
Ronald B. Abelson
Examiner (ID: 14522, Phone: (571)272-3165 , Office: P/2476 )
| Most Active Art Unit | 2476 |
| Art Unit(s) | 2666, 2476, 2419, 2619, 2616, 2663 |
| Total Applications | 2097 |
| Issued Applications | 1821 |
| Pending Applications | 143 |
| Abandoned Applications | 161 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 9098067
[patent_doc_number] => 08561937
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-22
[patent_title] => 'Unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 12/906096
[patent_app_country] => US
[patent_app_date] => 2010-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 6367
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 229
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12906096
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/906096 | Unmanned aerial vehicle | Oct 16, 2010 | Issued |
Array
(
[id] => 8801044
[patent_doc_number] => 08439313
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-14
[patent_title] => 'Forward swept winglet'
[patent_app_type] => utility
[patent_app_number] => 12/905382
[patent_app_country] => US
[patent_app_date] => 2010-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 17
[patent_no_of_words] => 6646
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12905382
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/905382 | Forward swept winglet | Oct 14, 2010 | Issued |
Array
(
[id] => 7544124
[patent_doc_number] => 08052088
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-08
[patent_title] => 'Injection-molded window panel and related methods'
[patent_app_type] => utility
[patent_app_number] => 12/904547
[patent_app_country] => US
[patent_app_date] => 2010-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 3080
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/052/08052088.pdf
[firstpage_image] =>[orig_patent_app_number] => 12904547
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/904547 | Injection-molded window panel and related methods | Oct 13, 2010 | Issued |
Array
(
[id] => 6192798
[patent_doc_number] => 20110024552
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-02-03
[patent_title] => 'Anhedral Tip Blades for Tiltrotor Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/903928
[patent_app_country] => US
[patent_app_date] => 2010-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7860
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0024/20110024552.pdf
[firstpage_image] =>[orig_patent_app_number] => 12903928
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/903928 | Anhedral tip blades for tiltrotor aircraft | Oct 12, 2010 | Issued |
Array
(
[id] => 6183739
[patent_doc_number] => 20110168835
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'Three Wing, Six Tilt-Propulsion Units, VTOL Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/900790
[patent_app_country] => US
[patent_app_date] => 2010-10-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 9987
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0168/20110168835.pdf
[firstpage_image] =>[orig_patent_app_number] => 12900790
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/900790 | Three wing, six tilt-propulsion units, VTOL aircraft | Oct 7, 2010 | Issued |
Array
(
[id] => 6026525
[patent_doc_number] => 20110079677
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-07
[patent_title] => 'Ornithopter'
[patent_app_type] => utility
[patent_app_number] => 12/924592
[patent_app_country] => US
[patent_app_date] => 2010-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2092
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0079/20110079677.pdf
[firstpage_image] =>[orig_patent_app_number] => 12924592
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/924592 | Ornithopter | Sep 29, 2010 | Abandoned |
Array
(
[id] => 6026527
[patent_doc_number] => 20110079679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-07
[patent_title] => 'DEVICE FOR LOCKING AN ENGINE ON AN AIRCRAFT PYLON'
[patent_app_type] => utility
[patent_app_number] => 12/894726
[patent_app_country] => US
[patent_app_date] => 2010-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2478
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0079/20110079679.pdf
[firstpage_image] =>[orig_patent_app_number] => 12894726
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/894726 | Device for locking an engine on an aircraft pylon | Sep 29, 2010 | Issued |
Array
(
[id] => 8434271
[patent_doc_number] => 08282037
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-09
[patent_title] => 'Nacelle flow assembly'
[patent_app_type] => utility
[patent_app_number] => 12/894505
[patent_app_country] => US
[patent_app_date] => 2010-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1835
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 121
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12894505
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/894505 | Nacelle flow assembly | Sep 29, 2010 | Issued |
Array
(
[id] => 8049063
[patent_doc_number] => 20120074263
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-29
[patent_title] => 'Dynamically controlled cross flow instability inhibiting assembly'
[patent_app_type] => utility
[patent_app_number] => 12/893618
[patent_app_country] => US
[patent_app_date] => 2010-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0074/20120074263.pdf
[firstpage_image] =>[orig_patent_app_number] => 12893618
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/893618 | Dynamically controlled cross flow instability inhibiting assembly | Sep 28, 2010 | Issued |
Array
(
[id] => 8919547
[patent_doc_number] => 08485471
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-16
[patent_title] => 'Passive ejection seat arm flail restraint apparatus and method'
[patent_app_type] => utility
[patent_app_number] => 12/893217
[patent_app_country] => US
[patent_app_date] => 2010-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2199
[patent_no_of_claims] => 16
[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] =>[firstpage_image] =>[orig_patent_app_number] => 12893217
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/893217 | Passive ejection seat arm flail restraint apparatus and method | Sep 28, 2010 | Issued |
Array
(
[id] => 8857063
[patent_doc_number] => 08459588
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-06-11
[patent_title] => 'Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels'
[patent_app_type] => utility
[patent_app_number] => 12/892374
[patent_app_country] => US
[patent_app_date] => 2010-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12892374
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/892374 | Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels | Sep 27, 2010 | Issued |
Array
(
[id] => 9284675
[patent_doc_number] => 08640994
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-02-04
[patent_title] => 'Agile dedicated spacecraft for spinning microwave imagers and sounders'
[patent_app_type] => utility
[patent_app_number] => 12/891094
[patent_app_country] => US
[patent_app_date] => 2010-09-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12891094
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/891094 | Agile dedicated spacecraft for spinning microwave imagers and sounders | Sep 26, 2010 | Issued |
Array
(
[id] => 4477638
[patent_doc_number] => 07900877
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-03-08
[patent_title] => 'Active winglet'
[patent_app_type] => utility
[patent_app_number] => 12/890557
[patent_app_country] => US
[patent_app_date] => 2010-09-24
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/900/07900877.pdf
[firstpage_image] =>[orig_patent_app_number] => 12890557
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/890557 | Active winglet | Sep 23, 2010 | Issued |
Array
(
[id] => 8758451
[patent_doc_number] => 08418967
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-16
[patent_title] => 'Passive adaptive structures'
[patent_app_type] => utility
[patent_app_number] => 12/859966
[patent_app_country] => US
[patent_app_date] => 2010-08-20
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12859966
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/859966 | Passive adaptive structures | Aug 19, 2010 | Issued |
Array
(
[id] => 8993430
[patent_doc_number] => 08517302
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Aircraft with integrated lift and propulsion system'
[patent_app_type] => utility
[patent_app_number] => 12/857191
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/857191 | Aircraft with integrated lift and propulsion system | Aug 15, 2010 | Issued |
Array
(
[id] => 7738519
[patent_doc_number] => 20120018590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-26
[patent_title] => 'Bernoulli Micro Plane'
[patent_app_type] => utility
[patent_app_number] => 12/839423
[patent_app_country] => US
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[pdf_file] => publications/A1/0018/20120018590.pdf
[firstpage_image] =>[orig_patent_app_number] => 12839423
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/839423 | Bernoulli Micro Plane | Jul 19, 2010 | Abandoned |
Array
(
[id] => 6129911
[patent_doc_number] => 20110006155
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-13
[patent_title] => 'Actuator Arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/830739
[patent_app_country] => US
[patent_app_date] => 2010-07-06
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0006/20110006155.pdf
[firstpage_image] =>[orig_patent_app_number] => 12830739
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/830739 | Actuator arrangement | Jul 5, 2010 | Issued |
Array
(
[id] => 6183745
[patent_doc_number] => 20110168836
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'AIRCRAFT ENGINE SUPPORTING PYLON'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/830749 | Aircraft engine supporting pylon | Jul 5, 2010 | Issued |
Array
(
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[patent_title] => 'System and method for transporting cargo utilizing an air towing system that can achieve vertical take-off and vertical landing'
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Array
(
[id] => 9084798
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[patent_title] => 'Cross-bleed dam'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/821517 | Cross-bleed dam | Jun 22, 2010 | Issued |