
Lissi Mojica Marquis
Examiner (ID: 12147)
| Most Active Art Unit | 3104 |
| Art Unit(s) | 3614, 3661, 3104, 3105, 3107, 3613 |
| Total Applications | 667 |
| Issued Applications | 565 |
| Pending Applications | 34 |
| Abandoned Applications | 68 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
| 08/140555 | FOILS: HYDROFOILS AND AIRFOILS | Oct 24, 1993 | Abandoned |
Array
(
[id] => 3506150
[patent_doc_number] => 05505408
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-04-09
[patent_title] => 'Differential yoke-aerofin thrust vector control system'
[patent_app_type] => 1
[patent_app_number] => 8/139939
[patent_app_country] => US
[patent_app_date] => 1993-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 16
[patent_no_of_words] => 5735
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/505/05505408.pdf
[firstpage_image] =>[orig_patent_app_number] => 139939
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/139939 | Differential yoke-aerofin thrust vector control system | Oct 18, 1993 | Issued |
Array
(
[id] => 3435958
[patent_doc_number] => 05419516
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-05-30
[patent_title] => 'Device for coupling at least two spacecraft and use of the device for repairing tether damage'
[patent_app_type] => 1
[patent_app_number] => 8/135989
[patent_app_country] => US
[patent_app_date] => 1993-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2042
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/419/05419516.pdf
[firstpage_image] =>[orig_patent_app_number] => 135989
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/135989 | Device for coupling at least two spacecraft and use of the device for repairing tether damage | Oct 13, 1993 | Issued |
Array
(
[id] => 3611846
[patent_doc_number] => 05611503
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-03-18
[patent_title] => 'Optimal airplane passenger seating configurations and methods therefor'
[patent_app_type] => 1
[patent_app_number] => 8/135704
[patent_app_country] => US
[patent_app_date] => 1993-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 27
[patent_no_of_words] => 8966
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 16
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/611/05611503.pdf
[firstpage_image] =>[orig_patent_app_number] => 135704
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/135704 | Optimal airplane passenger seating configurations and methods therefor | Oct 12, 1993 | Issued |
| 08/130208 | POLYURETHANE DEICER | Sep 30, 1993 | Abandoned |
| 08/129458 | VTOL AIRCRAFT | Sep 28, 1993 | Abandoned |
Array
(
[id] => 3477171
[patent_doc_number] => 05474265
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-12-12
[patent_title] => 'Rigid kruger nose for the leading edge of an aircraft wing'
[patent_app_type] => 1
[patent_app_number] => 8/126708
[patent_app_country] => US
[patent_app_date] => 1993-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 5281
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/474/05474265.pdf
[firstpage_image] =>[orig_patent_app_number] => 126708
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/126708 | Rigid kruger nose for the leading edge of an aircraft wing | Sep 23, 1993 | Issued |
Array
(
[id] => 3096739
[patent_doc_number] => 05413292
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-05-09
[patent_title] => 'Vehicle cabin construction'
[patent_app_type] => 1
[patent_app_number] => 8/121407
[patent_app_country] => US
[patent_app_date] => 1993-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 25
[patent_no_of_words] => 5627
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 226
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/413/05413292.pdf
[firstpage_image] =>[orig_patent_app_number] => 121407
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/121407 | Vehicle cabin construction | Sep 14, 1993 | Issued |
Array
(
[id] => 3506134
[patent_doc_number] => 05505407
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-04-09
[patent_title] => 'Air-land vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/118966
[patent_app_country] => US
[patent_app_date] => 1993-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 25
[patent_no_of_words] => 7099
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 492
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/505/05505407.pdf
[firstpage_image] =>[orig_patent_app_number] => 118966
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/118966 | Air-land vehicle | Sep 8, 1993 | Issued |
Array
(
[id] => 3578890
[patent_doc_number] => 05566909
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-10-22
[patent_title] => 'System and method for deploying multiple probes'
[patent_app_type] => 1
[patent_app_number] => 8/118069
[patent_app_country] => US
[patent_app_date] => 1993-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 6432
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/566/05566909.pdf
[firstpage_image] =>[orig_patent_app_number] => 118069
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/118069 | System and method for deploying multiple probes | Sep 7, 1993 | Issued |
Array
(
[id] => 3688402
[patent_doc_number] => 05645250
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-07-08
[patent_title] => 'Multi-purpose aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/112877
[patent_app_country] => US
[patent_app_date] => 1993-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 61
[patent_figures_cnt] => 63
[patent_no_of_words] => 25871
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/645/05645250.pdf
[firstpage_image] =>[orig_patent_app_number] => 112877
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/112877 | Multi-purpose aircraft | Aug 25, 1993 | Issued |
Array
(
[id] => 3712048
[patent_doc_number] => 05681011
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-28
[patent_title] => 'Method for injecting payloads into orbit'
[patent_app_type] => 1
[patent_app_number] => 8/111095
[patent_app_country] => US
[patent_app_date] => 1993-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3326
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/681/05681011.pdf
[firstpage_image] =>[orig_patent_app_number] => 111095
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/111095 | Method for injecting payloads into orbit | Aug 23, 1993 | Issued |
Array
(
[id] => 3024868
[patent_doc_number] => 05372332
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-12-13
[patent_title] => 'Survivability enhancement air vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/109228
[patent_app_country] => US
[patent_app_date] => 1993-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 1391
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/372/05372332.pdf
[firstpage_image] =>[orig_patent_app_number] => 109228
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/109228 | Survivability enhancement air vehicle | Aug 18, 1993 | Issued |
| 08/106299 | INFRARED DEICERS FOR AIRCRAFT POSITIONED ON A TAXIWAY AND METHODS FOR USING SAME | Aug 12, 1993 | Abandoned |
Array
(
[id] => 3024065
[patent_doc_number] => 05375793
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-12-27
[patent_title] => 'Process for the control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviation'
[patent_app_type] => 1
[patent_app_number] => 8/105498
[patent_app_country] => US
[patent_app_date] => 1993-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2091
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/375/05375793.pdf
[firstpage_image] =>[orig_patent_app_number] => 105498
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/105498 | Process for the control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviation | Aug 10, 1993 | Issued |
Array
(
[id] => 3470895
[patent_doc_number] => 05456429
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-10-10
[patent_title] => 'Thrust maneuver system'
[patent_app_type] => 1
[patent_app_number] => 8/100268
[patent_app_country] => US
[patent_app_date] => 1993-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1987
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 17
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/456/05456429.pdf
[firstpage_image] =>[orig_patent_app_number] => 100268
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/100268 | Thrust maneuver system | Aug 1, 1993 | Issued |
Array
(
[id] => 3431602
[patent_doc_number] => 05465923
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-11-14
[patent_title] => 'Vertical take-off/landing of aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/095438
[patent_app_country] => US
[patent_app_date] => 1993-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 3320
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 193
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/465/05465923.pdf
[firstpage_image] =>[orig_patent_app_number] => 095438
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/095438 | Vertical take-off/landing of aircraft | Jul 22, 1993 | Issued |
| 08/091312 | FUSELAGE STRUCTURE FOR HELICOPTER | Jul 13, 1993 | Pending |
Array
(
[id] => 3515125
[patent_doc_number] => 05540405
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-30
[patent_title] => 'Method and apparatus for compensating for magnetic disturbance torques on a satellite'
[patent_app_type] => 1
[patent_app_number] => 8/089381
[patent_app_country] => US
[patent_app_date] => 1993-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3658
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/540/05540405.pdf
[firstpage_image] =>[orig_patent_app_number] => 089381
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/089381 | Method and apparatus for compensating for magnetic disturbance torques on a satellite | Jul 8, 1993 | Issued |
Array
(
[id] => 3408876
[patent_doc_number] => 05452865
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-09-26
[patent_title] => 'Aircraft frequency adaptive modal suppression system'
[patent_app_type] => 1
[patent_app_number] => 8/086447
[patent_app_country] => US
[patent_app_date] => 1993-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2385
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/452/05452865.pdf
[firstpage_image] =>[orig_patent_app_number] => 086447
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/086447 | Aircraft frequency adaptive modal suppression system | Jun 27, 1993 | Issued |