
Emmanuel Lionel Moise
Supervisory Patent Examiner (ID: 18823, Phone: (571)272-3865 , Office: P/2455 )
| Most Active Art Unit | 2133 |
| Art Unit(s) | 2136, 2137, 2786, 2133, 2681, 2455, 2306, 2784 |
| Total Applications | 829 |
| Issued Applications | 688 |
| Pending Applications | 72 |
| Abandoned Applications | 70 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7659931
[patent_doc_number] => 20110309200
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-22
[patent_title] => 'Apparatus, Satellite and Method for Trapping High-Speed Particles'
[patent_app_type] => utility
[patent_app_number] => 13/165109
[patent_app_country] => US
[patent_app_date] => 2011-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4104
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0309/20110309200.pdf
[firstpage_image] =>[orig_patent_app_number] => 13165109
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/165109 | Apparatus, Satellite and Method for Trapping High-Speed Particles | Jun 20, 2011 | Abandoned |
Array
(
[id] => 7762368
[patent_doc_number] => 20120032033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-09
[patent_title] => 'Wing piercing airplane'
[patent_app_type] => utility
[patent_app_number] => 13/164056
[patent_app_country] => US
[patent_app_date] => 2011-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1221
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0032/20120032033.pdf
[firstpage_image] =>[orig_patent_app_number] => 13164056
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/164056 | Wing piercing airplane | Jun 19, 2011 | Abandoned |
Array
(
[id] => 9349278
[patent_doc_number] => 08668164
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-03-11
[patent_title] => 'Aero-acoustic optimisation method for complex-section mechanical parts and corresponding mechanical part and landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/163895
[patent_app_country] => US
[patent_app_date] => 2011-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 2389
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13163895
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/163895 | Aero-acoustic optimisation method for complex-section mechanical parts and corresponding mechanical part and landing gear | Jun 19, 2011 | Issued |
Array
(
[id] => 8519505
[patent_doc_number] => 20120318913
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'ON-BOARD AIRCRAFT AUXILIARY POWER SYSTEMS HAVING DUAL AUXILIARY POWER UNITS'
[patent_app_type] => utility
[patent_app_number] => 13/162931
[patent_app_country] => US
[patent_app_date] => 2011-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2496
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13162931
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/162931 | On-board aircraft auxiliary power systems having dual auxiliary power units | Jun 16, 2011 | Issued |
Array
(
[id] => 8519520
[patent_doc_number] => 20120318928
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'Spacecraft magnetic shield'
[patent_app_type] => utility
[patent_app_number] => 13/134733
[patent_app_country] => US
[patent_app_date] => 2011-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1676
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13134733
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/134733 | Spacecraft magnetic shield | Jun 14, 2011 | Issued |
Array
(
[id] => 8517277
[patent_doc_number] => 20120316685
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-13
[patent_title] => 'GIMBAL SYSTEM WITH LINEAR MOUNT'
[patent_app_type] => utility
[patent_app_number] => 13/155129
[patent_app_country] => US
[patent_app_date] => 2011-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 8444
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13155129
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/155129 | Gimbal system with linear mount | Jun 6, 2011 | Issued |
Array
(
[id] => 8506298
[patent_doc_number] => 20120305706
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'System and Method for Insulating Frame Member'
[patent_app_type] => utility
[patent_app_number] => 13/154422
[patent_app_country] => US
[patent_app_date] => 2011-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 11169
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13154422
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/154422 | System and method for insulating frame member | Jun 5, 2011 | Issued |
Array
(
[id] => 8506303
[patent_doc_number] => 20120305711
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'INTEGRAL THERMALLY INSULATED FUEL BLADDER'
[patent_app_type] => utility
[patent_app_number] => 13/152221
[patent_app_country] => US
[patent_app_date] => 2011-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3669
[patent_no_of_claims] => 18
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13152221
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/152221 | Integral thermally insulated fuel bladder | Jun 1, 2011 | Issued |
Array
(
[id] => 8310210
[patent_doc_number] => 20120187237
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'DIRECTIONAL CONTROL FOR A HELICOPTER'
[patent_app_type] => utility
[patent_app_number] => 13/149333
[patent_app_country] => US
[patent_app_date] => 2011-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2143
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13149333
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/149333 | Directional control for a helicopter | May 30, 2011 | Issued |
Array
(
[id] => 9243178
[patent_doc_number] => 08607453
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-17
[patent_title] => 'Method of manufacture by superplastic forming and by fishplating of a rib for an aerodynamic fairing of an aircraft engine mounting pylon'
[patent_app_type] => utility
[patent_app_number] => 13/115408
[patent_app_country] => US
[patent_app_date] => 2011-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 4387
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13115408
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/115408 | Method of manufacture by superplastic forming and by fishplating of a rib for an aerodynamic fairing of an aircraft engine mounting pylon | May 24, 2011 | Issued |
Array
(
[id] => 7577053
[patent_doc_number] => 20110290935
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-01
[patent_title] => 'METHOD OF MANUFACTURE BY SUPERPLASTIC FORMING AND BY FISHPLATING OF A RIB FOR AN AERODYNAMIC FAIRING OF AN AIRCRAFT ENGINE MOUNTING PYLON'
[patent_app_type] => utility
[patent_app_number] => 13/115331
[patent_app_country] => US
[patent_app_date] => 2011-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3990
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0290/20110290935.pdf
[firstpage_image] =>[orig_patent_app_number] => 13115331
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/115331 | Method of manufacture by superplastic forming and by fishplating of a rib for an aerodynamic fairing of an aircraft engine mounting pylon | May 24, 2011 | Issued |
Array
(
[id] => 8493042
[patent_doc_number] => 20120292449
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-22
[patent_title] => 'IN-SPACE PROCESSING AND DELIVERY SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/113001
[patent_app_country] => US
[patent_app_date] => 2011-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 7210
[patent_no_of_claims] => 55
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13113001
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/113001 | In-space processing and delivery system | May 19, 2011 | Issued |
Array
(
[id] => 8705182
[patent_doc_number] => 20130062471
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-14
[patent_title] => 'INCLINED ORBIT SATELLITE COMMUNICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/112117
[patent_app_country] => US
[patent_app_date] => 2011-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 8022
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13112117
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/112117 | INCLINED ORBIT SATELLITE COMMUNICATION SYSTEM | May 19, 2011 | Abandoned |
Array
(
[id] => 8493033
[patent_doc_number] => 20120292441
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-22
[patent_title] => 'SYSTEM AND METHOD FOR REDUCING THE NOISE OF PUSHER TYPE AIRCRAFT PROPELLERS'
[patent_app_type] => utility
[patent_app_number] => 13/111414
[patent_app_country] => US
[patent_app_date] => 2011-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6078
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13111414
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/111414 | System and method for reducing the noise of pusher type aircraft propellers | May 18, 2011 | Issued |
Array
(
[id] => 7583885
[patent_doc_number] => 20110278395
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-17
[patent_title] => 'STRUCTURAL COMPONENT WITH IMPROVED CONDUCTIVITY AND MECHANICAL STRENGTH, AND A METHOD FOR ITS MANUFACTURE'
[patent_app_type] => utility
[patent_app_number] => 13/105959
[patent_app_country] => US
[patent_app_date] => 2011-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3766
[patent_no_of_claims] => 19
[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/A1/0278/20110278395.pdf
[firstpage_image] =>[orig_patent_app_number] => 13105959
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/105959 | Structural component with improved conductivity and mechanical strength, and a method for its manufacture | May 11, 2011 | Issued |
Array
(
[id] => 8338680
[patent_doc_number] => 08240603
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-14
[patent_title] => 'Mat for reducing the disturbance of particulate matter and liquids by wind'
[patent_app_type] => utility
[patent_app_number] => 13/064812
[patent_app_country] => US
[patent_app_date] => 2011-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 4973
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 260
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13064812
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/064812 | Mat for reducing the disturbance of particulate matter and liquids by wind | Apr 17, 2011 | Issued |
Array
(
[id] => 9389730
[patent_doc_number] => 08686329
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-01
[patent_title] => 'Torsion spring wing deployment initiator'
[patent_app_type] => utility
[patent_app_number] => 13/378183
[patent_app_country] => US
[patent_app_date] => 2011-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 56
[patent_no_of_words] => 3726
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13378183
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/378183 | Torsion spring wing deployment initiator | Apr 7, 2011 | Issued |
Array
(
[id] => 7787438
[patent_doc_number] => 20120048994
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-01
[patent_title] => 'Air Vehicle Flight Mechanism and Control Method'
[patent_app_type] => utility
[patent_app_number] => 13/023772
[patent_app_country] => US
[patent_app_date] => 2011-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 44
[patent_figures_cnt] => 44
[patent_no_of_words] => 11110
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0048/20120048994.pdf
[firstpage_image] =>[orig_patent_app_number] => 13023772
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/023772 | Air vehicle flight mechanism and control method | Feb 8, 2011 | Issued |
Array
(
[id] => 5960317
[patent_doc_number] => 20110184704
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-28
[patent_title] => 'Fairing of aircraft elevator'
[patent_app_type] => utility
[patent_app_number] => 12/927380
[patent_app_country] => US
[patent_app_date] => 2010-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2316
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0184/20110184704.pdf
[firstpage_image] =>[orig_patent_app_number] => 12927380
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/927380 | Fairing of aircraft elevator | Nov 11, 2010 | Abandoned |
Array
(
[id] => 9231280
[patent_doc_number] => 08596580
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-12-03
[patent_title] => 'Advanced performance refueling boom'
[patent_app_type] => utility
[patent_app_number] => 12/891394
[patent_app_country] => US
[patent_app_date] => 2010-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 17
[patent_no_of_words] => 5098
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12891394
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/891394 | Advanced performance refueling boom | Sep 26, 2010 | Issued |