Ronald Baum
Examiner (ID: 15057, Phone: (571)272-3861 , Office: P/2439 )
Most Active Art Unit | 2439 |
Art Unit(s) | 2131, 2135, 2136, 2439, 2139 |
Total Applications | 545 |
Issued Applications | 358 |
Pending Applications | 59 |
Abandoned Applications | 128 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 7439829
[patent_doc_number] => 20040195443
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-07
[patent_title] => 'Self stowing thrust reverser'
[patent_app_type] => new
[patent_app_number] => 10/781410
[patent_app_country] => US
[patent_app_date] => 2004-02-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4648
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20040195443.pdf
[firstpage_image] =>[orig_patent_app_number] => 10781410
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/781410 | Self stowing thrust reverser | Feb 17, 2004 | Issued |
Array
(
[id] => 1102301
[patent_doc_number] => 06811123
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-02
[patent_title] => 'Store ejection system with integral isolation valve and associated ejection method'
[patent_app_type] => B1
[patent_app_number] => 10/780202
[patent_app_country] => US
[patent_app_date] => 2004-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5372
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/811/06811123.pdf
[firstpage_image] =>[orig_patent_app_number] => 10780202
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/780202 | Store ejection system with integral isolation valve and associated ejection method | Feb 16, 2004 | Issued |
Array
(
[id] => 1029585
[patent_doc_number] => 06877698
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-12
[patent_title] => 'Aircraft evacuation slide inflation system using a stored liquified gas capable of thermal decomposition'
[patent_app_type] => utility
[patent_app_number] => 10/778287
[patent_app_country] => US
[patent_app_date] => 2004-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2823
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/877/06877698.pdf
[firstpage_image] =>[orig_patent_app_number] => 10778287
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/778287 | Aircraft evacuation slide inflation system using a stored liquified gas capable of thermal decomposition | Feb 10, 2004 | Issued |
Array
(
[id] => 1055066
[patent_doc_number] => 06854689
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-02-15
[patent_title] => 'Methods and systems for operating aircraft landing gears'
[patent_app_type] => utility
[patent_app_number] => 10/774981
[patent_app_country] => US
[patent_app_date] => 2004-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4870
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/854/06854689.pdf
[firstpage_image] =>[orig_patent_app_number] => 10774981
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/774981 | Methods and systems for operating aircraft landing gears | Feb 8, 2004 | Issued |
Array
(
[id] => 6949539
[patent_doc_number] => 20050224633
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'LOW-DRAG ROTOR/WING FLAP'
[patent_app_type] => utility
[patent_app_number] => 10/770764
[patent_app_country] => US
[patent_app_date] => 2004-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3109
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224633.pdf
[firstpage_image] =>[orig_patent_app_number] => 10770764
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/770764 | Low-drag rotor/wing flap | Feb 2, 2004 | Issued |
Array
(
[id] => 771109
[patent_doc_number] => 07000872
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-02-21
[patent_title] => 'Circular parachute'
[patent_app_type] => utility
[patent_app_number] => 10/769151
[patent_app_country] => US
[patent_app_date] => 2004-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2898
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/000/07000872.pdf
[firstpage_image] =>[orig_patent_app_number] => 10769151
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/769151 | Circular parachute | Jan 29, 2004 | Issued |
Array
(
[id] => 667563
[patent_doc_number] => 07093798
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-22
[patent_title] => 'Transformable airplane'
[patent_app_type] => utility
[patent_app_number] => 10/769125
[patent_app_country] => US
[patent_app_date] => 2004-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 25
[patent_no_of_words] => 4986
[patent_no_of_claims] => 75
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/093/07093798.pdf
[firstpage_image] =>[orig_patent_app_number] => 10769125
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/769125 | Transformable airplane | Jan 29, 2004 | Issued |
Array
(
[id] => 7048307
[patent_doc_number] => 20050184194
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-25
[patent_title] => 'Hoist for aircraft cabin construction'
[patent_app_type] => utility
[patent_app_number] => 10/768935
[patent_app_country] => US
[patent_app_date] => 2004-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3226
[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/A1/0184/20050184194.pdf
[firstpage_image] =>[orig_patent_app_number] => 10768935
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/768935 | Hoist for aircraft cabin construction | Jan 29, 2004 | Issued |
Array
(
[id] => 1016663
[patent_doc_number] => 06889940
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-05-10
[patent_title] => 'Auxiliary fuel tank systems for aircraft and methods for their manufacture and use'
[patent_app_type] => utility
[patent_app_number] => 10/768269
[patent_app_country] => US
[patent_app_date] => 2004-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 16
[patent_no_of_words] => 8895
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/889/06889940.pdf
[firstpage_image] =>[orig_patent_app_number] => 10768269
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/768269 | Auxiliary fuel tank systems for aircraft and methods for their manufacture and use | Jan 28, 2004 | Issued |
Array
(
[id] => 7132513
[patent_doc_number] => 20050178880
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Auxiliary fuel tank systems for aircraft and methods for their manufacture and use'
[patent_app_type] => utility
[patent_app_number] => 10/768267
[patent_app_country] => US
[patent_app_date] => 2004-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 8954
[patent_no_of_claims] => 51
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0178/20050178880.pdf
[firstpage_image] =>[orig_patent_app_number] => 10768267
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/768267 | Auxiliary fuel tank systems for aircraft and methods for their manufacture and use | Jan 28, 2004 | Issued |
Array
(
[id] => 7132511
[patent_doc_number] => 20050178879
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'VTOL tailsitter flying wing'
[patent_app_type] => utility
[patent_app_number] => 10/757483
[patent_app_country] => US
[patent_app_date] => 2004-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2046
[patent_no_of_claims] => 4
[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/A1/0178/20050178879.pdf
[firstpage_image] =>[orig_patent_app_number] => 10757483
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/757483 | VTOL tailsitter flying wing | Jan 14, 2004 | Abandoned |
Array
(
[id] => 608303
[patent_doc_number] => 07150431
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-19
[patent_title] => 'Electrical generator fluid-flow-coolant filtration'
[patent_app_type] => utility
[patent_app_number] => 10/757880
[patent_app_country] => US
[patent_app_date] => 2004-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2012
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/150/07150431.pdf
[firstpage_image] =>[orig_patent_app_number] => 10757880
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/757880 | Electrical generator fluid-flow-coolant filtration | Jan 13, 2004 | Issued |
Array
(
[id] => 664494
[patent_doc_number] => 07097137
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-29
[patent_title] => 'Launch and recovery system for unmanned aerial vehicles'
[patent_app_type] => utility
[patent_app_number] => 10/754251
[patent_app_country] => US
[patent_app_date] => 2004-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 32
[patent_no_of_words] => 13643
[patent_no_of_claims] => 39
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 143
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/097/07097137.pdf
[firstpage_image] =>[orig_patent_app_number] => 10754251
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/754251 | Launch and recovery system for unmanned aerial vehicles | Jan 8, 2004 | Issued |
Array
(
[id] => 1013644
[patent_doc_number] => 06892983
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-17
[patent_title] => 'Anti-hijacking system'
[patent_app_type] => utility
[patent_app_number] => 10/753550
[patent_app_country] => US
[patent_app_date] => 2004-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 18
[patent_no_of_words] => 3105
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 64
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/892/06892983.pdf
[firstpage_image] =>[orig_patent_app_number] => 10753550
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/753550 | Anti-hijacking system | Jan 7, 2004 | Issued |
Array
(
[id] => 7337989
[patent_doc_number] => 20040245383
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Mounting arrangement for a gas turbine engine'
[patent_app_type] => new
[patent_app_number] => 10/751931
[patent_app_country] => US
[patent_app_date] => 2004-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4638
[patent_no_of_claims] => 10
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245383.pdf
[firstpage_image] =>[orig_patent_app_number] => 10751931
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/751931 | Mounting arrangement for a gas turbine engine | Jan 6, 2004 | Issued |
Array
(
[id] => 7132565
[patent_doc_number] => 20050178913
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Modification design for the improvement of slow flying aircraft\'s wing'
[patent_app_type] => utility
[patent_app_number] => 10/747513
[patent_app_country] => US
[patent_app_date] => 2003-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 944
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0178/20050178913.pdf
[firstpage_image] =>[orig_patent_app_number] => 10747513
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/747513 | Modification design for the improvement of slow flying aircraft's wing | Dec 29, 2003 | Abandoned |
Array
(
[id] => 1051840
[patent_doc_number] => 06857599
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-22
[patent_title] => 'Highly swept canard with low sweep wing supersonic aircraft configuration'
[patent_app_type] => utility
[patent_app_number] => 10/746744
[patent_app_country] => US
[patent_app_date] => 2003-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 754
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/857/06857599.pdf
[firstpage_image] =>[orig_patent_app_number] => 10746744
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/746744 | Highly swept canard with low sweep wing supersonic aircraft configuration | Dec 22, 2003 | Issued |
Array
(
[id] => 7058740
[patent_doc_number] => 20050001099
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Safety device for parachute canopy'
[patent_app_type] => utility
[patent_app_number] => 10/740924
[patent_app_country] => US
[patent_app_date] => 2003-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0001/20050001099.pdf
[firstpage_image] =>[orig_patent_app_number] => 10740924
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/740924 | Safety device for parachute canopy | Dec 21, 2003 | Issued |
Array
(
[id] => 1084607
[patent_doc_number] => 06830221
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-12-14
[patent_title] => 'Integrated glass ceramic spacecraft'
[patent_app_type] => B1
[patent_app_number] => 10/742058
[patent_app_country] => US
[patent_app_date] => 2003-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/830/06830221.pdf
[firstpage_image] =>[orig_patent_app_number] => 10742058
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/742058 | Integrated glass ceramic spacecraft | Dec 18, 2003 | Issued |
Array
(
[id] => 937745
[patent_doc_number] => 06971609
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-12-06
[patent_title] => 'Asymmetric passenger arrangement'
[patent_app_type] => utility
[patent_app_number] => 10/740952
[patent_app_country] => US
[patent_app_date] => 2003-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1531
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[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/971/06971609.pdf
[firstpage_image] =>[orig_patent_app_number] => 10740952
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/740952 | Asymmetric passenger arrangement | Dec 17, 2003 | Issued |