id] => 2757465
[patent_doc_number] => 05074489
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-24
[patent_title] => 'Method and system for supporting an airborne vehicle in space'
[patent_app_type] => 1
[patent_app_number] => 7/415734
[patent_app_country] => US
[patent_app_date] => 1989-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1840
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 124
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/074/05074489.pdf
[firstpage_image] =>[orig_patent_app_number] => 415734
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/415734 | Method and system for supporting an airborne vehicle in space | Oct 1, 1989 | Issued |
Array
(
[id] => 2736062
[patent_doc_number] => 05020746
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-04
[patent_title] => 'Method for satellite station keeping'
[patent_app_type] => 1
[patent_app_number] => 7/415005
[patent_app_country] => US
[patent_app_date] => 1989-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3538
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/020/05020746.pdf
[firstpage_image] =>[orig_patent_app_number] => 415005
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/415005 | Method for satellite station keeping | Sep 28, 1989 | Issued |
Array
(
[id] => 2770831
[patent_doc_number] => 05092543
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-03
[patent_title] => 'Spacecraft attitude control with avoidance constraint'
[patent_app_type] => 1
[patent_app_number] => 7/413136
[patent_app_country] => US
[patent_app_date] => 1989-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2931
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/092/05092543.pdf
[firstpage_image] =>[orig_patent_app_number] => 413136
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/413136 | Spacecraft attitude control with avoidance constraint | Sep 26, 1989 | Issued |
Array
(
[id] => 2865117
[patent_doc_number] => 05108048
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-28
[patent_title] => 'Stowage bin and support panel system for convertible aircraft and method of installation'
[patent_app_type] => 1
[patent_app_number] => 7/407606
[patent_app_country] => US
[patent_app_date] => 1989-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 22
[patent_no_of_words] => 6493
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/108/05108048.pdf
[firstpage_image] =>[orig_patent_app_number] => 407606
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/407606 | Stowage bin and support panel system for convertible aircraft and method of installation | Sep 14, 1989 | Issued |
Array
(
[id] => 2752227
[patent_doc_number] => 05005786
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-09
[patent_title] => 'Docking and active damping device for space structures'
[patent_app_type] => 1
[patent_app_number] => 7/402586
[patent_app_country] => US
[patent_app_date] => 1989-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 11
[patent_no_of_words] => 6377
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/005/05005786.pdf
[firstpage_image] =>[orig_patent_app_number] => 402586
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/402586 | Docking and active damping device for space structures | Sep 4, 1989 | Issued |
Array
(
[id] => 2657493
[patent_doc_number] => 05026004
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-25
[patent_title] => 'Variable air intake ramps for aerospace vehicles'
[patent_app_type] => 1
[patent_app_number] => 7/398866
[patent_app_country] => US
[patent_app_date] => 1989-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1179
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/026/05026004.pdf
[firstpage_image] =>[orig_patent_app_number] => 398866
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/398866 | Variable air intake ramps for aerospace vehicles | Aug 24, 1989 | Issued |
Array
(
[id] => 2584975
[patent_doc_number] => 04930579
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-06-05
[patent_title] => 'Fire extinguishing device for the home heating plant utilizing an existing spigot as the water source'
[patent_app_type] => 1
[patent_app_number] => 7/396740
[patent_app_country] => US
[patent_app_date] => 1989-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2194
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/930/04930579.pdf
[firstpage_image] =>[orig_patent_app_number] => 396740
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/396740 | Fire extinguishing device for the home heating plant utilizing an existing spigot as the water source | Aug 17, 1989 | Issued |
Array
(
[id] => 2721021
[patent_doc_number] => 05076517
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-31
[patent_title] => 'Programmable, linear collective control system for a helicopter'
[patent_app_type] => 1
[patent_app_number] => 7/393346
[patent_app_country] => US
[patent_app_date] => 1989-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3965
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/076/05076517.pdf
[firstpage_image] =>[orig_patent_app_number] => 393346
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/393346 | Programmable, linear collective control system for a helicopter | Aug 13, 1989 | Issued |
Array
(
[id] => 2656170
[patent_doc_number] => 04982798
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-01-08
[patent_title] => 'Extinguisher for use in an automobile'
[patent_app_type] => 1
[patent_app_number] => 7/379187
[patent_app_country] => US
[patent_app_date] => 1989-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1146
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/982/04982798.pdf
[firstpage_image] =>[orig_patent_app_number] => 379187
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/379187 | Extinguisher for use in an automobile | Jul 11, 1989 | Issued |
Array
(
[id] => 2655396
[patent_doc_number] => 05046685
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-09-10
[patent_title] => 'Fixed circular wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/376716
[patent_app_country] => US
[patent_app_date] => 1989-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3103
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 299
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/046/05046685.pdf
[firstpage_image] =>[orig_patent_app_number] => 376716
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/376716 | Fixed circular wing aircraft | Jul 6, 1989 | Issued |
Array
(
[id] => 2751907
[patent_doc_number] => 04993887
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-02-19
[patent_title] => 'Compensator for solids conveyed in a stream of gas'
[patent_app_type] => 1
[patent_app_number] => 7/376397
[patent_app_country] => US
[patent_app_date] => 1989-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 927
[patent_no_of_claims] => 8
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[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/993/04993887.pdf
[firstpage_image] =>[orig_patent_app_number] => 376397
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/376397 | Compensator for solids conveyed in a stream of gas | Jul 5, 1989 | Issued |
Array
(
[id] => 2756651
[patent_doc_number] => 05006019
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-09
[patent_title] => 'Pneumatic pickup probe'
[patent_app_type] => 1
[patent_app_number] => 7/375458
[patent_app_country] => US
[patent_app_date] => 1989-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/006/05006019.pdf
[firstpage_image] =>[orig_patent_app_number] => 375458
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/375458 | Pneumatic pickup probe | Jun 28, 1989 | Issued |
Array
(
[id] => 2711982
[patent_doc_number] => 05024398
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-18
[patent_title] => 'Office module for passenger aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/372535
[patent_app_country] => US
[patent_app_date] => 1989-06-28
[patent_effective_date] => 0000-00-00
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/024/05024398.pdf
[firstpage_image] =>[orig_patent_app_number] => 372535
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/372535 | Office module for passenger aircraft | Jun 27, 1989 | Issued |
Array
(
[id] => 2733513
[patent_doc_number] => 04986497
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-01-22
[patent_title] => 'Aircraft-de-icing system'
[patent_app_type] => 1
[patent_app_number] => 7/367424
[patent_app_country] => US
[patent_app_date] => 1989-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/986/04986497.pdf
[firstpage_image] =>[orig_patent_app_number] => 367424
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/367424 | Aircraft-de-icing system | Jun 15, 1989 | Issued |