
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] => 2907743
[patent_doc_number] => 05199668
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-06
[patent_title] => 'Launcher for radio controlled flights of a model airplane, releasing the model airplane for flight upon depressing a foot pedal thereof'
[patent_app_type] => 1
[patent_app_number] => 7/824576
[patent_app_country] => US
[patent_app_date] => 1992-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2872
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 437
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/199/05199668.pdf
[firstpage_image] =>[orig_patent_app_number] => 824576
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/824576 | Launcher for radio controlled flights of a model airplane, releasing the model airplane for flight upon depressing a foot pedal thereof | Jan 22, 1992 | Issued |
Array
(
[id] => 2995749
[patent_doc_number] => 05275357
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-04
[patent_title] => 'Aircraft engine mount'
[patent_app_type] => 1
[patent_app_number] => 7/821376
[patent_app_country] => US
[patent_app_date] => 1992-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 6073
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 222
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/275/05275357.pdf
[firstpage_image] =>[orig_patent_app_number] => 821376
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/821376 | Aircraft engine mount | Jan 15, 1992 | Issued |
Array
(
[id] => 2929082
[patent_doc_number] => 05253826
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-19
[patent_title] => 'Lightweight sealed parachute and harness assembly'
[patent_app_type] => 1
[patent_app_number] => 7/818799
[patent_app_country] => US
[patent_app_date] => 1992-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 14
[patent_no_of_words] => 3914
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/253/05253826.pdf
[firstpage_image] =>[orig_patent_app_number] => 818799
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/818799 | Lightweight sealed parachute and harness assembly | Jan 8, 1992 | Issued |
| 07/810129 | ADJUSTABLE SPRINKLER HEAD POSITIONING ASSEMBLY | Dec 18, 1991 | Abandoned |
Array
(
[id] => 3073910
[patent_doc_number] => 05279483
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-18
[patent_title] => 'Attitude control system for a three-axis stabilized satellite especially a remote sensing satellite'
[patent_app_type] => 1
[patent_app_number] => 7/806599
[patent_app_country] => US
[patent_app_date] => 1991-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 19
[patent_no_of_words] => 3307
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 272
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/279/05279483.pdf
[firstpage_image] =>[orig_patent_app_number] => 806599
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/806599 | Attitude control system for a three-axis stabilized satellite especially a remote sensing satellite | Dec 11, 1991 | Issued |
Array
(
[id] => 3413196
[patent_doc_number] => 05402852
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-04-04
[patent_title] => 'Compositions of matter for stopping fires, explosions and oxidations of materials and build up of electrostatic charges and method and apparatus for making same'
[patent_app_type] => 1
[patent_app_number] => 7/806901
[patent_app_country] => US
[patent_app_date] => 1991-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 39
[patent_no_of_words] => 11350
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/402/05402852.pdf
[firstpage_image] =>[orig_patent_app_number] => 806901
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/806901 | Compositions of matter for stopping fires, explosions and oxidations of materials and build up of electrostatic charges and method and apparatus for making same | Dec 11, 1991 | Issued |
Array
(
[id] => 2960148
[patent_doc_number] => 05224668
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-07-06
[patent_title] => 'Torque linkage damper'
[patent_app_type] => 1
[patent_app_number] => 7/806007
[patent_app_country] => US
[patent_app_date] => 1991-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1727
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 230
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/224/05224668.pdf
[firstpage_image] =>[orig_patent_app_number] => 806007
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/806007 | Torque linkage damper | Dec 8, 1991 | Issued |
Array
(
[id] => 2877871
[patent_doc_number] => 05209435
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-05-11
[patent_title] => 'Passsenger car with emergency exit'
[patent_app_type] => 1
[patent_app_number] => 7/803023
[patent_app_country] => US
[patent_app_date] => 1991-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 3717
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/209/05209435.pdf
[firstpage_image] =>[orig_patent_app_number] => 803023
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/803023 | Passsenger car with emergency exit | Dec 5, 1991 | Issued |
Array
(
[id] => 2934984
[patent_doc_number] => 05261630
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-16
[patent_title] => 'Ejection seat control using aircraft radio altimeter'
[patent_app_type] => 1
[patent_app_number] => 7/802376
[patent_app_country] => US
[patent_app_date] => 1991-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1232
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/261/05261630.pdf
[firstpage_image] =>[orig_patent_app_number] => 802376
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/802376 | Ejection seat control using aircraft radio altimeter | Dec 3, 1991 | Issued |
| 07/800776 | METHOD AND APPARATUS FOR COMPENSATING FOR MAGNETIC DISTURBANCE TORQUES ON A SATELLITE | Nov 26, 1991 | Abandoned |
Array
(
[id] => 2903915
[patent_doc_number] => 05205518
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-27
[patent_title] => 'Gyroless yaw control system for a three axis stabilized, zero-momentum spacecraft'
[patent_app_type] => 1
[patent_app_number] => 7/799457
[patent_app_country] => US
[patent_app_date] => 1991-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3910
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 345
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/205/05205518.pdf
[firstpage_image] =>[orig_patent_app_number] => 799457
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/799457 | Gyroless yaw control system for a three axis stabilized, zero-momentum spacecraft | Nov 24, 1991 | Issued |
Array
(
[id] => 2924329
[patent_doc_number] => 05190244
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-02
[patent_title] => 'Antiresonant suspension device for a helicopter'
[patent_app_type] => 1
[patent_app_number] => 7/794066
[patent_app_country] => US
[patent_app_date] => 1991-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4190
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 336
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/190/05190244.pdf
[firstpage_image] =>[orig_patent_app_number] => 794066
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/794066 | Antiresonant suspension device for a helicopter | Nov 18, 1991 | Issued |
Array
(
[id] => 2771702
[patent_doc_number] => 05129596
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-14
[patent_title] => 'Landing gear of a model airplane'
[patent_app_type] => 1
[patent_app_number] => 7/793281
[patent_app_country] => US
[patent_app_date] => 1991-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1120
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 214
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/129/05129596.pdf
[firstpage_image] =>[orig_patent_app_number] => 793281
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/793281 | Landing gear of a model airplane | Nov 11, 1991 | Issued |
Array
(
[id] => 2972192
[patent_doc_number] => 05265828
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-30
[patent_title] => 'Child safety seat adaptable to aircraft seat attach points'
[patent_app_type] => 1
[patent_app_number] => 7/790186
[patent_app_country] => US
[patent_app_date] => 1991-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 4165
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/265/05265828.pdf
[firstpage_image] =>[orig_patent_app_number] => 790186
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/790186 | Child safety seat adaptable to aircraft seat attach points | Nov 7, 1991 | Issued |
Array
(
[id] => 2788817
[patent_doc_number] => 05114073
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-19
[patent_title] => 'Wheel and rail assembly'
[patent_app_type] => 1
[patent_app_number] => 7/789440
[patent_app_country] => US
[patent_app_date] => 1991-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 3621
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/114/05114073.pdf
[firstpage_image] =>[orig_patent_app_number] => 789440
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/789440 | Wheel and rail assembly | Nov 5, 1991 | Issued |
| 07/779867 | PROPELLANT TANK CONFORMAL LIFTING BODY SPACECRAFT | Oct 20, 1991 | Abandoned |
Array
(
[id] => 2881208
[patent_doc_number] => 05244170
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-09-14
[patent_title] => 'Passive nonlinear interface strut (PNIS)'
[patent_app_type] => 1
[patent_app_number] => 7/776159
[patent_app_country] => US
[patent_app_date] => 1991-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 8
[patent_no_of_words] => 2179
[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/05/244/05244170.pdf
[firstpage_image] =>[orig_patent_app_number] => 776159
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/776159 | Passive nonlinear interface strut (PNIS) | Oct 14, 1991 | Issued |
Array
(
[id] => 3043428
[patent_doc_number] => 05337982
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-16
[patent_title] => 'Apparatus and method for controlling the vertical profile of an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/774776
[patent_app_country] => US
[patent_app_date] => 1991-10-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3578
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 279
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/337/05337982.pdf
[firstpage_image] =>[orig_patent_app_number] => 774776
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/774776 | Apparatus and method for controlling the vertical profile of an aircraft | Oct 9, 1991 | Issued |
Array
(
[id] => 2903599
[patent_doc_number] => 05205502
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-27
[patent_title] => 'Aviation electronics instrument latching swing handle'
[patent_app_type] => 1
[patent_app_number] => 7/766469
[patent_app_country] => US
[patent_app_date] => 1991-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1086
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/205/05205502.pdf
[firstpage_image] =>[orig_patent_app_number] => 766469
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/766469 | Aviation electronics instrument latching swing handle | Sep 25, 1991 | Issued |
Array
(
[id] => 2825330
[patent_doc_number] => 05170963
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-15
[patent_title] => 'VTOL aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/764806
[patent_app_country] => US
[patent_app_date] => 1991-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 18
[patent_no_of_words] => 6895
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/170/05170963.pdf
[firstpage_image] =>[orig_patent_app_number] => 764806
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/764806 | VTOL aircraft | Sep 23, 1991 | Issued |