
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] => 2963690
[patent_doc_number] => 05251850
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-12
[patent_title] => 'Device for adjustment of the height of an airship'
[patent_app_type] => 1
[patent_app_number] => 7/741410
[patent_app_country] => US
[patent_app_date] => 1991-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 5
[patent_no_of_words] => 896
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 138
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/251/05251850.pdf
[firstpage_image] =>[orig_patent_app_number] => 741410
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/741410 | Device for adjustment of the height of an airship | Sep 16, 1991 | Issued |
Array
(
[id] => 2880639
[patent_doc_number] => 05240206
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-31
[patent_title] => 'Airship'
[patent_app_type] => 1
[patent_app_number] => 7/756750
[patent_app_country] => US
[patent_app_date] => 1991-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3317
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/240/05240206.pdf
[firstpage_image] =>[orig_patent_app_number] => 756750
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/756750 | Airship | Sep 8, 1991 | Issued |
Array
(
[id] => 2782979
[patent_doc_number] => 05143321
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-01
[patent_title] => 'Folding protective cover for turbo-engines'
[patent_app_type] => 1
[patent_app_number] => 7/756349
[patent_app_country] => US
[patent_app_date] => 1991-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1932
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/143/05143321.pdf
[firstpage_image] =>[orig_patent_app_number] => 756349
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/756349 | Folding protective cover for turbo-engines | Sep 8, 1991 | Issued |
Array
(
[id] => 3443317
[patent_doc_number] => 05377937
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-01-03
[patent_title] => 'Aircraft flare control system utilizing an envelope limiter'
[patent_app_type] => 1
[patent_app_number] => 7/754083
[patent_app_country] => US
[patent_app_date] => 1991-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6281
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 21
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/377/05377937.pdf
[firstpage_image] =>[orig_patent_app_number] => 754083
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/754083 | Aircraft flare control system utilizing an envelope limiter | Sep 2, 1991 | Issued |
Array
(
[id] => 2963758
[patent_doc_number] => 05251853
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-12
[patent_title] => 'Canopy for paraglider and/or parachute'
[patent_app_type] => 1
[patent_app_number] => 7/753550
[patent_app_country] => US
[patent_app_date] => 1991-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2427
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/251/05251853.pdf
[firstpage_image] =>[orig_patent_app_number] => 753550
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/753550 | Canopy for paraglider and/or parachute | Sep 2, 1991 | Issued |
Array
(
[id] => 2789673
[patent_doc_number] => 05145128
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-08
[patent_title] => 'Storage device and method for storing video monitoring equipment for airliner'
[patent_app_type] => 1
[patent_app_number] => 7/751886
[patent_app_country] => US
[patent_app_date] => 1991-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 4629
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/145/05145128.pdf
[firstpage_image] =>[orig_patent_app_number] => 751886
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751886 | Storage device and method for storing video monitoring equipment for airliner | Aug 28, 1991 | Issued |
Array
(
[id] => 2919105
[patent_doc_number] => 05195700
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-23
[patent_title] => 'Low speed model following velocity command system for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751437
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4422
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 397
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/195/05195700.pdf
[firstpage_image] =>[orig_patent_app_number] => 751437
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751437 | Low speed model following velocity command system for rotary wing aircraft | Aug 27, 1991 | Issued |
Array
(
[id] => 2769537
[patent_doc_number] => 05141177
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-08-25
[patent_title] => 'Model following control system'
[patent_app_type] => 1
[patent_app_number] => 7/751434
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3071
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 270
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/141/05141177.pdf
[firstpage_image] =>[orig_patent_app_number] => 751434
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751434 | Model following control system | Aug 27, 1991 | Issued |
Array
(
[id] => 2809644
[patent_doc_number] => 05169090
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-08
[patent_title] => 'Attitude synchronization for model following control systems'
[patent_app_type] => 1
[patent_app_number] => 7/751429
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4401
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 274
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/169/05169090.pdf
[firstpage_image] =>[orig_patent_app_number] => 751429
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751429 | Attitude synchronization for model following control systems | Aug 27, 1991 | Issued |
Array
(
[id] => 2874823
[patent_doc_number] => 05238203
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-24
[patent_title] => 'High speed turn coordination for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751431
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 17
[patent_no_of_words] => 7546
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 291
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/238/05238203.pdf
[firstpage_image] =>[orig_patent_app_number] => 751431
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751431 | High speed turn coordination for rotary wing aircraft | Aug 27, 1991 | Issued |
Array
(
[id] => 2901874
[patent_doc_number] => 05178307
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-01-12
[patent_title] => 'High speed yaw control system for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751432
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 17
[patent_no_of_words] => 7280
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 253
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/178/05178307.pdf
[firstpage_image] =>[orig_patent_app_number] => 751432
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751432 | High speed yaw control system for rotary wing aircraft | Aug 27, 1991 | Issued |
Array
(
[id] => 2871500
[patent_doc_number] => 05213283
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-05-25
[patent_title] => 'Low speed turn coordination for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751436
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 17
[patent_no_of_words] => 7666
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 305
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/213/05213283.pdf
[firstpage_image] =>[orig_patent_app_number] => 751436
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751436 | Low speed turn coordination for rotary wing aircraft | Aug 27, 1991 | Issued |
Array
(
[id] => 2871470
[patent_doc_number] => 05213282
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-05-25
[patent_title] => 'Maneuver feel system for a rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751456
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5234
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 265
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/213/05213282.pdf
[firstpage_image] =>[orig_patent_app_number] => 751456
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751456 | Maneuver feel system for a rotary wing aircraft | Aug 27, 1991 | Issued |
Array
(
[id] => 2926565
[patent_doc_number] => 05222691
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-06-29
[patent_title] => 'Automatic turn coordination trim control for rotary wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/751433
[patent_app_country] => US
[patent_app_date] => 1991-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 17
[patent_no_of_words] => 7403
[patent_no_of_claims] => 6
[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/05/222/05222691.pdf
[firstpage_image] =>[orig_patent_app_number] => 751433
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/751433 | Automatic turn coordination trim control for rotary wing aircraft | Aug 27, 1991 | Issued |
| 07/750355 | HELICOPTER ENGINE CONTROL HAVING YAW INPUT ANTICIPATION | Aug 26, 1991 | Abandoned |
Array
(
[id] => 3085111
[patent_doc_number] => 05314147
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-24
[patent_title] => 'Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering'
[patent_app_type] => 1
[patent_app_number] => 7/750846
[patent_app_country] => US
[patent_app_date] => 1991-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 5067
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 402
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/314/05314147.pdf
[firstpage_image] =>[orig_patent_app_number] => 750846
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/750846 | Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering | Aug 26, 1991 | Issued |
Array
(
[id] => 2908050
[patent_doc_number] => 05192037
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-09
[patent_title] => 'Double-pivoting deployment system for aerosurfaces'
[patent_app_type] => 1
[patent_app_number] => 7/749316
[patent_app_country] => US
[patent_app_date] => 1991-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2616
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 205
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/192/05192037.pdf
[firstpage_image] =>[orig_patent_app_number] => 749316
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/749316 | Double-pivoting deployment system for aerosurfaces | Aug 22, 1991 | Issued |
Array
(
[id] => 2809681
[patent_doc_number] => 05169092
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-08
[patent_title] => 'Paraglider canopy'
[patent_app_type] => 1
[patent_app_number] => 7/744327
[patent_app_country] => US
[patent_app_date] => 1991-08-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 11
[patent_no_of_words] => 1775
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 244
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/169/05169092.pdf
[firstpage_image] =>[orig_patent_app_number] => 744327
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/744327 | Paraglider canopy | Aug 12, 1991 | Issued |
Array
(
[id] => 2924366
[patent_doc_number] => 05190246
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-02
[patent_title] => 'Shuttle orbiter with telescoping main propulsion unit and payload'
[patent_app_type] => 1
[patent_app_number] => 7/743469
[patent_app_country] => US
[patent_app_date] => 1991-08-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 1519
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/190/05190246.pdf
[firstpage_image] =>[orig_patent_app_number] => 743469
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/743469 | Shuttle orbiter with telescoping main propulsion unit and payload | Aug 6, 1991 | Issued |
Array
(
[id] => 2913577
[patent_doc_number] => 05186418
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'Self guided recoverable airborne instrument module'
[patent_app_type] => 1
[patent_app_number] => 7/738350
[patent_app_country] => US
[patent_app_date] => 1991-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4173
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/186/05186418.pdf
[firstpage_image] =>[orig_patent_app_number] => 738350
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/738350 | Self guided recoverable airborne instrument module | Jul 30, 1991 | Issued |