
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] => 6541649
[patent_doc_number] => 20100044511
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-25
[patent_title] => 'Aircraft structure'
[patent_app_type] => utility
[patent_app_number] => 12/458663
[patent_app_country] => US
[patent_app_date] => 2009-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2148
[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/A1/0044/20100044511.pdf
[firstpage_image] =>[orig_patent_app_number] => 12458663
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/458663 | Aircraft structure | Jul 19, 2009 | Issued |
Array
(
[id] => 8531959
[patent_doc_number] => 08308109
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Aircraft structure'
[patent_app_type] => utility
[patent_app_number] => 12/458664
[patent_app_country] => US
[patent_app_date] => 2009-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2215
[patent_no_of_claims] => 9
[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] =>[firstpage_image] =>[orig_patent_app_number] => 12458664
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/458664 | Aircraft structure | Jul 19, 2009 | Issued |
Array
(
[id] => 9025036
[patent_doc_number] => 08534610
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-09-17
[patent_title] => 'Method and apparatus for a leading edge slat on a wing of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/505061
[patent_app_country] => US
[patent_app_date] => 2009-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 5946
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 136
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12505061
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/505061 | Method and apparatus for a leading edge slat on a wing of an aircraft | Jul 16, 2009 | Issued |
Array
(
[id] => 7544117
[patent_doc_number] => 08052081
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-08
[patent_title] => 'Dual rotor helicopter with tilted rotational axes'
[patent_app_type] => utility
[patent_app_number] => 12/458608
[patent_app_country] => US
[patent_app_date] => 2009-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 18
[patent_no_of_words] => 4650
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 82
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/052/08052081.pdf
[firstpage_image] =>[orig_patent_app_number] => 12458608
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/458608 | Dual rotor helicopter with tilted rotational axes | Jul 15, 2009 | Issued |
Array
(
[id] => 6279302
[patent_doc_number] => 20100155529
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-24
[patent_title] => 'Landing gear with noise reduction fairing'
[patent_app_type] => utility
[patent_app_number] => 12/458407
[patent_app_country] => US
[patent_app_date] => 2009-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3335
[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] => publications/A1/0155/20100155529.pdf
[firstpage_image] =>[orig_patent_app_number] => 12458407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/458407 | Landing gear with noise reduction fairing | Jul 9, 2009 | Issued |
Array
(
[id] => 7794466
[patent_doc_number] => 08123171
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Load assisted release system'
[patent_app_type] => utility
[patent_app_number] => 12/494842
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 14
[patent_no_of_words] => 6423
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/123/08123171.pdf
[firstpage_image] =>[orig_patent_app_number] => 12494842
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/494842 | Load assisted release system | Jun 29, 2009 | Issued |
Array
(
[id] => 9072830
[patent_doc_number] => 08550400
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-08
[patent_title] => 'Aircraft with retracted front landing gear'
[patent_app_type] => utility
[patent_app_number] => 12/494845
[patent_app_country] => US
[patent_app_date] => 2009-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 4583
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12494845
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/494845 | Aircraft with retracted front landing gear | Jun 29, 2009 | Issued |
Array
(
[id] => 5461361
[patent_doc_number] => 20090321561
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'NACELLE FOR AIRCRAFT COMPRISING MEANS OF REVERSING THRUST AND AIRCRAFT COMPRISING AT LEAST ONE SUCH NACELLE'
[patent_app_type] => utility
[patent_app_number] => 12/491746
[patent_app_country] => US
[patent_app_date] => 2009-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4705
[patent_no_of_claims] => 13
[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/A1/0321/20090321561.pdf
[firstpage_image] =>[orig_patent_app_number] => 12491746
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/491746 | Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle | Jun 24, 2009 | Issued |
Array
(
[id] => 6602428
[patent_doc_number] => 20100032948
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-11
[patent_title] => 'Method and apparatus for operating and controlling airborne wind energy generation craft and the generation of electrical energy using such craft'
[patent_app_type] => utility
[patent_app_number] => 12/459017
[patent_app_country] => US
[patent_app_date] => 2009-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 10170
[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] => publications/A1/0032/20100032948.pdf
[firstpage_image] =>[orig_patent_app_number] => 12459017
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/459017 | Method and apparatus for operating and controlling airborne wind energy generation craft and the generation of electrical energy using such craft | Jun 24, 2009 | Abandoned |
Array
(
[id] => 6244561
[patent_doc_number] => 20100024387
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'AIRCRAFT NACELLE WHICH INCLUDES THRUST REVERSER SYSTEM AND AIRCRAFT INCORPORATING AT LEAST ONE SUCH NACELLE'
[patent_app_type] => utility
[patent_app_number] => 12/490964
[patent_app_country] => US
[patent_app_date] => 2009-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4394
[patent_no_of_claims] => 13
[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/A1/0024/20100024387.pdf
[firstpage_image] =>[orig_patent_app_number] => 12490964
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/490964 | Aircraft nacelle which includes thrust reverser system and aircraft incorporating at least one such nacelle | Jun 23, 2009 | Issued |
Array
(
[id] => 6129898
[patent_doc_number] => 20110006151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-13
[patent_title] => 'AERIAL RECOVERY OF SMALL AND MICRO AIR VEHICLES'
[patent_app_type] => utility
[patent_app_number] => 12/487907
[patent_app_country] => US
[patent_app_date] => 2009-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3913
[patent_no_of_claims] => 18
[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/A1/0006/20110006151.pdf
[firstpage_image] =>[orig_patent_app_number] => 12487907
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/487907 | AERIAL RECOVERY OF SMALL AND MICRO AIR VEHICLES | Jun 18, 2009 | Abandoned |
Array
(
[id] => 6247584
[patent_doc_number] => 20100026007
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Apparatus and method for harvesting wind power using tethered airfoil'
[patent_app_type] => utility
[patent_app_number] => 12/456694
[patent_app_country] => US
[patent_app_date] => 2009-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4293
[patent_no_of_claims] => 30
[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/A1/0026/20100026007.pdf
[firstpage_image] =>[orig_patent_app_number] => 12456694
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/456694 | Apparatus and method for harvesting wind power using tethered airfoil | Jun 18, 2009 | Abandoned |
Array
(
[id] => 7995403
[patent_doc_number] => 08079546
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-12-20
[patent_title] => 'Samara wing'
[patent_app_type] => utility
[patent_app_number] => 12/456585
[patent_app_country] => US
[patent_app_date] => 2009-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3557
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/079/08079546.pdf
[firstpage_image] =>[orig_patent_app_number] => 12456585
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/456585 | Samara wing | Jun 17, 2009 | Issued |
Array
(
[id] => 8197730
[patent_doc_number] => 08186617
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Aircraft having a lambda-box wing configuration'
[patent_app_type] => utility
[patent_app_number] => 12/481854
[patent_app_country] => US
[patent_app_date] => 2009-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4646
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 259
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/186/08186617.pdf
[firstpage_image] =>[orig_patent_app_number] => 12481854
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/481854 | Aircraft having a lambda-box wing configuration | Jun 9, 2009 | Issued |
Array
(
[id] => 5371421
[patent_doc_number] => 20090308981
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-17
[patent_title] => 'AIRCRAFT WING ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 12/481267
[patent_app_country] => US
[patent_app_date] => 2009-06-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2596
[patent_no_of_claims] => 17
[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/A1/0308/20090308981.pdf
[firstpage_image] =>[orig_patent_app_number] => 12481267
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/481267 | Aircraft wing assembly | Jun 8, 2009 | Issued |
Array
(
[id] => 5364603
[patent_doc_number] => 20090302162
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'PASSIVE VARIABLE SPEED DROGUE'
[patent_app_type] => utility
[patent_app_number] => 12/477696
[patent_app_country] => US
[patent_app_date] => 2009-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2118
[patent_no_of_claims] => 15
[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/A1/0302/20090302162.pdf
[firstpage_image] =>[orig_patent_app_number] => 12477696
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/477696 | PASSIVE VARIABLE SPEED DROGUE | Jun 2, 2009 | Abandoned |
Array
(
[id] => 8327239
[patent_doc_number] => 08235329
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-08-07
[patent_title] => 'Dynamically actuated adaptive control structures'
[patent_app_type] => utility
[patent_app_number] => 12/476484
[patent_app_country] => US
[patent_app_date] => 2009-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 13
[patent_no_of_words] => 3337
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 65
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12476484
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/476484 | Dynamically actuated adaptive control structures | Jun 1, 2009 | Issued |
Array
(
[id] => 6374277
[patent_doc_number] => 20100301159
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-02
[patent_title] => 'Mounting set, system and method'
[patent_app_type] => utility
[patent_app_number] => 12/457120
[patent_app_country] => US
[patent_app_date] => 2009-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 9746
[patent_no_of_claims] => 43
[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/A1/0301/20100301159.pdf
[firstpage_image] =>[orig_patent_app_number] => 12457120
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/457120 | Mounting set, system and method | May 31, 2009 | Issued |
Array
(
[id] => 7540753
[patent_doc_number] => 08058597
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-15
[patent_title] => 'Low cost deployment system and method for airborne object'
[patent_app_type] => utility
[patent_app_number] => 12/436567
[patent_app_country] => US
[patent_app_date] => 2009-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3502
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/058/08058597.pdf
[firstpage_image] =>[orig_patent_app_number] => 12436567
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/436567 | Low cost deployment system and method for airborne object | May 5, 2009 | Issued |
Array
(
[id] => 5483080
[patent_doc_number] => 20090272845
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-05
[patent_title] => 'AIRSHIP HANDLING DEVICES AND ASSOCIATED SYSTEMS AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 12/432631
[patent_app_country] => US
[patent_app_date] => 2009-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 6916
[patent_no_of_claims] => 21
[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/A1/0272/20090272845.pdf
[firstpage_image] =>[orig_patent_app_number] => 12432631
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/432631 | AIRSHIP HANDLING DEVICES AND ASSOCIATED SYSTEMS AND METHODS | Apr 28, 2009 | Abandoned |