
Marc R. Burgess
Examiner (ID: 6453, Phone: (571)272-9385 , Office: P/3643 )
| Most Active Art Unit | 3643 |
| Art Unit(s) | 3642, 3643, 3666, 3615, 3647 |
| Total Applications | 628 |
| Issued Applications | 221 |
| Pending Applications | 101 |
| Abandoned Applications | 321 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8131351
[patent_doc_number] => 20120090229
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-19
[patent_title] => 'REFLECTIVE NETTING MATERIAL'
[patent_app_type] => utility
[patent_app_number] => 13/264309
[patent_app_country] => US
[patent_app_date] => 2010-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 5104
[patent_no_of_claims] => 81
[patent_no_of_ind_claims] => 80
[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] => 13264309
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/264309 | REFLECTIVE NETTING MATERIAL | Apr 15, 2010 | Abandoned |
Array
(
[id] => 15781251
[patent_doc_number] => 10624324
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-21
[patent_title] => Fishing device
[patent_app_type] => utility
[patent_app_number] => 13/264297
[patent_app_country] => US
[patent_app_date] => 2010-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1983
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 677
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13264297
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/264297 | Fishing device | Apr 13, 2010 | Issued |
Array
(
[id] => 7706162
[patent_doc_number] => 20120001028
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-05
[patent_title] => 'WING OF AN AIRCRAFT AND ASSEMBLY OF A WING COMPRISING A DEVICE FOR INFLUENCING A FLOW'
[patent_app_type] => utility
[patent_app_number] => 13/254841
[patent_app_country] => US
[patent_app_date] => 2010-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 10685
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 8
[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] => 13254841
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/254841 | Wing of an aircraft and assembly of a wing comprising a device for influencing a flow | Mar 3, 2010 | Issued |
Array
(
[id] => 8298818
[patent_doc_number] => 20120181376
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-19
[patent_title] => 'MUNITION AND GUIDANCE NAVIGATION AND CONTROL UNIT'
[patent_app_type] => utility
[patent_app_number] => 12/689837
[patent_app_country] => US
[patent_app_date] => 2010-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 4388
[patent_no_of_claims] => 14
[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] => 12689837
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/689837 | MUNITION AND GUIDANCE NAVIGATION AND CONTROL UNIT | Jan 18, 2010 | Abandoned |
Array
(
[id] => 6167088
[patent_doc_number] => 20110174230
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-21
[patent_title] => 'FERTILIZED EGGS COLLECTION APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 13/121627
[patent_app_country] => US
[patent_app_date] => 2009-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 13477
[patent_no_of_claims] => 25
[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] => publications/A1/0174/20110174230.pdf
[firstpage_image] =>[orig_patent_app_number] => 13121627
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/121627 | FERTILIZED EGGS COLLECTION APPARATUS | Dec 2, 2009 | Abandoned |
Array
(
[id] => 6136786
[patent_doc_number] => 20110127368
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-02
[patent_title] => 'SINGLE PLANE MOUNT SYSTEM FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/629317
[patent_app_country] => US
[patent_app_date] => 2009-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2091
[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/A1/0127/20110127368.pdf
[firstpage_image] =>[orig_patent_app_number] => 12629317
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/629317 | Single plane mount system for gas turbine engine | Dec 1, 2009 | Issued |
Array
(
[id] => 7659920
[patent_doc_number] => 20110309189
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-22
[patent_title] => 'RIGID AIRCRAFT PYLON FITTED WITH A RIB EXTENSION FOR TAKING UP THE MOMENT IN THE LENGTHWAYS DIRECTION'
[patent_app_type] => utility
[patent_app_number] => 13/131999
[patent_app_country] => US
[patent_app_date] => 2009-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3792
[patent_no_of_claims] => 10
[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/A1/0309/20110309189.pdf
[firstpage_image] =>[orig_patent_app_number] => 13131999
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/131999 | Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction | Nov 29, 2009 | Issued |
Array
(
[id] => 9501834
[patent_doc_number] => 08740140
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-03
[patent_title] => 'Multifunctional electromechanical device for landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/132158
[patent_app_country] => US
[patent_app_date] => 2009-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3094
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13132158
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/132158 | Multifunctional electromechanical device for landing gear | Nov 18, 2009 | Issued |
Array
(
[id] => 11199196
[patent_doc_number] => 09429400
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-08-30
[patent_title] => 'Flow control device and method for aircraft and missile forebody'
[patent_app_type] => utility
[patent_app_number] => 12/615218
[patent_app_country] => US
[patent_app_date] => 2009-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 14
[patent_no_of_words] => 8219
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 96
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12615218
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/615218 | Flow control device and method for aircraft and missile forebody | Nov 8, 2009 | Issued |
Array
(
[id] => 7495831
[patent_doc_number] => 20110259271
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-10-27
[patent_title] => 'ROTARY PLATFORMS'
[patent_app_type] => utility
[patent_app_number] => 13/127332
[patent_app_country] => US
[patent_app_date] => 2009-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5325
[patent_no_of_claims] => 30
[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] => publications/A1/0259/20110259271.pdf
[firstpage_image] =>[orig_patent_app_number] => 13127332
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/127332 | ROTARY PLATFORMS | Nov 2, 2009 | Abandoned |
Array
(
[id] => 5977818
[patent_doc_number] => 20110094145
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-28
[patent_title] => 'RETRACTABLE FISHING NET HAVING AN ELASTIC AND INCREMENTAL NET EXTENSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/603790
[patent_app_country] => US
[patent_app_date] => 2009-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2444
[patent_no_of_claims] => 9
[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/A1/0094/20110094145.pdf
[firstpage_image] =>[orig_patent_app_number] => 12603790
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/603790 | RETRACTABLE FISHING NET HAVING AN ELASTIC AND INCREMENTAL NET EXTENSION SYSTEM | Oct 21, 2009 | Abandoned |
Array
(
[id] => 7509654
[patent_doc_number] => 20110255968
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-10-20
[patent_title] => 'ADJUSTER DEVICE FOR AN AIRCRAFT, COMBINATION OF AN ADJUSTER DEVICE AND AN ADJUSTER DEVICE FAULT RECOGNITION FUNCTION, FAULT-TOLERANT ADJUSTER SYSTEM AND METHOD FOR RECONFIGURING THE ADJUSTER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/125381
[patent_app_country] => US
[patent_app_date] => 2009-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 9088
[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] => publications/A1/0255/20110255968.pdf
[firstpage_image] =>[orig_patent_app_number] => 13125381
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/125381 | ADJUSTER DEVICE FOR AN AIRCRAFT, COMBINATION OF AN ADJUSTER DEVICE AND AN ADJUSTER DEVICE FAULT RECOGNITION FUNCTION, FAULT-TOLERANT ADJUSTER SYSTEM AND METHOD FOR RECONFIGURING THE ADJUSTER SYSTEM | Oct 21, 2009 | Abandoned |
Array
(
[id] => 11191251
[patent_doc_number] => 09422050
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Fore flap disposed on the wing of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/122733
[patent_app_country] => US
[patent_app_date] => 2009-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3880
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 396
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13122733
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/122733 | Fore flap disposed on the wing of an aircraft | Oct 5, 2009 | Issued |
Array
(
[id] => 8076535
[patent_doc_number] => 20120011770
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-19
[patent_title] => 'SEED STICKER AND METHOD FOR MANUFACTURING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/259922
[patent_app_country] => US
[patent_app_date] => 2009-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2081
[patent_no_of_claims] => 6
[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/A1/0011/20120011770.pdf
[firstpage_image] =>[orig_patent_app_number] => 13259922
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/259922 | Seed sticker | Sep 28, 2009 | Issued |
Array
(
[id] => 6183247
[patent_doc_number] => 20110168483
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'BLUFF BODY NOISE CONTROL'
[patent_app_type] => utility
[patent_app_number] => 12/998115
[patent_app_country] => US
[patent_app_date] => 2009-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 7275
[patent_no_of_claims] => 23
[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/A1/0168/20110168483.pdf
[firstpage_image] =>[orig_patent_app_number] => 12998115
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/998115 | BLUFF BODY NOISE CONTROL | Sep 27, 2009 | Abandoned |
Array
(
[id] => 9573550
[patent_doc_number] => 08763959
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-01
[patent_title] => 'Two-element airfoil configured for minimizing accretion of contaminant'
[patent_app_type] => utility
[patent_app_number] => 13/119319
[patent_app_country] => US
[patent_app_date] => 2009-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 32
[patent_no_of_words] => 9186
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13119319
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/119319 | Two-element airfoil configured for minimizing accretion of contaminant | Sep 15, 2009 | Issued |
Array
(
[id] => 6098444
[patent_doc_number] => 20110163205
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-07
[patent_title] => 'AEROFOIL ACCESSORIES AND METHOD FOR MODIFYING THE GEOMETRY OF A WING ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/119315
[patent_app_country] => US
[patent_app_date] => 2009-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 11536
[patent_no_of_claims] => 25
[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/A1/0163/20110163205.pdf
[firstpage_image] =>[orig_patent_app_number] => 13119315
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/119315 | Aerofoil accessories and method for modifying the geometry of a wing element | Sep 15, 2009 | Issued |
Array
(
[id] => 5931810
[patent_doc_number] => 20110210206
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-01
[patent_title] => 'CONNECTION OF A WING TO A FUSELAGE OF AN AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 13/058552
[patent_app_country] => US
[patent_app_date] => 2009-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5098
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 11
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0210/20110210206.pdf
[firstpage_image] =>[orig_patent_app_number] => 13058552
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/058552 | Connection of a wing to a fuselage of an airplane | Aug 17, 2009 | Issued |
Array
(
[id] => 8531961
[patent_doc_number] => 08308111
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Panel assembly for a space-based power generation system'
[patent_app_type] => utility
[patent_app_number] => 12/512531
[patent_app_country] => US
[patent_app_date] => 2009-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 2009
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[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] => 12512531
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/512531 | Panel assembly for a space-based power generation system | Jul 29, 2009 | Issued |
Array
(
[id] => 8646365
[patent_doc_number] => 20130032095
[patent_country] => US
[patent_kind] => A2
[patent_issue_date] => 2013-02-07
[patent_title] => 'TRANSPORTING UNIT FOR LIVE POULTRY ON BOARD A TRUCK'
[patent_app_type] => utility
[patent_app_number] => 13/384979
[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] => 2395
[patent_no_of_claims] => 45
[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] => 13384979
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/384979 | Method for transporting live poultry on board a truck | Jul 19, 2009 | Issued |