
Carla Mattix
Examiner (ID: 2351)
| Most Active Art Unit | 3106 |
| Art Unit(s) | 3106, 3105 |
| Total Applications | 310 |
| Issued Applications | 284 |
| Pending Applications | 4 |
| Abandoned Applications | 22 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2924412
[patent_doc_number] => 05190248
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-02
[patent_title] => 'Protection of aircraft structures'
[patent_app_type] => 1
[patent_app_number] => 7/610237
[patent_app_country] => US
[patent_app_date] => 1990-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3093
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/190/05190248.pdf
[firstpage_image] =>[orig_patent_app_number] => 610237
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/610237 | Protection of aircraft structures | Nov 6, 1990 | Issued |
Array
(
[id] => 2785441
[patent_doc_number] => 05139242
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-08-18
[patent_title] => 'Linear suspension device'
[patent_app_type] => 1
[patent_app_number] => 7/609811
[patent_app_country] => US
[patent_app_date] => 1990-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 1189
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/139/05139242.pdf
[firstpage_image] =>[orig_patent_app_number] => 609811
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/609811 | Linear suspension device | Nov 5, 1990 | Issued |
Array
(
[id] => 2737874
[patent_doc_number] => 05071092
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-10
[patent_title] => 'Fairing arrangements for aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/609613
[patent_app_country] => US
[patent_app_date] => 1990-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 1016
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/071/05071092.pdf
[firstpage_image] =>[orig_patent_app_number] => 609613
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/609613 | Fairing arrangements for aircraft | Nov 5, 1990 | Issued |
Array
(
[id] => 2862767
[patent_doc_number] => 05117947
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-06-02
[patent_title] => 'Disk brake friction pad wear sensor'
[patent_app_type] => 1
[patent_app_number] => 7/608484
[patent_app_country] => US
[patent_app_date] => 1990-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 3808
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/117/05117947.pdf
[firstpage_image] =>[orig_patent_app_number] => 608484
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/608484 | Disk brake friction pad wear sensor | Oct 31, 1990 | Issued |
Array
(
[id] => 2849289
[patent_doc_number] => 05082211
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-21
[patent_title] => 'Method and apparatus for mitigating space debris'
[patent_app_type] => 1
[patent_app_number] => 7/606897
[patent_app_country] => US
[patent_app_date] => 1990-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 7173
[patent_no_of_claims] => 49
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/082/05082211.pdf
[firstpage_image] =>[orig_patent_app_number] => 606897
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/606897 | Method and apparatus for mitigating space debris | Oct 30, 1990 | Issued |
Array
(
[id] => 2844406
[patent_doc_number] => 05083728
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-28
[patent_title] => 'Rocket engine nozzle throat plug engine recovery system'
[patent_app_type] => 1
[patent_app_number] => 7/608175
[patent_app_country] => US
[patent_app_date] => 1990-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2426
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/083/05083728.pdf
[firstpage_image] =>[orig_patent_app_number] => 608175
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/608175 | Rocket engine nozzle throat plug engine recovery system | Oct 30, 1990 | Issued |
Array
(
[id] => 2834105
[patent_doc_number] => 05104069
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-14
[patent_title] => 'Apparatus and method for ejecting matter from an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/604471
[patent_app_country] => US
[patent_app_date] => 1990-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 5
[patent_no_of_words] => 1264
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 200
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/104/05104069.pdf
[firstpage_image] =>[orig_patent_app_number] => 604471
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/604471 | Apparatus and method for ejecting matter from an aircraft | Oct 28, 1990 | Issued |
Array
(
[id] => 2911155
[patent_doc_number] => 05186289
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'Retractable lifeline safety device'
[patent_app_type] => 1
[patent_app_number] => 7/604758
[patent_app_country] => US
[patent_app_date] => 1990-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 12
[patent_no_of_words] => 3706
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/186/05186289.pdf
[firstpage_image] =>[orig_patent_app_number] => 604758
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/604758 | Retractable lifeline safety device | Oct 25, 1990 | Issued |
Array
(
[id] => 2735939
[patent_doc_number] => 05020739
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-06-04
[patent_title] => 'Selectable towline spin chute system'
[patent_app_type] => 1
[patent_app_number] => 7/603335
[patent_app_country] => US
[patent_app_date] => 1990-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 2321
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/020/05020739.pdf
[firstpage_image] =>[orig_patent_app_number] => 603335
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/603335 | Selectable towline spin chute system | Oct 24, 1990 | Issued |
Array
(
[id] => 2812259
[patent_doc_number] => 05094411
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-10
[patent_title] => 'Control configured vortex flaps'
[patent_app_type] => 1
[patent_app_number] => 7/600595
[patent_app_country] => US
[patent_app_date] => 1990-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 3265
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/094/05094411.pdf
[firstpage_image] =>[orig_patent_app_number] => 600595
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/600595 | Control configured vortex flaps | Oct 18, 1990 | Issued |
| 07/597725 | FUSELAGE WALL INNER LINING PLATE | Oct 16, 1990 | Abandoned |
Array
(
[id] => 2757551
[patent_doc_number] => 05074494
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-12-24
[patent_title] => 'Elastomeric swashplate configuration for helicopters'
[patent_app_type] => 1
[patent_app_number] => 7/598470
[patent_app_country] => US
[patent_app_date] => 1990-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 1565
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/074/05074494.pdf
[firstpage_image] =>[orig_patent_app_number] => 598470
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/598470 | Elastomeric swashplate configuration for helicopters | Oct 10, 1990 | Issued |
Array
(
[id] => 2844354
[patent_doc_number] => 05083725
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-28
[patent_title] => 'Elastomeric swashplate configuration for helicopters'
[patent_app_type] => 1
[patent_app_number] => 7/598469
[patent_app_country] => US
[patent_app_date] => 1990-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1386
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 190
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/083/05083725.pdf
[firstpage_image] =>[orig_patent_app_number] => 598469
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/598469 | Elastomeric swashplate configuration for helicopters | Oct 10, 1990 | Issued |
| 07/597923 | DOOR FOR AIRCRAFT NACELLE | Oct 9, 1990 | Abandoned |
| 07/593690 | EQUIPMENT CARRYING REMOTE CONTROLLED AIRCRAFT | Oct 4, 1990 | Abandoned |
Array
(
[id] => 2770088
[patent_doc_number] => 05086994
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-02-11
[patent_title] => 'Oscillating and continuous motion gear drive assembly'
[patent_app_type] => 1
[patent_app_number] => 7/592255
[patent_app_country] => US
[patent_app_date] => 1990-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3033
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 315
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/086/05086994.pdf
[firstpage_image] =>[orig_patent_app_number] => 592255
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/592255 | Oscillating and continuous motion gear drive assembly | Oct 2, 1990 | Issued |
Array
(
[id] => 2789402
[patent_doc_number] => 05114104
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-19
[patent_title] => 'Articulated control surface'
[patent_app_type] => 1
[patent_app_number] => 7/591532
[patent_app_country] => US
[patent_app_date] => 1990-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2109
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/114/05114104.pdf
[firstpage_image] =>[orig_patent_app_number] => 591532
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/591532 | Articulated control surface | Sep 30, 1990 | Issued |
| 07/588774 | AIRSHIP AND METHOD FOR CONTROLLING ITS FLIGHT | Sep 26, 1990 | Abandoned |
Array
(
[id] => 2677581
[patent_doc_number] => 05018683
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-05-28
[patent_title] => 'System for controlling turbulence inside and just outside a cavity'
[patent_app_type] => 1
[patent_app_number] => 7/589822
[patent_app_country] => US
[patent_app_date] => 1990-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1170
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/018/05018683.pdf
[firstpage_image] =>[orig_patent_app_number] => 589822
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/589822 | System for controlling turbulence inside and just outside a cavity | Sep 26, 1990 | Issued |
Array
(
[id] => 2680781
[patent_doc_number] => 05064146
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-11-12
[patent_title] => 'Pivoting seat for fighter aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/589703
[patent_app_country] => US
[patent_app_date] => 1990-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 1456
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/064/05064146.pdf
[firstpage_image] =>[orig_patent_app_number] => 589703
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/589703 | Pivoting seat for fighter aircraft | Sep 25, 1990 | Issued |