
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] => 2766079
[patent_doc_number] => 05150858
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-29
[patent_title] => 'Jettisonable aerodynamic control surfaces'
[patent_app_type] => 1
[patent_app_number] => 7/491934
[patent_app_country] => US
[patent_app_date] => 1990-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 1366
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/150/05150858.pdf
[firstpage_image] =>[orig_patent_app_number] => 491934
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/491934 | Jettisonable aerodynamic control surfaces | Mar 11, 1990 | Issued |
Array
(
[id] => 2773479
[patent_doc_number] => 05100083
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-31
[patent_title] => 'Retractable landing gear with self-braced folding strut'
[patent_app_type] => 1
[patent_app_number] => 7/479516
[patent_app_country] => US
[patent_app_date] => 1990-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 20
[patent_no_of_words] => 6210
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/100/05100083.pdf
[firstpage_image] =>[orig_patent_app_number] => 479516
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/479516 | Retractable landing gear with self-braced folding strut | Feb 12, 1990 | Issued |
Array
(
[id] => 2693549
[patent_doc_number] => 05067673
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-11-26
[patent_title] => 'Essentially passive method for inverting the orientation of a dual spin spacecraft'
[patent_app_type] => 1
[patent_app_number] => 7/477274
[patent_app_country] => US
[patent_app_date] => 1990-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 4368
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 190
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/067/05067673.pdf
[firstpage_image] =>[orig_patent_app_number] => 477274
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/477274 | Essentially passive method for inverting the orientation of a dual spin spacecraft | Feb 6, 1990 | Issued |
Array
(
[id] => 2810114
[patent_doc_number] => 05115996
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-26
[patent_title] => 'VTOL aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/472696
[patent_app_country] => US
[patent_app_date] => 1990-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 25
[patent_no_of_words] => 10385
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 26
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/115/05115996.pdf
[firstpage_image] =>[orig_patent_app_number] => 472696
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/472696 | VTOL aircraft | Jan 30, 1990 | Issued |
Array
(
[id] => 2783109
[patent_doc_number] => 05143328
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-01
[patent_title] => 'Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters'
[patent_app_type] => 1
[patent_app_number] => 7/472096
[patent_app_country] => US
[patent_app_date] => 1990-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 20
[patent_no_of_words] => 13125
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/143/05143328.pdf
[firstpage_image] =>[orig_patent_app_number] => 472096
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/472096 | Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters | Jan 29, 1990 | Issued |
Array
(
[id] => 2913595
[patent_doc_number] => 05186419
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'Space transfer vehicle and integrated guidance launch system'
[patent_app_type] => 1
[patent_app_number] => 7/472395
[patent_app_country] => US
[patent_app_date] => 1990-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2543
[patent_no_of_claims] => 3
[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/05/186/05186419.pdf
[firstpage_image] =>[orig_patent_app_number] => 472395
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/472395 | Space transfer vehicle and integrated guidance launch system | Jan 29, 1990 | Issued |
Array
(
[id] => 2796845
[patent_doc_number] => 05078338
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-07
[patent_title] => 'Means for maintaining a desired relationship between roll and yaw stability in a swept-wing aircraft by varying dihedral as a function of lift coefficient'
[patent_app_type] => 1
[patent_app_number] => 7/467534
[patent_app_country] => US
[patent_app_date] => 1990-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 9352
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 306
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/078/05078338.pdf
[firstpage_image] =>[orig_patent_app_number] => 467534
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/467534 | Means for maintaining a desired relationship between roll and yaw stability in a swept-wing aircraft by varying dihedral as a function of lift coefficient | Jan 18, 1990 | Issued |
Array
(
[id] => 2858408
[patent_doc_number] => 05090641
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-25
[patent_title] => 'Casing for a parachute'
[patent_app_type] => 1
[patent_app_number] => 7/463615
[patent_app_country] => US
[patent_app_date] => 1990-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2431
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/090/05090641.pdf
[firstpage_image] =>[orig_patent_app_number] => 463615
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/463615 | Casing for a parachute | Jan 10, 1990 | Issued |
Array
(
[id] => 2730244
[patent_doc_number] => 05011100
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-04-30
[patent_title] => 'Kite'
[patent_app_type] => 1
[patent_app_number] => 7/463174
[patent_app_country] => US
[patent_app_date] => 1990-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1991
[patent_no_of_claims] => 8
[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/05/011/05011100.pdf
[firstpage_image] =>[orig_patent_app_number] => 463174
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/463174 | Kite | Jan 9, 1990 | Issued |
Array
(
[id] => 2731413
[patent_doc_number] => 05022610
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-11
[patent_title] => 'Retracting ramp toe'
[patent_app_type] => 1
[patent_app_number] => 7/462726
[patent_app_country] => US
[patent_app_date] => 1990-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 17
[patent_no_of_words] => 2312
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 278
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/022/05022610.pdf
[firstpage_image] =>[orig_patent_app_number] => 462726
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/462726 | Retracting ramp toe | Jan 8, 1990 | Issued |
Array
(
[id] => 2821833
[patent_doc_number] => 05120006
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-09
[patent_title] => 'Kite-like flying device with independent wing surface control'
[patent_app_type] => 1
[patent_app_number] => 7/462124
[patent_app_country] => US
[patent_app_date] => 1990-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 18
[patent_no_of_words] => 5694
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/120/05120006.pdf
[firstpage_image] =>[orig_patent_app_number] => 462124
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/462124 | Kite-like flying device with independent wing surface control | Jan 7, 1990 | Issued |
| 07/461975 | COMPOUND HELICOPTER WITH ENGINE SHAFT POWER OUTPUT CONTROL | Jan 7, 1990 | Abandoned |
Array
(
[id] => 2773514
[patent_doc_number] => 05100085
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-31
[patent_title] => 'Aircraft wingtip vorticity redistribution apparatus'
[patent_app_type] => 1
[patent_app_number] => 7/458844
[patent_app_country] => US
[patent_app_date] => 1989-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 11
[patent_no_of_words] => 6276
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/100/05100085.pdf
[firstpage_image] =>[orig_patent_app_number] => 458844
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/458844 | Aircraft wingtip vorticity redistribution apparatus | Dec 28, 1989 | Issued |
Array
(
[id] => 2831092
[patent_doc_number] => 05106035
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-21
[patent_title] => 'Aircraft propulsion system using air liquefaction and storage'
[patent_app_type] => 1
[patent_app_number] => 7/459254
[patent_app_country] => US
[patent_app_date] => 1989-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3331
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/106/05106035.pdf
[firstpage_image] =>[orig_patent_app_number] => 459254
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/459254 | Aircraft propulsion system using air liquefaction and storage | Dec 28, 1989 | Issued |
Array
(
[id] => 2680871
[patent_doc_number] => 05064151
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-11-12
[patent_title] => 'Assured crew return vehicle'
[patent_app_type] => 1
[patent_app_number] => 7/458476
[patent_app_country] => US
[patent_app_date] => 1989-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 35
[patent_figures_cnt] => 38
[patent_no_of_words] => 17655
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/064/05064151.pdf
[firstpage_image] =>[orig_patent_app_number] => 458476
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/458476 | Assured crew return vehicle | Dec 27, 1989 | Issued |
Array
(
[id] => 2719889
[patent_doc_number] => 05031863
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-16
[patent_title] => 'Upward/outward opening, plug-type overwing emergency exit hatch'
[patent_app_type] => 1
[patent_app_number] => 7/454686
[patent_app_country] => US
[patent_app_date] => 1989-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 11
[patent_no_of_words] => 5751
[patent_no_of_claims] => 13
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[patent_words_short_claim] => 242
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/031/05031863.pdf
[firstpage_image] =>[orig_patent_app_number] => 454686
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/454686 | Upward/outward opening, plug-type overwing emergency exit hatch | Dec 20, 1989 | Issued |
Array
(
[id] => 2719827
[patent_doc_number] => 05031860
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-07-16
[patent_title] => 'Integrated capsulized cabin for passenger aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/447785
[patent_app_country] => US
[patent_app_date] => 1989-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 1099
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 228
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/031/05031860.pdf
[firstpage_image] =>[orig_patent_app_number] => 447785
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/447785 | Integrated capsulized cabin for passenger aircraft | Dec 7, 1989 | Issued |
Array
(
[id] => 2694944
[patent_doc_number] => 05060887
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-10-29
[patent_title] => 'Apparatus for deicing an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/446625
[patent_app_country] => US
[patent_app_date] => 1989-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 10
[patent_no_of_words] => 1378
[patent_no_of_claims] => 1
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[patent_words_short_claim] => 371
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/060/05060887.pdf
[firstpage_image] =>[orig_patent_app_number] => 446625
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/446625 | Apparatus for deicing an aircraft | Dec 5, 1989 | Issued |
Array
(
[id] => 2693068
[patent_doc_number] => 05054715
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-10-08
[patent_title] => 'Apparatus and methods for reducing aircraft lifting surface flutter'
[patent_app_type] => 1
[patent_app_number] => 7/442094
[patent_app_country] => US
[patent_app_date] => 1989-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/054/05054715.pdf
[firstpage_image] =>[orig_patent_app_number] => 442094
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/442094 | Apparatus and methods for reducing aircraft lifting surface flutter | Nov 27, 1989 | Issued |
Array
(
[id] => 2642681
[patent_doc_number] => 04928908
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1990-05-29
[patent_title] => 'Balloon made of metal vapor deposited film'
[patent_app_type] => 1
[patent_app_number] => 7/437767
[patent_app_country] => US
[patent_app_date] => 1989-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/04/928/04928908.pdf
[firstpage_image] =>[orig_patent_app_number] => 437767
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/437767 | Balloon made of metal vapor deposited film | Nov 15, 1989 | Issued |