![](/images/general/no_picture/200_user.png)
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] => 6832584
[patent_doc_number] => 20030160129
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-28
[patent_title] => 'ROTATIONAL CANTED-JOINT MISSILE CONTROL SYSTEM'
[patent_app_type] => new
[patent_app_number] => 10/083518
[patent_app_country] => US
[patent_app_date] => 2002-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1399
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0160/20030160129.pdf
[firstpage_image] =>[orig_patent_app_number] => 10083518
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/083518 | Rotational canted-joint missile control system | Feb 24, 2002 | Issued |
Array
(
[id] => 6738098
[patent_doc_number] => 20030155466
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-21
[patent_title] => 'DOT (DEPARTMENT OF TRANSPORTATION) LAVATORY AND SHOWER COMBINATION'
[patent_app_type] => new
[patent_app_number] => 10/078859
[patent_app_country] => US
[patent_app_date] => 2002-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2582
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 46
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0155/20030155466.pdf
[firstpage_image] =>[orig_patent_app_number] => 10078859
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/078859 | Dot (department of transportation) lavatory and shower combination | Feb 19, 2002 | Issued |
Array
(
[id] => 1220615
[patent_doc_number] => 06698691
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-02
[patent_title] => 'Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same'
[patent_app_type] => B2
[patent_app_number] => 10/074053
[patent_app_country] => US
[patent_app_date] => 2002-02-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 9
[patent_no_of_words] => 4513
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/698/06698691.pdf
[firstpage_image] =>[orig_patent_app_number] => 10074053
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/074053 | Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same | Feb 13, 2002 | Issued |
Array
(
[id] => 1220594
[patent_doc_number] => 06698687
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-02
[patent_title] => 'Aircraft wing heat exchanger apparatus and method'
[patent_app_type] => B2
[patent_app_number] => 10/075063
[patent_app_country] => US
[patent_app_date] => 2002-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2191
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/698/06698687.pdf
[firstpage_image] =>[orig_patent_app_number] => 10075063
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/075063 | Aircraft wing heat exchanger apparatus and method | Feb 12, 2002 | Issued |
Array
(
[id] => 1224654
[patent_doc_number] => 06695263
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-02-24
[patent_title] => 'System for geosynchronous spacecraft rapid earth reacquisition'
[patent_app_type] => B1
[patent_app_number] => 10/073013
[patent_app_country] => US
[patent_app_date] => 2002-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3568
[patent_no_of_claims] => 56
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 61
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/695/06695263.pdf
[firstpage_image] =>[orig_patent_app_number] => 10073013
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/073013 | System for geosynchronous spacecraft rapid earth reacquisition | Feb 11, 2002 | Issued |
Array
(
[id] => 1257165
[patent_doc_number] => 06663045
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-16
[patent_title] => 'Method and apparatus for actuating an aircraft nose portion'
[patent_app_type] => B2
[patent_app_number] => 10/073496
[patent_app_country] => US
[patent_app_date] => 2002-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 4053
[patent_no_of_claims] => 82
[patent_no_of_ind_claims] => 15
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/663/06663045.pdf
[firstpage_image] =>[orig_patent_app_number] => 10073496
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/073496 | Method and apparatus for actuating an aircraft nose portion | Feb 10, 2002 | Issued |
Array
(
[id] => 6205238
[patent_doc_number] => 20020070313
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-06-13
[patent_title] => 'Liquid hydrogen stratospheric aircraft'
[patent_app_type] => new
[patent_app_number] => 10/073828
[patent_app_country] => US
[patent_app_date] => 2002-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 8305
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 37
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0070/20020070313.pdf
[firstpage_image] =>[orig_patent_app_number] => 10073828
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/073828 | Liquid hydrogen stratospheric aircraft | Feb 10, 2002 | Abandoned |
Array
(
[id] => 6520549
[patent_doc_number] => 20020109041
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-15
[patent_title] => 'Spiralling missile - A'
[patent_app_type] => new
[patent_app_number] => 10/067963
[patent_app_country] => US
[patent_app_date] => 2002-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 1424
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 218
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0109/20020109041.pdf
[firstpage_image] =>[orig_patent_app_number] => 10067963
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/067963 | Spiralling missileA | Feb 7, 2002 | Issued |
Array
(
[id] => 1514365
[patent_doc_number] => 06499693
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-31
[patent_title] => 'Aircraft to respond to threats'
[patent_app_type] => B1
[patent_app_number] => 09/683740
[patent_app_country] => US
[patent_app_date] => 2002-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4225
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/499/06499693.pdf
[firstpage_image] =>[orig_patent_app_number] => 09683740
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/683740 | Aircraft to respond to threats | Feb 7, 2002 | Issued |
Array
(
[id] => 1377785
[patent_doc_number] => 06536710
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-03-25
[patent_title] => 'Overhead lattice support structure'
[patent_app_type] => B1
[patent_app_number] => 10/071997
[patent_app_country] => US
[patent_app_date] => 2002-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2693
[patent_no_of_claims] => 39
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/536/06536710.pdf
[firstpage_image] =>[orig_patent_app_number] => 10071997
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/071997 | Overhead lattice support structure | Feb 5, 2002 | Issued |
Array
(
[id] => 1286593
[patent_doc_number] => 06629668
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-10-07
[patent_title] => 'Jump correcting projectile system'
[patent_app_type] => B1
[patent_app_number] => 10/062092
[patent_app_country] => US
[patent_app_date] => 2002-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2732
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/629/06629668.pdf
[firstpage_image] =>[orig_patent_app_number] => 10062092
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/062092 | Jump correcting projectile system | Feb 3, 2002 | Issued |
Array
(
[id] => 1274840
[patent_doc_number] => 06641083
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-11-04
[patent_title] => 'Balloon'
[patent_app_type] => B2
[patent_app_number] => 10/061274
[patent_app_country] => US
[patent_app_date] => 2002-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3680
[patent_no_of_claims] => 6
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/641/06641083.pdf
[firstpage_image] =>[orig_patent_app_number] => 10061274
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/061274 | Balloon | Feb 3, 2002 | Issued |
Array
(
[id] => 1245987
[patent_doc_number] => 06672541
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-06
[patent_title] => 'Flight crew rest and attendant rest environmental control system'
[patent_app_type] => B2
[patent_app_number] => 10/058819
[patent_app_country] => US
[patent_app_date] => 2002-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2478
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/672/06672541.pdf
[firstpage_image] =>[orig_patent_app_number] => 10058819
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/058819 | Flight crew rest and attendant rest environmental control system | Jan 27, 2002 | Issued |
Array
(
[id] => 1400778
[patent_doc_number] => 06513756
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-04
[patent_title] => 'Installation of single passenger interface unit and method thereof'
[patent_app_type] => B1
[patent_app_number] => 10/057289
[patent_app_country] => US
[patent_app_date] => 2002-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2355
[patent_no_of_claims] => 17
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[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/513/06513756.pdf
[firstpage_image] =>[orig_patent_app_number] => 10057289
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/057289 | Installation of single passenger interface unit and method thereof | Jan 24, 2002 | Issued |
Array
(
[id] => 5900754
[patent_doc_number] => 20020139894
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-10-03
[patent_title] => 'Roadable aircraft boat that flies in a wind of its own making'
[patent_app_type] => new
[patent_app_number] => 10/057194
[patent_app_country] => US
[patent_app_date] => 2002-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20020139894.pdf
[firstpage_image] =>[orig_patent_app_number] => 10057194
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/057194 | Roadable aircraft boat that flies in a wind of its own making | Jan 24, 2002 | Abandoned |
Array
(
[id] => 5981666
[patent_doc_number] => 20020096603
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-25
[patent_title] => 'Supporting structure for a solar sail of a satellite'
[patent_app_type] => new
[patent_app_number] => 10/053615
[patent_app_country] => US
[patent_app_date] => 2002-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3420
[patent_no_of_claims] => 14
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0096/20020096603.pdf
[firstpage_image] =>[orig_patent_app_number] => 10053615
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/053615 | Supporting structure for a solar sail of a satellite | Jan 23, 2002 | Issued |
10/057507 | Impulse drive for spaceships | Jan 21, 2002 | Abandoned |
Array
(
[id] => 5981657
[patent_doc_number] => 20020096599
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-25
[patent_title] => 'Hybrid winged airship (dynastat)'
[patent_app_type] => new
[patent_app_number] => 10/050934
[patent_app_country] => US
[patent_app_date] => 2002-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0096/20020096599.pdf
[firstpage_image] =>[orig_patent_app_number] => 10050934
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/050934 | Hybrid winged airship (dynastat) | Jan 21, 2002 | Issued |
Array
(
[id] => 1301112
[patent_doc_number] => 06612298
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-09-02
[patent_title] => 'Safety for sporting pellet or air guns'
[patent_app_type] => B2
[patent_app_number] => 10/041991
[patent_app_country] => US
[patent_app_date] => 2002-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/612/06612298.pdf
[firstpage_image] =>[orig_patent_app_number] => 10041991
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/041991 | Safety for sporting pellet or air guns | Jan 8, 2002 | Issued |
Array
(
[id] => 6269083
[patent_doc_number] => 20020104921
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-08
[patent_title] => 'Electrical remote-control and remote-power flying saucer'
[patent_app_type] => new
[patent_app_number] => 10/048091
[patent_app_country] => US
[patent_app_date] => 2001-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0104/20020104921.pdf
[firstpage_image] =>[orig_patent_app_number] => 10048091
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/048091 | Electrical remote-control and remote-power flying saucer | Dec 16, 2001 | Abandoned |