
Frederick Lyndon Lagman
Examiner (ID: 14185, Phone: (571)272-7043 , Office: P/3678 )
Most Active Art Unit | 3678 |
Art Unit(s) | 3678, 3672, 3501, 3625, 3673, 3506 |
Total Applications | 3144 |
Issued Applications | 2523 |
Pending Applications | 198 |
Abandoned Applications | 421 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 6430411
[patent_doc_number] => 20100281874
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-11
[patent_title] => 'Airflow vectoring member'
[patent_app_type] => utility
[patent_app_number] => 12/006981
[patent_app_country] => US
[patent_app_date] => 2008-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3037
[patent_no_of_claims] => 23
[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/A1/0281/20100281874.pdf
[firstpage_image] =>[orig_patent_app_number] => 12006981
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/006981 | Airflow vectoring member | Jan 7, 2008 | Abandoned |
Array
(
[id] => 7985277
[patent_doc_number] => 08074931
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-12-13
[patent_title] => 'Drogue deploying/retrieval device, system, and method'
[patent_app_type] => utility
[patent_app_number] => 11/938636
[patent_app_country] => US
[patent_app_date] => 2007-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 11
[patent_no_of_words] => 3300
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/074/08074931.pdf
[firstpage_image] =>[orig_patent_app_number] => 11938636
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/938636 | Drogue deploying/retrieval device, system, and method | Nov 11, 2007 | Issued |
Array
(
[id] => 5262088
[patent_doc_number] => 20090114773
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-07
[patent_title] => 'METHODS FOR FUEL-EFFICIENT TRANSPORTATION OF CARGO BY AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/935328
[patent_app_country] => US
[patent_app_date] => 2007-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4243
[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/A1/0114/20090114773.pdf
[firstpage_image] =>[orig_patent_app_number] => 11935328
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/935328 | METHODS FOR FUEL-EFFICIENT TRANSPORTATION OF CARGO BY AIRCRAFT | Nov 4, 2007 | Abandoned |
Array
(
[id] => 5327657
[patent_doc_number] => 20090108134
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-30
[patent_title] => 'ICING PROTECTION SYSTEM AND METHOD FOR ENHANCING HEAT TRANSFER'
[patent_app_type] => utility
[patent_app_number] => 11/923753
[patent_app_country] => US
[patent_app_date] => 2007-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4809
[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/A1/0108/20090108134.pdf
[firstpage_image] =>[orig_patent_app_number] => 11923753
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/923753 | ICING PROTECTION SYSTEM AND METHOD FOR ENHANCING HEAT TRANSFER | Oct 24, 2007 | Abandoned |
Array
(
[id] => 5431883
[patent_doc_number] => 20090166469
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Aircraft arrestor system and method of decelerating an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/977167
[patent_app_country] => US
[patent_app_date] => 2007-10-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1308
[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/A1/0166/20090166469.pdf
[firstpage_image] =>[orig_patent_app_number] => 11977167
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/977167 | Aircraft arrestor system and method of decelerating an aircraft | Oct 22, 2007 | Issued |
Array
(
[id] => 5425594
[patent_doc_number] => 20090084904
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods'
[patent_app_type] => utility
[patent_app_number] => 11/866209
[patent_app_country] => US
[patent_app_date] => 2007-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3732
[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/A1/0084/20090084904.pdf
[firstpage_image] =>[orig_patent_app_number] => 11866209
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/866209 | Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods | Oct 1, 2007 | Abandoned |
Array
(
[id] => 5425585
[patent_doc_number] => 20090084895
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'Aircraft Skid Shoes with Wear-Resistant Cladding Layers'
[patent_app_type] => utility
[patent_app_number] => 11/863398
[patent_app_country] => US
[patent_app_date] => 2007-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1970
[patent_no_of_claims] => 16
[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/A1/0084/20090084895.pdf
[firstpage_image] =>[orig_patent_app_number] => 11863398
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/863398 | Aircraft Skid Shoes with Wear-Resistant Cladding Layers | Sep 27, 2007 | Abandoned |
Array
(
[id] => 4544908
[patent_doc_number] => 07837154
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Deployable heat shield and deceleration structure for spacecraft'
[patent_app_type] => utility
[patent_app_number] => 11/903566
[patent_app_country] => US
[patent_app_date] => 2007-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 13
[patent_no_of_words] => 4037
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 269
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/837/07837154.pdf
[firstpage_image] =>[orig_patent_app_number] => 11903566
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/903566 | Deployable heat shield and deceleration structure for spacecraft | Sep 19, 2007 | Issued |
Array
(
[id] => 5268317
[patent_doc_number] => 20090072092
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'Bimodal kite system'
[patent_app_type] => utility
[patent_app_number] => 11/901262
[patent_app_country] => US
[patent_app_date] => 2007-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3744
[patent_no_of_claims] => 23
[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/A1/0072/20090072092.pdf
[firstpage_image] =>[orig_patent_app_number] => 11901262
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/901262 | Bimodal kite system | Sep 12, 2007 | Abandoned |
Array
(
[id] => 5364592
[patent_doc_number] => 20090302151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'Aircraft with fixed, swinging and folding wings'
[patent_app_type] => utility
[patent_app_number] => 11/900090
[patent_app_country] => US
[patent_app_date] => 2007-09-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3014
[patent_no_of_claims] => 20
[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/A1/0302/20090302151.pdf
[firstpage_image] =>[orig_patent_app_number] => 11900090
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/900090 | Aircraft with fixed, swinging and folding wings | Sep 9, 2007 | Issued |
Array
(
[id] => 6230861
[patent_doc_number] => 20100264264
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-21
[patent_title] => 'METHOD FOR PRODUCING AN AIRCRAFT WITH REDUCED ENVRIONMENTAL IMPACT AND THE AIRCRAFT THUS OBTAINED'
[patent_app_type] => utility
[patent_app_number] => 11/850438
[patent_app_country] => US
[patent_app_date] => 2007-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3149
[patent_no_of_claims] => 15
[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/A1/0264/20100264264.pdf
[firstpage_image] =>[orig_patent_app_number] => 11850438
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/850438 | Method for producing an aircraft with reduced environmental impact and the aircraft thus obtained | Sep 4, 2007 | Issued |
Array
(
[id] => 5345857
[patent_doc_number] => 20090001218
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'Stifffened multispar torsion box'
[patent_app_type] => utility
[patent_app_number] => 11/897029
[patent_app_country] => US
[patent_app_date] => 2007-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2031
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0001/20090001218.pdf
[firstpage_image] =>[orig_patent_app_number] => 11897029
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/897029 | Stifffened multispar torsion box | Aug 27, 2007 | Abandoned |
Array
(
[id] => 4843049
[patent_doc_number] => 20080179457
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'PASSENGER AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/775882
[patent_app_country] => US
[patent_app_date] => 2007-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2010
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20080179457.pdf
[firstpage_image] =>[orig_patent_app_number] => 11775882
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/775882 | PASSENGER AIRCRAFT | Jul 10, 2007 | Abandoned |
11/827053 | Vertical take off and landing aircraft system with energy recapture technology | Jul 9, 2007 | Abandoned |
Array
(
[id] => 4849294
[patent_doc_number] => 20080315036
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-25
[patent_title] => 'Aircraft Having Multiple Seating Configurations and Associated Systems and Methods'
[patent_app_type] => utility
[patent_app_number] => 11/767790
[patent_app_country] => US
[patent_app_date] => 2007-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4977
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0315/20080315036.pdf
[firstpage_image] =>[orig_patent_app_number] => 11767790
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/767790 | Aircraft having multiple seating configurations and associated systems and methods | Jun 24, 2007 | Issued |
Array
(
[id] => 5162903
[patent_doc_number] => 20070284483
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-13
[patent_title] => 'MOBILE AIRFOIL DEVICE FOR AN AIRCRAFT WING'
[patent_app_type] => utility
[patent_app_number] => 11/760934
[patent_app_country] => US
[patent_app_date] => 2007-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 4259
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0284/20070284483.pdf
[firstpage_image] =>[orig_patent_app_number] => 11760934
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/760934 | MOBILE AIRFOIL DEVICE FOR AN AIRCRAFT WING | Jun 10, 2007 | Abandoned |
Array
(
[id] => 8673924
[patent_doc_number] => 08382028
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-26
[patent_title] => 'Rotary wing aircraft rotating machinery vibration control system'
[patent_app_type] => utility
[patent_app_number] => 11/757002
[patent_app_country] => US
[patent_app_date] => 2007-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 5625
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11757002
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/757002 | Rotary wing aircraft rotating machinery vibration control system | May 31, 2007 | Issued |
Array
(
[id] => 4768470
[patent_doc_number] => 20080054124
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-03-06
[patent_title] => 'CONTROLLABLE REFUELING DROGUES AND ASSOCIATED SYSTEMS AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 11/752156
[patent_app_country] => US
[patent_app_date] => 2007-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4381
[patent_no_of_claims] => 26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0054/20080054124.pdf
[firstpage_image] =>[orig_patent_app_number] => 11752156
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/752156 | Controllable refueling drogues and associated systems and methods | May 21, 2007 | Issued |
Array
(
[id] => 8553665
[patent_doc_number] => 08328132
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-11
[patent_title] => 'Damage-tolerant attachment system for an aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 11/745032
[patent_app_country] => US
[patent_app_date] => 2007-05-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1527
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11745032
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/745032 | Damage-tolerant attachment system for an aircraft engine | May 6, 2007 | Issued |
Array
(
[id] => 4883684
[patent_doc_number] => 20080258016
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-23
[patent_title] => 'NACELLE ASSEMBLY WITHOUT LOWER BI-FI SPLITTER'
[patent_app_type] => utility
[patent_app_number] => 11/738607
[patent_app_country] => US
[patent_app_date] => 2007-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1083
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0258/20080258016.pdf
[firstpage_image] =>[orig_patent_app_number] => 11738607
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/738607 | NACELLE ASSEMBLY WITHOUT LOWER BI-FI SPLITTER | Apr 22, 2007 | Abandoned |