
Matthew A. Hopkins
Examiner (ID: 7651, Phone: (571)270-5154 , Office: P/2463 )
| Most Active Art Unit | 2463 |
| Art Unit(s) | 2463 |
| Total Applications | 267 |
| Issued Applications | 210 |
| Pending Applications | 0 |
| Abandoned Applications | 58 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 3051057
[patent_doc_number] => 05351914
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-10-04
[patent_title] => 'Hydraulic control system for aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/894554
[patent_app_country] => US
[patent_app_date] => 1992-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 4127
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/351/05351914.pdf
[firstpage_image] =>[orig_patent_app_number] => 894554
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/894554 | Hydraulic control system for aircraft | Jun 4, 1992 | Issued |
Array
(
[id] => 2818063
[patent_doc_number] => 05174523
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-29
[patent_title] => 'Compound helicopter with engine shaft power output control'
[patent_app_type] => 1
[patent_app_number] => 7/895166
[patent_app_country] => US
[patent_app_date] => 1992-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2670
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 357
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/174/05174523.pdf
[firstpage_image] =>[orig_patent_app_number] => 895166
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/895166 | Compound helicopter with engine shaft power output control | Jun 4, 1992 | Issued |
Array
(
[id] => 3071757
[patent_doc_number] => 05277348
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-11
[patent_title] => 'Articulated parachute harness'
[patent_app_type] => 1
[patent_app_number] => 7/892205
[patent_app_country] => US
[patent_app_date] => 1992-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 10
[patent_no_of_words] => 3369
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/277/05277348.pdf
[firstpage_image] =>[orig_patent_app_number] => 892205
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/892205 | Articulated parachute harness | Jun 1, 1992 | Issued |
Array
(
[id] => 2883704
[patent_doc_number] => 05271581
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-12-21
[patent_title] => 'Window clip for aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/891544
[patent_app_country] => US
[patent_app_date] => 1992-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 1157
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/271/05271581.pdf
[firstpage_image] =>[orig_patent_app_number] => 891544
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/891544 | Window clip for aircraft | May 28, 1992 | Issued |
Array
(
[id] => 2884992
[patent_doc_number] => 05217185
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-06-08
[patent_title] => 'Ablative shielding for hypervelocity projectiles'
[patent_app_type] => 1
[patent_app_number] => 7/887674
[patent_app_country] => US
[patent_app_date] => 1992-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2249
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/217/05217185.pdf
[firstpage_image] =>[orig_patent_app_number] => 887674
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/887674 | Ablative shielding for hypervelocity projectiles | May 20, 1992 | Issued |
Array
(
[id] => 2884974
[patent_doc_number] => 05217184
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-06-08
[patent_title] => 'Retaining wall for holding cargo in an aircraft cabin'
[patent_app_type] => 1
[patent_app_number] => 7/883425
[patent_app_country] => US
[patent_app_date] => 1992-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3107
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/217/05217184.pdf
[firstpage_image] =>[orig_patent_app_number] => 883425
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/883425 | Retaining wall for holding cargo in an aircraft cabin | May 12, 1992 | Issued |
Array
(
[id] => 2883723
[patent_doc_number] => 05271582
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-12-21
[patent_title] => 'Modular mother satellite bus for subsidiary payloads'
[patent_app_type] => 1
[patent_app_number] => 7/877145
[patent_app_country] => US
[patent_app_date] => 1992-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 18
[patent_no_of_words] => 9460
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/271/05271582.pdf
[firstpage_image] =>[orig_patent_app_number] => 877145
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/877145 | Modular mother satellite bus for subsidiary payloads | Apr 30, 1992 | Issued |
Array
(
[id] => 3030455
[patent_doc_number] => 05285986
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-02-15
[patent_title] => 'Rigid airship with a carrier frame of ribs and beams enclosed by skin sections forming an envelope'
[patent_app_type] => 1
[patent_app_number] => 7/869645
[patent_app_country] => US
[patent_app_date] => 1992-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 7076
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 248
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/285/05285986.pdf
[firstpage_image] =>[orig_patent_app_number] => 869645
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/869645 | Rigid airship with a carrier frame of ribs and beams enclosed by skin sections forming an envelope | Apr 15, 1992 | Issued |
Array
(
[id] => 2825384
[patent_doc_number] => 05170966
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-15
[patent_title] => 'Safety device for an emergency landing of an aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/866574
[patent_app_country] => US
[patent_app_date] => 1992-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2086
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/170/05170966.pdf
[firstpage_image] =>[orig_patent_app_number] => 866574
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/866574 | Safety device for an emergency landing of an aircraft | Apr 9, 1992 | Issued |
Array
(
[id] => 2871537
[patent_doc_number] => 05213285
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-05-25
[patent_title] => 'Rotating aircraft tire/landing gear apparatus'
[patent_app_type] => 1
[patent_app_number] => 7/867154
[patent_app_country] => US
[patent_app_date] => 1992-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3119
[patent_no_of_claims] => 17
[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/05/213/05213285.pdf
[firstpage_image] =>[orig_patent_app_number] => 867154
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/867154 | Rotating aircraft tire/landing gear apparatus | Apr 9, 1992 | Issued |
Array
(
[id] => 2874858
[patent_doc_number] => 05238205
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-24
[patent_title] => 'Mounting structure for a propulsion unit in a model airplane'
[patent_app_type] => 1
[patent_app_number] => 7/865534
[patent_app_country] => US
[patent_app_date] => 1992-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2345
[patent_no_of_claims] => 8
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[patent_words_short_claim] => 277
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/238/05238205.pdf
[firstpage_image] =>[orig_patent_app_number] => 865534
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/865534 | Mounting structure for a propulsion unit in a model airplane | Apr 8, 1992 | Issued |
Array
(
[id] => 3055698
[patent_doc_number] => 05294079
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-03-15
[patent_title] => 'Space transfer vehicle'
[patent_app_type] => 1
[patent_app_number] => 7/861675
[patent_app_country] => US
[patent_app_date] => 1992-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3744
[patent_no_of_claims] => 19
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/294/05294079.pdf
[firstpage_image] =>[orig_patent_app_number] => 861675
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/861675 | Space transfer vehicle | Mar 31, 1992 | Issued |
Array
(
[id] => 3001280
[patent_doc_number] => 05340057
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-23
[patent_title] => 'Thrust vectoring free wing aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/850913
[patent_app_country] => US
[patent_app_date] => 1992-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 4231
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/340/05340057.pdf
[firstpage_image] =>[orig_patent_app_number] => 850913
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/850913 | Thrust vectoring free wing aircraft | Mar 12, 1992 | Issued |
Array
(
[id] => 3073927
[patent_doc_number] => 05279484
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-18
[patent_title] => 'Manned space vehicle with low-level hydrogen-oxygen-carbon dioxide propulsion unit'
[patent_app_type] => 1
[patent_app_number] => 7/849485
[patent_app_country] => US
[patent_app_date] => 1992-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 1606
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/279/05279484.pdf
[firstpage_image] =>[orig_patent_app_number] => 849485
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/849485 | Manned space vehicle with low-level hydrogen-oxygen-carbon dioxide propulsion unit | Mar 10, 1992 | Issued |
Array
(
[id] => 3016085
[patent_doc_number] => 05348331
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-09-20
[patent_title] => 'Trailer stabilizer and method'
[patent_app_type] => 1
[patent_app_number] => 7/839622
[patent_app_country] => US
[patent_app_date] => 1992-02-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/348/05348331.pdf
[firstpage_image] =>[orig_patent_app_number] => 839622
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/839622 | Trailer stabilizer and method | Feb 20, 1992 | Issued |
Array
(
[id] => 3070189
[patent_doc_number] => 05277266
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-11
[patent_title] => 'Snow tiller to help cool the engine and lubricate the track of a snowmobile'
[patent_app_type] => 1
[patent_app_number] => 7/839902
[patent_app_country] => US
[patent_app_date] => 1992-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/277/05277266.pdf
[firstpage_image] =>[orig_patent_app_number] => 839902
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/839902 | Snow tiller to help cool the engine and lubricate the track of a snowmobile | Feb 20, 1992 | Issued |
Array
(
[id] => 3001228
[patent_doc_number] => 05340054
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-08-23
[patent_title] => 'Suppressor of oscillations in airframe cavities'
[patent_app_type] => 1
[patent_app_number] => 7/839721
[patent_app_country] => US
[patent_app_date] => 1992-02-14
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/340/05340054.pdf
[firstpage_image] =>[orig_patent_app_number] => 839721
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/839721 | Suppressor of oscillations in airframe cavities | Feb 13, 1992 | Issued |
Array
(
[id] => 3082203
[patent_doc_number] => 05292089
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-03-08
[patent_title] => 'Tie down apparatus'
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[patent_app_number] => 7/832005
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[pdf_file] => patents/05/292/05292089.pdf
[firstpage_image] =>[orig_patent_app_number] => 832005
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/832005 | Tie down apparatus | Feb 5, 1992 | Issued |
Array
(
[id] => 2919124
[patent_doc_number] => 05195701
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-23
[patent_title] => 'Air cargo container with bomb damage mitigation features'
[patent_app_type] => 1
[patent_app_number] => 7/830725
[patent_app_country] => US
[patent_app_date] => 1992-02-04
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[pdf_file] => patents/05/195/05195701.pdf
[firstpage_image] =>[orig_patent_app_number] => 830725
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/830725 | Air cargo container with bomb damage mitigation features | Feb 3, 1992 | Issued |
Array
(
[id] => 3039088
[patent_doc_number] => 05344103
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-09-06
[patent_title] => 'Actuating system for aircraft wing slat and flap panels'
[patent_app_type] => 1
[patent_app_number] => 7/825664
[patent_app_country] => US
[patent_app_date] => 1992-01-24
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/344/05344103.pdf
[firstpage_image] =>[orig_patent_app_number] => 825664
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/825664 | Actuating system for aircraft wing slat and flap panels | Jan 23, 1992 | Issued |