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] => 1087167
[patent_doc_number] => 06827313
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-12-07
[patent_title] => 'Multi-crew modules for space flight'
[patent_app_type] => B1
[patent_app_number] => 10/738675
[patent_app_country] => US
[patent_app_date] => 2003-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 18
[patent_no_of_words] => 4429
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/827/06827313.pdf
[firstpage_image] =>[orig_patent_app_number] => 10738675
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/738675 | Multi-crew modules for space flight | Dec 15, 2003 | Issued |
Array
(
[id] => 6949548
[patent_doc_number] => 20050224642
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Landing gear method and apparatus for braking and maneuvering'
[patent_app_type] => utility
[patent_app_number] => 10/734216
[patent_app_country] => US
[patent_app_date] => 2003-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4698
[patent_no_of_claims] => 22
[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/A1/0224/20050224642.pdf
[firstpage_image] =>[orig_patent_app_number] => 10734216
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/734216 | Landing gear method and apparatus for braking and maneuvering | Dec 14, 2003 | Issued |
Array
(
[id] => 7219681
[patent_doc_number] => 20050077435
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-14
[patent_title] => 'PROFILED WING UNIT OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 10/733550
[patent_app_country] => US
[patent_app_date] => 2003-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3465
[patent_no_of_claims] => 23
[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/A1/0077/20050077435.pdf
[firstpage_image] =>[orig_patent_app_number] => 10733550
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/733550 | Profiled wing unit of an aircraft | Dec 9, 2003 | Issued |
Array
(
[id] => 7338010
[patent_doc_number] => 20040245393
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Bendable wing for micro air vehicle'
[patent_app_type] => new
[patent_app_number] => 10/731777
[patent_app_country] => US
[patent_app_date] => 2003-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2938
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245393.pdf
[firstpage_image] =>[orig_patent_app_number] => 10731777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/731777 | Bendable wing for micro air vehicle | Dec 8, 2003 | Abandoned |
Array
(
[id] => 7301002
[patent_doc_number] => 20040113017
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-06-17
[patent_title] => 'Control device and method for emergency opening of an aircraft evacuation door'
[patent_app_type] => new
[patent_app_number] => 10/728050
[patent_app_country] => US
[patent_app_date] => 2003-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3864
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0113/20040113017.pdf
[firstpage_image] =>[orig_patent_app_number] => 10728050
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/728050 | Control device and method for emergency opening of an aircraft evacuation door | Dec 2, 2003 | Issued |
Array
(
[id] => 514300
[patent_doc_number] => 07185858
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-03-06
[patent_title] => 'Spacecraft gyro calibration system'
[patent_app_type] => utility
[patent_app_number] => 10/723782
[patent_app_country] => US
[patent_app_date] => 2003-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 5881
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/185/07185858.pdf
[firstpage_image] =>[orig_patent_app_number] => 10723782
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/723782 | Spacecraft gyro calibration system | Nov 25, 2003 | Issued |
Array
(
[id] => 5019218
[patent_doc_number] => 20070145183
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-28
[patent_title] => 'A DEVICE FOR ASSISTING AN AIRPLANE IN INTERCEPTING A SEGMENT OF A FLIGHT PATH UTILIZING POSITIONAL AND GROUND SPEED INDICATORS'
[patent_app_type] => utility
[patent_app_number] => 10/723064
[patent_app_country] => US
[patent_app_date] => 2003-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5471
[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/A1/0145/20070145183.pdf
[firstpage_image] =>[orig_patent_app_number] => 10723064
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/723064 | Device for assisting an airplane in intercepting a segment of a flight path utilizing positional and ground speed indicators | Nov 25, 2003 | Issued |
Array
(
[id] => 7094465
[patent_doc_number] => 20050127242
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-16
[patent_title] => 'Payload dispensing system particularly suited for unmanned aerial vehicles'
[patent_app_type] => utility
[patent_app_number] => 10/729578
[patent_app_country] => US
[patent_app_date] => 2003-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3444
[patent_no_of_claims] => 30
[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/A1/0127/20050127242.pdf
[firstpage_image] =>[orig_patent_app_number] => 10729578
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/729578 | Payload dispensing system particularly suited for unmanned aerial vehicles | Nov 24, 2003 | Abandoned |
Array
(
[id] => 1113754
[patent_doc_number] => 06799739
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-10-05
[patent_title] => 'Aircraft control surface drive system and associated methods'
[patent_app_type] => B1
[patent_app_number] => 10/720786
[patent_app_country] => US
[patent_app_date] => 2003-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5397
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 281
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/799/06799739.pdf
[firstpage_image] =>[orig_patent_app_number] => 10720786
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/720786 | Aircraft control surface drive system and associated methods | Nov 23, 2003 | Issued |
Array
(
[id] => 673524
[patent_doc_number] => 07086393
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-08-08
[patent_title] => 'Hybrid airgun'
[patent_app_type] => utility
[patent_app_number] => 10/722173
[patent_app_country] => US
[patent_app_date] => 2003-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 5400
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/086/07086393.pdf
[firstpage_image] =>[orig_patent_app_number] => 10722173
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/722173 | Hybrid airgun | Nov 23, 2003 | Issued |
Array
(
[id] => 1048607
[patent_doc_number] => 06860451
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-03-01
[patent_title] => 'Spacecraft spin axis reorientation method'
[patent_app_type] => utility
[patent_app_number] => 10/719329
[patent_app_country] => US
[patent_app_date] => 2003-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 14
[patent_no_of_words] => 4780
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/860/06860451.pdf
[firstpage_image] =>[orig_patent_app_number] => 10719329
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/719329 | Spacecraft spin axis reorientation method | Nov 20, 2003 | Issued |
Array
(
[id] => 1159837
[patent_doc_number] => 06752353
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-06-22
[patent_title] => 'Optimal control design for aircraft antiskid brake control systems'
[patent_app_type] => B2
[patent_app_number] => 10/716696
[patent_app_country] => US
[patent_app_date] => 2003-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3669
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/752/06752353.pdf
[firstpage_image] =>[orig_patent_app_number] => 10716696
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/716696 | Optimal control design for aircraft antiskid brake control systems | Nov 17, 2003 | Issued |
Array
(
[id] => 7143808
[patent_doc_number] => 20040169110
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-09-02
[patent_title] => 'Aerodynamic component for controlling a landing guide path of an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/713161
[patent_app_country] => US
[patent_app_date] => 2003-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3254
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 42
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0169/20040169110.pdf
[firstpage_image] =>[orig_patent_app_number] => 10713161
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/713161 | Aerodynamic component for controlling a landing guide path of an aircraft | Nov 16, 2003 | Issued |
Array
(
[id] => 7304739
[patent_doc_number] => 20040140398
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-22
[patent_title] => 'Baggage compartment including a guide connecting a support structure and a bin'
[patent_app_type] => new
[patent_app_number] => 10/712036
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4389
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0140/20040140398.pdf
[firstpage_image] =>[orig_patent_app_number] => 10712036
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/712036 | Baggage compartment including a guide connecting a support structure and a bin | Nov 13, 2003 | Issued |
Array
(
[id] => 7450219
[patent_doc_number] => 20040099769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-27
[patent_title] => 'Gliding vehicle guidance'
[patent_app_type] => new
[patent_app_number] => 10/716977
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2952
[patent_no_of_claims] => 13
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[patent_words_short_claim] => 113
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0099/20040099769.pdf
[firstpage_image] =>[orig_patent_app_number] => 10716977
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/716977 | Gliding vehicle guidance | Nov 13, 2003 | Issued |
Array
(
[id] => 7139786
[patent_doc_number] => 20050116107
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Area ruling for vertical stabilizers'
[patent_app_type] => utility
[patent_app_number] => 10/706670
[patent_app_country] => US
[patent_app_date] => 2003-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5410
[patent_no_of_claims] => 46
[patent_no_of_ind_claims] => 28
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20050116107.pdf
[firstpage_image] =>[orig_patent_app_number] => 10706670
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/706670 | Area ruling for vertical stabilizers | Nov 10, 2003 | Abandoned |
Array
(
[id] => 716874
[patent_doc_number] => 07048227
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-05-23
[patent_title] => 'Parachute supported aircraft with controlled wing collapse and inflation'
[patent_app_type] => utility
[patent_app_number] => 10/705682
[patent_app_country] => US
[patent_app_date] => 2003-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 14
[patent_no_of_words] => 8117
[patent_no_of_claims] => 28
[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] => patents/07/048/07048227.pdf
[firstpage_image] =>[orig_patent_app_number] => 10705682
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/705682 | Parachute supported aircraft with controlled wing collapse and inflation | Nov 9, 2003 | Issued |
Array
(
[id] => 1096385
[patent_doc_number] => 06817577
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-16
[patent_title] => 'Airplane door lock system'
[patent_app_type] => B2
[patent_app_number] => 10/691386
[patent_app_country] => US
[patent_app_date] => 2003-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_words_short_claim] => 94
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/817/06817577.pdf
[firstpage_image] =>[orig_patent_app_number] => 10691386
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/691386 | Airplane door lock system | Oct 21, 2003 | Issued |
Array
(
[id] => 1019515
[patent_doc_number] => 06886779
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'Impact-absorbing, load-limiting connection device and rotary wing aircraft having such a connection device'
[patent_app_type] => utility
[patent_app_number] => 10/691005
[patent_app_country] => US
[patent_app_date] => 2003-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_claims] => 20
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[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886779.pdf
[firstpage_image] =>[orig_patent_app_number] => 10691005
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/691005 | Impact-absorbing, load-limiting connection device and rotary wing aircraft having such a connection device | Oct 21, 2003 | Issued |
Array
(
[id] => 1042303
[patent_doc_number] => 06866232
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-03-15
[patent_title] => 'Automated docking of space vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/687988
[patent_app_country] => US
[patent_app_date] => 2003-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 8740
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/866/06866232.pdf
[firstpage_image] =>[orig_patent_app_number] => 10687988
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/687988 | Automated docking of space vehicle | Oct 16, 2003 | Issued |