
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] => 3024962
[patent_doc_number] => 05372337
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-12-13
[patent_title] => 'Unmanned aerial aircraft having a single engine with dual jet exhausts'
[patent_app_type] => 1
[patent_app_number] => 7/877210
[patent_app_country] => US
[patent_app_date] => 1992-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 1888
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/372/05372337.pdf
[firstpage_image] =>[orig_patent_app_number] => 877210
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/877210 | Unmanned aerial aircraft having a single engine with dual jet exhausts | Apr 30, 1992 | Issued |
Array
(
[id] => 2947600
[patent_doc_number] => 05273240
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-12-28
[patent_title] => 'Impact absorption system, particularly for aircraft seats'
[patent_app_type] => 1
[patent_app_number] => 7/876366
[patent_app_country] => US
[patent_app_date] => 1992-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 2986
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/273/05273240.pdf
[firstpage_image] =>[orig_patent_app_number] => 876366
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/876366 | Impact absorption system, particularly for aircraft seats | Apr 29, 1992 | Issued |
Array
(
[id] => 2961144
[patent_doc_number] => 05255875
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-26
[patent_title] => 'Protective hardside covers for vehicle surfaces'
[patent_app_type] => 1
[patent_app_number] => 7/876536
[patent_app_country] => US
[patent_app_date] => 1992-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 5234
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/255/05255875.pdf
[firstpage_image] =>[orig_patent_app_number] => 876536
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/876536 | Protective hardside covers for vehicle surfaces | Apr 29, 1992 | Issued |
| 07/874706 | LIFTING BODY WITH REDUCED-STRENGTH TRAILING VORTICES | Apr 27, 1992 | Abandoned |
Array
(
[id] => 3038351
[patent_doc_number] => 05282589
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-02-01
[patent_title] => 'Terrain cueing'
[patent_app_type] => 1
[patent_app_number] => 7/872376
[patent_app_country] => US
[patent_app_date] => 1992-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2662
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/282/05282589.pdf
[firstpage_image] =>[orig_patent_app_number] => 872376
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/872376 | Terrain cueing | Apr 22, 1992 | Issued |
Array
(
[id] => 3450843
[patent_doc_number] => 05381985
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-01-17
[patent_title] => 'Wingtip mounted, counter-rotating proprotor for tiltwing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/872336
[patent_app_country] => US
[patent_app_date] => 1992-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2566
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/381/05381985.pdf
[firstpage_image] =>[orig_patent_app_number] => 872336
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/872336 | Wingtip mounted, counter-rotating proprotor for tiltwing aircraft | Apr 22, 1992 | Issued |
Array
(
[id] => 2938399
[patent_doc_number] => 05242131
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-09-07
[patent_title] => 'Steerable landing gear'
[patent_app_type] => 1
[patent_app_number] => 7/865066
[patent_app_country] => US
[patent_app_date] => 1992-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3354
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/242/05242131.pdf
[firstpage_image] =>[orig_patent_app_number] => 865066
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/865066 | Steerable landing gear | Apr 7, 1992 | Issued |
Array
(
[id] => 3065037
[patent_doc_number] => 05322248
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-06-21
[patent_title] => 'Methods and arrangements tailoring aerodynamic forces afforded by a payload to reduce flight loads and to assist flight control for the coupled system'
[patent_app_type] => 1
[patent_app_number] => 7/857876
[patent_app_country] => US
[patent_app_date] => 1992-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2039
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/322/05322248.pdf
[firstpage_image] =>[orig_patent_app_number] => 857876
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/857876 | Methods and arrangements tailoring aerodynamic forces afforded by a payload to reduce flight loads and to assist flight control for the coupled system | Mar 25, 1992 | Issued |
Array
(
[id] => 2961252
[patent_doc_number] => 05255881
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-10-26
[patent_title] => 'Lift augmentation for highly swept wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/857397
[patent_app_country] => US
[patent_app_date] => 1992-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2835
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 296
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/255/05255881.pdf
[firstpage_image] =>[orig_patent_app_number] => 857397
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/857397 | Lift augmentation for highly swept wing aircraft | Mar 24, 1992 | Issued |
Array
(
[id] => 3064817
[patent_doc_number] => 05320307
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-06-14
[patent_title] => 'Aircraft engine thrust mount'
[patent_app_type] => 1
[patent_app_number] => 7/857136
[patent_app_country] => US
[patent_app_date] => 1992-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 6656
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 301
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/320/05320307.pdf
[firstpage_image] =>[orig_patent_app_number] => 857136
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/857136 | Aircraft engine thrust mount | Mar 24, 1992 | Issued |
| 07/857317 | AUTOGYRO AIRCRAFT | Mar 24, 1992 | Abandoned |
Array
(
[id] => 2922843
[patent_doc_number] => 05259575
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-09
[patent_title] => 'Airplane stretcher system'
[patent_app_type] => 1
[patent_app_number] => 7/855607
[patent_app_country] => US
[patent_app_date] => 1992-03-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 4548
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/259/05259575.pdf
[firstpage_image] =>[orig_patent_app_number] => 855607
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/855607 | Airplane stretcher system | Mar 19, 1992 | Issued |
Array
(
[id] => 3443307
[patent_doc_number] => 05377936
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-01-03
[patent_title] => 'Net kinetic energy differential guidance and propulsion system for satellites and space vehicles'
[patent_app_type] => 1
[patent_app_number] => 7/854346
[patent_app_country] => US
[patent_app_date] => 1992-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 17
[patent_no_of_words] => 8199
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/377/05377936.pdf
[firstpage_image] =>[orig_patent_app_number] => 854346
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/854346 | Net kinetic energy differential guidance and propulsion system for satellites and space vehicles | Mar 18, 1992 | Issued |
| 07/853894 | MAGNETIC POWER SYSTEM FOR LOW-FRICTION TRANSPORTATION OF LOADS | Mar 18, 1992 | Abandoned |
Array
(
[id] => 3085025
[patent_doc_number] => 05314142
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-24
[patent_title] => 'Wing root aerofoil for forward swept wings'
[patent_app_type] => 1
[patent_app_number] => 7/854016
[patent_app_country] => US
[patent_app_date] => 1992-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 20
[patent_no_of_words] => 2253
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/314/05314142.pdf
[firstpage_image] =>[orig_patent_app_number] => 854016
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/854016 | Wing root aerofoil for forward swept wings | Mar 17, 1992 | Issued |
Array
(
[id] => 2922824
[patent_doc_number] => 05259574
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-09
[patent_title] => 'Safety device for helicopters and similar equipment with rotors'
[patent_app_type] => 1
[patent_app_number] => 7/838426
[patent_app_country] => US
[patent_app_date] => 1992-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 1192
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/259/05259574.pdf
[firstpage_image] =>[orig_patent_app_number] => 838426
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/838426 | Safety device for helicopters and similar equipment with rotors | Mar 5, 1992 | Issued |
Array
(
[id] => 2942811
[patent_doc_number] => 05230487
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-07-27
[patent_title] => 'Apparatus for driving and guiding a flap secured to an aircraft wing'
[patent_app_type] => 1
[patent_app_number] => 7/847917
[patent_app_country] => US
[patent_app_date] => 1992-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 2558
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/230/05230487.pdf
[firstpage_image] =>[orig_patent_app_number] => 847917
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/847917 | Apparatus for driving and guiding a flap secured to an aircraft wing | Mar 5, 1992 | Issued |
Array
(
[id] => 3056746
[patent_doc_number] => 05364046
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-11-15
[patent_title] => 'Automatic compliant capture and docking mechanism for spacecraft'
[patent_app_type] => 1
[patent_app_number] => 7/839996
[patent_app_country] => US
[patent_app_date] => 1992-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 4015
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/364/05364046.pdf
[firstpage_image] =>[orig_patent_app_number] => 839996
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/839996 | Automatic compliant capture and docking mechanism for spacecraft | Feb 23, 1992 | Issued |
Array
(
[id] => 3646008
[patent_doc_number] => 05590853
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-01-07
[patent_title] => 'Aircraft control system'
[patent_app_type] => 1
[patent_app_number] => 7/829256
[patent_app_country] => US
[patent_app_date] => 1992-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2665
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 82
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/590/05590853.pdf
[firstpage_image] =>[orig_patent_app_number] => 829256
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/829256 | Aircraft control system | Feb 2, 1992 | Issued |
Array
(
[id] => 2942776
[patent_doc_number] => 05230485
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-07-27
[patent_title] => 'Connector device for securing structural components to each other'
[patent_app_type] => 1
[patent_app_number] => 7/825616
[patent_app_country] => US
[patent_app_date] => 1992-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2075
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/230/05230485.pdf
[firstpage_image] =>[orig_patent_app_number] => 825616
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/825616 | Connector device for securing structural components to each other | Jan 23, 1992 | Issued |