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] => 643446
[patent_doc_number] => 07118074
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-10-10
[patent_title] => 'Electrodynamic tether'
[patent_app_type] => utility
[patent_app_number] => 10/690161
[patent_app_country] => US
[patent_app_date] => 2003-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 4622
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/118/07118074.pdf
[firstpage_image] =>[orig_patent_app_number] => 10690161
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/690161 | Electrodynamic tether | Oct 16, 2003 | Issued |
Array
(
[id] => 7114230
[patent_doc_number] => 20050067530
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-31
[patent_title] => 'Cabin services system for a mobile platform'
[patent_app_type] => utility
[patent_app_number] => 10/670952
[patent_app_country] => US
[patent_app_date] => 2003-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3605
[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/A1/0067/20050067530.pdf
[firstpage_image] =>[orig_patent_app_number] => 10670952
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/670952 | Cabin services system for a mobile platform | Sep 24, 2003 | Abandoned |
Array
(
[id] => 1061423
[patent_doc_number] => 06848651
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-01
[patent_title] => 'Electro-hydraulic thrust reverser lock actuation system and method'
[patent_app_type] => utility
[patent_app_number] => 10/671373
[patent_app_country] => US
[patent_app_date] => 2003-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 4337
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/848/06848651.pdf
[firstpage_image] =>[orig_patent_app_number] => 10671373
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/671373 | Electro-hydraulic thrust reverser lock actuation system and method | Sep 23, 2003 | Issued |
Array
(
[id] => 7008205
[patent_doc_number] => 20050061921
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-24
[patent_title] => 'Aerodynamic tip protuberances for tip vortex intensity reduction'
[patent_app_type] => utility
[patent_app_number] => 10/666166
[patent_app_country] => US
[patent_app_date] => 2003-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1317
[patent_no_of_claims] => 25
[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/A1/0061/20050061921.pdf
[firstpage_image] =>[orig_patent_app_number] => 10666166
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/666166 | Aerodynamic tip protuberances for tip vortex intensity reduction | Sep 18, 2003 | Abandoned |
Array
(
[id] => 1116967
[patent_doc_number] => 06796531
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-09-28
[patent_title] => 'Canopy release locking bar'
[patent_app_type] => B1
[patent_app_number] => 10/665038
[patent_app_country] => US
[patent_app_date] => 2003-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 17
[patent_no_of_words] => 2090
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 27
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/796/06796531.pdf
[firstpage_image] =>[orig_patent_app_number] => 10665038
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/665038 | Canopy release locking bar | Sep 14, 2003 | Issued |
Array
(
[id] => 7113654
[patent_doc_number] => 20050066954
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-31
[patent_title] => 'Paintball gun barrel with compression chamber'
[patent_app_type] => utility
[patent_app_number] => 10/662800
[patent_app_country] => US
[patent_app_date] => 2003-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1484
[patent_no_of_claims] => 6
[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/A1/0066/20050066954.pdf
[firstpage_image] =>[orig_patent_app_number] => 10662800
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/662800 | Paintball gun barrel with compression chamber | Sep 11, 2003 | Abandoned |
Array
(
[id] => 977588
[patent_doc_number] => 06929222
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-16
[patent_title] => 'Non-jamming, fail safe flight control system with non-symmetric load alleviation capability'
[patent_app_type] => utility
[patent_app_number] => 10/657410
[patent_app_country] => US
[patent_app_date] => 2003-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 14
[patent_no_of_words] => 5953
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/929/06929222.pdf
[firstpage_image] =>[orig_patent_app_number] => 10657410
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/657410 | Non-jamming, fail safe flight control system with non-symmetric load alleviation capability | Sep 7, 2003 | Issued |
10/656951 | Complimentary retrograde/prograde satellite constellation | Sep 3, 2003 | Abandoned |
Array
(
[id] => 7080383
[patent_doc_number] => 20050045763
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'Aircraft lift device for low sonic boom'
[patent_app_type] => utility
[patent_app_number] => 10/651410
[patent_app_country] => US
[patent_app_date] => 2003-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 7505
[patent_no_of_claims] => 20
[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/A1/0045/20050045763.pdf
[firstpage_image] =>[orig_patent_app_number] => 10651410
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/651410 | Aircraft lift device for low sonic boom | Aug 28, 2003 | Issued |
Array
(
[id] => 7080391
[patent_doc_number] => 20050045771
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'Compact external launcher for small space payloads'
[patent_app_type] => utility
[patent_app_number] => 10/651226
[patent_app_country] => US
[patent_app_date] => 2003-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4996
[patent_no_of_claims] => 40
[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/A1/0045/20050045771.pdf
[firstpage_image] =>[orig_patent_app_number] => 10651226
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/651226 | Compact external launcher for small space payloads | Aug 27, 2003 | Issued |
Array
(
[id] => 1187751
[patent_doc_number] => 06732979
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-05-11
[patent_title] => 'Steer-by-wire tiller with position feel system'
[patent_app_type] => B1
[patent_app_number] => 10/652538
[patent_app_country] => US
[patent_app_date] => 2003-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 7246
[patent_no_of_claims] => 84
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/732/06732979.pdf
[firstpage_image] =>[orig_patent_app_number] => 10652538
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/652538 | Steer-by-wire tiller with position feel system | Aug 27, 2003 | Issued |
Array
(
[id] => 1090169
[patent_doc_number] => 06824097
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-30
[patent_title] => 'Vertical takeoff and landing aircraft'
[patent_app_type] => B1
[patent_app_number] => 10/649033
[patent_app_country] => US
[patent_app_date] => 2003-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 24
[patent_no_of_words] => 8506
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824097.pdf
[firstpage_image] =>[orig_patent_app_number] => 10649033
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/649033 | Vertical takeoff and landing aircraft | Aug 26, 2003 | Issued |
Array
(
[id] => 7058739
[patent_doc_number] => 20050001098
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-06
[patent_title] => 'Interior configuration for an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 10/477705
[patent_app_country] => US
[patent_app_date] => 2003-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4129
[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/A1/0001/20050001098.pdf
[firstpage_image] =>[orig_patent_app_number] => 10477705
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/477705 | Interior configuration for an aircraft cabin | Aug 20, 2003 | Issued |
Array
(
[id] => 1090174
[patent_doc_number] => 06824100
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-11-30
[patent_title] => 'Airplane landing gear'
[patent_app_type] => B1
[patent_app_number] => 10/641817
[patent_app_country] => US
[patent_app_date] => 2003-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2869
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/824/06824100.pdf
[firstpage_image] =>[orig_patent_app_number] => 10641817
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/641817 | Airplane landing gear | Aug 14, 2003 | Issued |
Array
(
[id] => 1072799
[patent_doc_number] => 06837461
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-01-04
[patent_title] => 'Balance load actuator'
[patent_app_type] => utility
[patent_app_number] => 10/638028
[patent_app_country] => US
[patent_app_date] => 2003-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3153
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/837/06837461.pdf
[firstpage_image] =>[orig_patent_app_number] => 10638028
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/638028 | Balance load actuator | Aug 7, 2003 | Issued |
Array
(
[id] => 1108417
[patent_doc_number] => 06805324
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-10-19
[patent_title] => 'Alternate methods of parachute construction'
[patent_app_type] => B2
[patent_app_number] => 10/631517
[patent_app_country] => US
[patent_app_date] => 2003-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/805/06805324.pdf
[firstpage_image] =>[orig_patent_app_number] => 10631517
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/631517 | Alternate methods of parachute construction | Jul 30, 2003 | Issued |
Array
(
[id] => 7337999
[patent_doc_number] => 20040245387
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'METHOD AND SYSTEM FOR CONTROLLING AN AIRCRAFT CONTROL SURFACE'
[patent_app_type] => new
[patent_app_number] => 10/631009
[patent_app_country] => US
[patent_app_date] => 2003-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4805
[patent_no_of_claims] => 17
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[patent_words_short_claim] => 143
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245387.pdf
[firstpage_image] =>[orig_patent_app_number] => 10631009
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/631009 | Method and system for controlling an aircraft control surface | Jul 30, 2003 | Issued |
Array
(
[id] => 1036012
[patent_doc_number] => 06871816
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-03-29
[patent_title] => 'Proactive optical trajectory following system'
[patent_app_type] => utility
[patent_app_number] => 10/633346
[patent_app_country] => US
[patent_app_date] => 2003-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/871/06871816.pdf
[firstpage_image] =>[orig_patent_app_number] => 10633346
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/633346 | Proactive optical trajectory following system | Jul 30, 2003 | Issued |
Array
(
[id] => 479095
[patent_doc_number] => 07219855
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-22
[patent_title] => 'Rising and moving apparatus and manufacturing method thereof'
[patent_app_type] => utility
[patent_app_number] => 10/618301
[patent_app_country] => US
[patent_app_date] => 2003-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 49
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/219/07219855.pdf
[firstpage_image] =>[orig_patent_app_number] => 10618301
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/618301 | Rising and moving apparatus and manufacturing method thereof | Jul 10, 2003 | Issued |
Array
(
[id] => 1051832
[patent_doc_number] => 06857596
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-02-22
[patent_title] => 'High speed electro-optic payout system incorporating a stationary optical terminus'
[patent_app_type] => utility
[patent_app_number] => 10/617545
[patent_app_country] => US
[patent_app_date] => 2003-07-10
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/857/06857596.pdf
[firstpage_image] =>[orig_patent_app_number] => 10617545
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/617545 | High speed electro-optic payout system incorporating a stationary optical terminus | Jul 9, 2003 | Issued |