
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 |
|---|---|---|---|
Array
(
[id] => 3798665
[patent_doc_number] => 05769361
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-23
[patent_title] => 'Emergency exit accessible from the outside for an aircraft cockpit'
[patent_app_type] => 1
[patent_app_number] => 8/611548
[patent_app_country] => US
[patent_app_date] => 1996-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3585
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/769/05769361.pdf
[firstpage_image] =>[orig_patent_app_number] => 611548
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/611548 | Emergency exit accessible from the outside for an aircraft cockpit | Mar 10, 1996 | Issued |
Array
(
[id] => 3821985
[patent_doc_number] => 05845873
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-08
[patent_title] => 'Large aircraft critical surface covers'
[patent_app_type] => 1
[patent_app_number] => 8/610858
[patent_app_country] => US
[patent_app_date] => 1996-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1117
[patent_no_of_claims] => 12
[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/05/845/05845873.pdf
[firstpage_image] =>[orig_patent_app_number] => 610858
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/610858 | Large aircraft critical surface covers | Mar 4, 1996 | Issued |
| 08/608942 | INHIBITION OF HYDROCARBON VAPOR IN FUEL TANKS | Feb 28, 1996 | Abandoned |
Array
(
[id] => 3817153
[patent_doc_number] => 05738309
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-14
[patent_title] => 'Single axis correction for orbit inclination'
[patent_app_type] => 1
[patent_app_number] => 8/608238
[patent_app_country] => US
[patent_app_date] => 1996-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4336
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/738/05738309.pdf
[firstpage_image] =>[orig_patent_app_number] => 608238
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/608238 | Single axis correction for orbit inclination | Feb 27, 1996 | Issued |
Array
(
[id] => 3830979
[patent_doc_number] => 05765783
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-16
[patent_title] => 'Vertically launchable and recoverable winged aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/613754
[patent_app_country] => US
[patent_app_date] => 1996-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 7392
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 15
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/765/05765783.pdf
[firstpage_image] =>[orig_patent_app_number] => 613754
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/613754 | Vertically launchable and recoverable winged aircraft | Feb 25, 1996 | Issued |
Array
(
[id] => 3713311
[patent_doc_number] => 05671898
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-30
[patent_title] => 'Aircraft having fixed and pivotal wings'
[patent_app_type] => 1
[patent_app_number] => 8/602958
[patent_app_country] => US
[patent_app_date] => 1996-02-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 2014
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/671/05671898.pdf
[firstpage_image] =>[orig_patent_app_number] => 602958
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/602958 | Aircraft having fixed and pivotal wings | Feb 15, 1996 | Issued |
Array
(
[id] => 3650368
[patent_doc_number] => 05667166
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-16
[patent_title] => 'Aircraft frequency adaptive modal suppression system'
[patent_app_type] => 1
[patent_app_number] => 8/600779
[patent_app_country] => US
[patent_app_date] => 1996-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2390
[patent_no_of_claims] => 1
[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/05/667/05667166.pdf
[firstpage_image] =>[orig_patent_app_number] => 600779
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/600779 | Aircraft frequency adaptive modal suppression system | Feb 12, 1996 | Issued |
Array
(
[id] => 3881297
[patent_doc_number] => 05749543
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-05-12
[patent_title] => 'Method and apparatus for controlling cargo in an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/511247
[patent_app_country] => US
[patent_app_date] => 1996-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2989
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 297
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/749/05749543.pdf
[firstpage_image] =>[orig_patent_app_number] => 511247
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/511247 | Method and apparatus for controlling cargo in an aircraft | Feb 7, 1996 | Issued |
Array
(
[id] => 3732482
[patent_doc_number] => 05716030
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-10
[patent_title] => 'Aperture door and calibration source for spacecraft remote sensing devices'
[patent_app_type] => 1
[patent_app_number] => 8/596047
[patent_app_country] => US
[patent_app_date] => 1996-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 2718
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/716/05716030.pdf
[firstpage_image] =>[orig_patent_app_number] => 596047
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/596047 | Aperture door and calibration source for spacecraft remote sensing devices | Feb 5, 1996 | Issued |
Array
(
[id] => 3830994
[patent_doc_number] => 05765784
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-16
[patent_title] => 'System and method for deploying multiple probes'
[patent_app_type] => 1
[patent_app_number] => 8/596974
[patent_app_country] => US
[patent_app_date] => 1996-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 6431
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/765/05765784.pdf
[firstpage_image] =>[orig_patent_app_number] => 596974
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/596974 | System and method for deploying multiple probes | Feb 4, 1996 | Issued |
Array
(
[id] => 3857073
[patent_doc_number] => 05823480
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-20
[patent_title] => 'Wing with a wing grid as the end section'
[patent_app_type] => 1
[patent_app_number] => 8/595588
[patent_app_country] => US
[patent_app_date] => 1996-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 3061
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/823/05823480.pdf
[firstpage_image] =>[orig_patent_app_number] => 595588
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/595588 | Wing with a wing grid as the end section | Jan 31, 1996 | Issued |
Array
(
[id] => 3687318
[patent_doc_number] => 05595358
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-01-21
[patent_title] => 'Multipurpose airborne vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/593019
[patent_app_country] => US
[patent_app_date] => 1996-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 4703
[patent_no_of_claims] => 23
[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/05/595/05595358.pdf
[firstpage_image] =>[orig_patent_app_number] => 593019
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/593019 | Multipurpose airborne vehicle | Jan 28, 1996 | Issued |
Array
(
[id] => 3810294
[patent_doc_number] => 05782436
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-21
[patent_title] => 'Torque tube breakout mechanism'
[patent_app_type] => 1
[patent_app_number] => 8/588749
[patent_app_country] => US
[patent_app_date] => 1996-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2894
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/782/05782436.pdf
[firstpage_image] =>[orig_patent_app_number] => 588749
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/588749 | Torque tube breakout mechanism | Jan 18, 1996 | Issued |
Array
(
[id] => 3772398
[patent_doc_number] => 05839696
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-24
[patent_title] => 'Modular payload arrangement'
[patent_app_type] => 1
[patent_app_number] => 8/577437
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1501
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/839/05839696.pdf
[firstpage_image] =>[orig_patent_app_number] => 577437
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577437 | Modular payload arrangement | Dec 21, 1995 | Issued |
Array
(
[id] => 3871669
[patent_doc_number] => 05833175
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-10
[patent_title] => 'Spacecraft with large east-west dimensions'
[patent_app_type] => 1
[patent_app_number] => 8/577447
[patent_app_country] => US
[patent_app_date] => 1995-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 14
[patent_no_of_words] => 2990
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 83
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/833/05833175.pdf
[firstpage_image] =>[orig_patent_app_number] => 577447
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/577447 | Spacecraft with large east-west dimensions | Dec 21, 1995 | Issued |
| 08/574837 | MAIN DECK CARGO DOOR ELECTRIC LOCK SYSTEM | Dec 18, 1995 | Abandoned |
Array
(
[id] => 3771862
[patent_doc_number] => 05735487
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-07
[patent_title] => 'Main deck cargo door control panel indication'
[patent_app_type] => 1
[patent_app_number] => 8/574836
[patent_app_country] => US
[patent_app_date] => 1995-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 1607
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 70
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/735/05735487.pdf
[firstpage_image] =>[orig_patent_app_number] => 574836
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/574836 | Main deck cargo door control panel indication | Dec 18, 1995 | Issued |
Array
(
[id] => 3681156
[patent_doc_number] => 05678786
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-21
[patent_title] => 'Reconfigurable helicopter flight control system'
[patent_app_type] => 1
[patent_app_number] => 8/567898
[patent_app_country] => US
[patent_app_date] => 1995-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 7761
[patent_no_of_claims] => 34
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 228
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/678/05678786.pdf
[firstpage_image] =>[orig_patent_app_number] => 567898
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/567898 | Reconfigurable helicopter flight control system | Dec 5, 1995 | Issued |
| 08/568144 | FLIGHT CONTROL SYSTEM FOR JET POWERED TRI-MODE AIRCRAFT | Dec 5, 1995 | Abandoned |
Array
(
[id] => 3750713
[patent_doc_number] => 05772154
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-06-30
[patent_title] => 'Leading edge heat shield for wings of spacecraft'
[patent_app_type] => 1
[patent_app_number] => 8/563418
[patent_app_country] => US
[patent_app_date] => 1995-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2105
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/772/05772154.pdf
[firstpage_image] =>[orig_patent_app_number] => 563418
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/563418 | Leading edge heat shield for wings of spacecraft | Nov 27, 1995 | Issued |