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] => 1985
[patent_doc_number] => 07815145
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-19
[patent_title] => 'Mounting system for use in mounting a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/650849
[patent_app_country] => US
[patent_app_date] => 2007-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1377
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/815/07815145.pdf
[firstpage_image] =>[orig_patent_app_number] => 11650849
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/650849 | Mounting system for use in mounting a gas turbine engine | Jan 7, 2007 | Issued |
Array
(
[id] => 7985267
[patent_doc_number] => 08074926
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-12-13
[patent_title] => 'Structural dynamic stability for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/644853
[patent_app_country] => US
[patent_app_date] => 2006-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3750
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 147
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/074/08074926.pdf
[firstpage_image] =>[orig_patent_app_number] => 11644853
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/644853 | Structural dynamic stability for an aircraft | Dec 21, 2006 | Issued |
Array
(
[id] => 8161110
[patent_doc_number] => 08172181
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Fuel range for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/644854
[patent_app_country] => US
[patent_app_date] => 2006-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2616
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/172/08172181.pdf
[firstpage_image] =>[orig_patent_app_number] => 11644854
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/644854 | Fuel range for an aircraft | Dec 21, 2006 | Issued |
Array
(
[id] => 4876380
[patent_doc_number] => 20080149763
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-26
[patent_title] => 'AIR TRANSPORT WITH SCALLOPED UNDERBODY'
[patent_app_type] => utility
[patent_app_number] => 11/614052
[patent_app_country] => US
[patent_app_date] => 2006-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3908
[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/A1/0149/20080149763.pdf
[firstpage_image] =>[orig_patent_app_number] => 11614052
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/614052 | Air transport with scalloped underbody | Dec 19, 2006 | Issued |
Array
(
[id] => 19546
[patent_doc_number] => 07798443
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-21
[patent_title] => 'Composite material for geometric morphing wing'
[patent_app_type] => utility
[patent_app_number] => 11/612244
[patent_app_country] => US
[patent_app_date] => 2006-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3566
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/798/07798443.pdf
[firstpage_image] =>[orig_patent_app_number] => 11612244
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/612244 | Composite material for geometric morphing wing | Dec 17, 2006 | Issued |
Array
(
[id] => 5250365
[patent_doc_number] => 20070131821
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-14
[patent_title] => 'Wing/winglet configuration and aircraft including it'
[patent_app_type] => utility
[patent_app_number] => 11/635616
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5187
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0131/20070131821.pdf
[firstpage_image] =>[orig_patent_app_number] => 11635616
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/635616 | Wing/winglet configuration and aircraft including it | Dec 7, 2006 | Abandoned |
Array
(
[id] => 5388890
[patent_doc_number] => 20090206202
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'Energy absorbing structure for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/636056
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3821
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0206/20090206202.pdf
[firstpage_image] =>[orig_patent_app_number] => 11636056
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/636056 | Energy absorbing structure for aircraft | Dec 7, 2006 | Issued |
Array
(
[id] => 4795153
[patent_doc_number] => 20080006739
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-10
[patent_title] => 'Vehicle power train including at least two power sources'
[patent_app_type] => utility
[patent_app_number] => 11/607854
[patent_app_country] => US
[patent_app_date] => 2006-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7761
[patent_no_of_claims] => 39
[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/A1/0006/20080006739.pdf
[firstpage_image] =>[orig_patent_app_number] => 11607854
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/607854 | Vehicle power train including at least two power sources | Dec 3, 2006 | Abandoned |
Array
(
[id] => 4828846
[patent_doc_number] => 20080128559
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-05
[patent_title] => 'Optimal sun safe attitude for satellite ground tracking'
[patent_app_type] => utility
[patent_app_number] => 11/633268
[patent_app_country] => US
[patent_app_date] => 2006-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3767
[patent_no_of_claims] => 18
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0128/20080128559.pdf
[firstpage_image] =>[orig_patent_app_number] => 11633268
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/633268 | Optimal sun safe attitude for satellite ground tracking | Dec 3, 2006 | Issued |
Array
(
[id] => 9098078
[patent_doc_number] => 08561948
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-22
[patent_title] => 'Method for ensuring the safety of an aircraft flying horizontally at low speed'
[patent_app_type] => utility
[patent_app_number] => 11/604296
[patent_app_country] => US
[patent_app_date] => 2006-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1985
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 213
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11604296
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/604296 | Method for ensuring the safety of an aircraft flying horizontally at low speed | Nov 26, 2006 | Issued |
Array
(
[id] => 165764
[patent_doc_number] => 07665689
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-23
[patent_title] => 'Unconventional integrated propulsion systems and methods for blended wing body aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/563099
[patent_app_country] => US
[patent_app_date] => 2006-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3812
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/665/07665689.pdf
[firstpage_image] =>[orig_patent_app_number] => 11563099
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/563099 | Unconventional integrated propulsion systems and methods for blended wing body aircraft | Nov 23, 2006 | Issued |
Array
(
[id] => 4900353
[patent_doc_number] => 20080119967
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-22
[patent_title] => 'Onboard Aircraft Weight And Balance System'
[patent_app_type] => utility
[patent_app_number] => 11/560451
[patent_app_country] => US
[patent_app_date] => 2006-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0119/20080119967.pdf
[firstpage_image] =>[orig_patent_app_number] => 11560451
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/560451 | Onboard aircraft weight and balance system | Nov 15, 2006 | Issued |
Array
(
[id] => 6246787
[patent_doc_number] => 20100025536
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'Boom Force Absorber Systems and Methods for Aerial Refueling'
[patent_app_type] => utility
[patent_app_number] => 11/557892
[patent_app_country] => US
[patent_app_date] => 2006-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20100025536.pdf
[firstpage_image] =>[orig_patent_app_number] => 11557892
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/557892 | Boom force absorber systems and methods for aerial refueling | Nov 7, 2006 | Issued |
Array
(
[id] => 5196539
[patent_doc_number] => 20070295857
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-27
[patent_title] => 'Emergency Device'
[patent_app_type] => utility
[patent_app_number] => 11/557115
[patent_app_country] => US
[patent_app_date] => 2006-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1764
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0295/20070295857.pdf
[firstpage_image] =>[orig_patent_app_number] => 11557115
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/557115 | Emergency Device | Nov 6, 2006 | Abandoned |
Array
(
[id] => 165768
[patent_doc_number] => 07665692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-23
[patent_title] => 'Baggage bin door and baggage bin'
[patent_app_type] => utility
[patent_app_number] => 11/589193
[patent_app_country] => US
[patent_app_date] => 2006-10-30
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/665/07665692.pdf
[firstpage_image] =>[orig_patent_app_number] => 11589193
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/589193 | Baggage bin door and baggage bin | Oct 29, 2006 | Issued |
Array
(
[id] => 4633173
[patent_doc_number] => 08011618
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-06
[patent_title] => 'Storage device for baggage for an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 11/589248
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/011/08011618.pdf
[firstpage_image] =>[orig_patent_app_number] => 11589248
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/589248 | Storage device for baggage for an aircraft cabin | Oct 29, 2006 | Issued |
Array
(
[id] => 5091894
[patent_doc_number] => 20070113503
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-24
[patent_title] => 'Jet Blast Wall Structures'
[patent_app_type] => utility
[patent_app_number] => 11/551256
[patent_app_country] => US
[patent_app_date] => 2006-10-20
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0113/20070113503.pdf
[firstpage_image] =>[orig_patent_app_number] => 11551256
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/551256 | Jet blast wall structures | Oct 19, 2006 | Issued |
Array
(
[id] => 4890528
[patent_doc_number] => 20080099624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'Space tether transport system'
[patent_app_type] => utility
[patent_app_number] => 11/549956
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[pdf_file] => publications/A1/0099/20080099624.pdf
[firstpage_image] =>[orig_patent_app_number] => 11549956
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/549956 | Space tether transport system | Oct 15, 2006 | Abandoned |
Array
(
[id] => 4890529
[patent_doc_number] => 20080099625
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'First satellite sub-constellation and offset second satellite sub-constellation'
[patent_app_type] => utility
[patent_app_number] => 11/546720
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[pdf_file] => publications/A1/0099/20080099625.pdf
[firstpage_image] =>[orig_patent_app_number] => 11546720
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/546720 | First satellite sub-constellation and offset second satellite sub-constellation | Oct 11, 2006 | Abandoned |
Array
(
[id] => 4508988
[patent_doc_number] => 07931232
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-26
[patent_title] => 'Rigid framework for aircraft engine mounting structure and engine mounting structure comprising same'
[patent_app_type] => utility
[patent_app_number] => 12/067944
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/931/07931232.pdf
[firstpage_image] =>[orig_patent_app_number] => 12067944
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/067944 | Rigid framework for aircraft engine mounting structure and engine mounting structure comprising same | Oct 4, 2006 | Issued |