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] => 6955454
[patent_doc_number] => 20050211824
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-29
[patent_title] => 'Turbine engine arrangements'
[patent_app_type] => utility
[patent_app_number] => 11/036360
[patent_app_country] => US
[patent_app_date] => 2005-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2504
[patent_no_of_claims] => 8
[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/A1/0211/20050211824.pdf
[firstpage_image] =>[orig_patent_app_number] => 11036360
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/036360 | Turbine engine arrangements | Jan 17, 2005 | Issued |
Array
(
[id] => 5691521
[patent_doc_number] => 20060151666
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-13
[patent_title] => 'Vertical take-off and landing (VTOL) aircraft with distributed thrust and control'
[patent_app_type] => utility
[patent_app_number] => 11/035263
[patent_app_country] => US
[patent_app_date] => 2005-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 8220
[patent_no_of_claims] => 52
[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/A1/0151/20060151666.pdf
[firstpage_image] =>[orig_patent_app_number] => 11035263
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/035263 | Vertical take-off and landing (VTOL) aircraft with distributed thrust and control | Jan 12, 2005 | Issued |
Array
(
[id] => 5892410
[patent_doc_number] => 20060000947
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-01-05
[patent_title] => 'Passenger sitting/sleeping arrangement'
[patent_app_type] => utility
[patent_app_number] => 11/026251
[patent_app_country] => US
[patent_app_date] => 2004-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3074
[patent_no_of_claims] => 18
[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/A1/0000/20060000947.pdf
[firstpage_image] =>[orig_patent_app_number] => 11026251
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/026251 | Passenger sitting/sleeping arrangement | Dec 29, 2004 | Issued |
Array
(
[id] => 6980960
[patent_doc_number] => 20050151028
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-14
[patent_title] => 'Apparatus for driving and adjusting flaps hinged to an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/021723
[patent_app_country] => US
[patent_app_date] => 2004-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2224
[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/A1/0151/20050151028.pdf
[firstpage_image] =>[orig_patent_app_number] => 11021723
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/021723 | Apparatus for driving and adjusting flaps hinged to an aircraft | Dec 21, 2004 | Issued |
Array
(
[id] => 6993886
[patent_doc_number] => 20050133662
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-23
[patent_title] => 'Convertible aircraft provided with two tilt fans on either side of the fuselage and with a third tilt fan arranged on the tail of the aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/016763
[patent_app_country] => US
[patent_app_date] => 2004-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2680
[patent_no_of_claims] => 19
[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/A1/0133/20050133662.pdf
[firstpage_image] =>[orig_patent_app_number] => 11016763
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/016763 | Convertible aircraft provided with two tilt fans on either side of the fuselage and with a third tilt fan arranged on the tail of the aircraft | Dec 20, 2004 | Abandoned |
Array
(
[id] => 5817771
[patent_doc_number] => 20060022084
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-02-02
[patent_title] => 'Convertible aircraft provided with two tilt fans on either side of the fuselage, and with a non-tilting fan inserted in the fuselage'
[patent_app_type] => utility
[patent_app_number] => 11/016902
[patent_app_country] => US
[patent_app_date] => 2004-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2854
[patent_no_of_claims] => 22
[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/A1/0022/20060022084.pdf
[firstpage_image] =>[orig_patent_app_number] => 11016902
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/016902 | Convertible aircraft provided with two tilt fans on either side of the fuselage, and with a non-tilting fan inserted in the fuselage | Dec 20, 2004 | Issued |
Array
(
[id] => 443851
[patent_doc_number] => 07252269
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-08-07
[patent_title] => 'Asymmetrical low-profile bulkhead'
[patent_app_type] => utility
[patent_app_number] => 11/017421
[patent_app_country] => US
[patent_app_date] => 2004-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 21
[patent_no_of_words] => 4201
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/252/07252269.pdf
[firstpage_image] =>[orig_patent_app_number] => 11017421
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/017421 | Asymmetrical low-profile bulkhead | Dec 19, 2004 | Issued |
Array
(
[id] => 6955459
[patent_doc_number] => 20050211829
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-29
[patent_title] => 'Magnetic Motive System'
[patent_app_type] => utility
[patent_app_number] => 10/905125
[patent_app_country] => US
[patent_app_date] => 2004-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4818
[patent_no_of_claims] => 39
[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/A1/0211/20050211829.pdf
[firstpage_image] =>[orig_patent_app_number] => 10905125
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/905125 | Magnetic Motive System | Dec 15, 2004 | Abandoned |
Array
(
[id] => 472577
[patent_doc_number] => 07226018
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-06-05
[patent_title] => 'Landing gear method and apparatus for braking and maneuvering'
[patent_app_type] => utility
[patent_app_number] => 11/011756
[patent_app_country] => US
[patent_app_date] => 2004-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 7283
[patent_no_of_claims] => 52
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/226/07226018.pdf
[firstpage_image] =>[orig_patent_app_number] => 11011756
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/011756 | Landing gear method and apparatus for braking and maneuvering | Dec 14, 2004 | Issued |
Array
(
[id] => 463703
[patent_doc_number] => 07234667
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-06-26
[patent_title] => 'Modular aerospace plane'
[patent_app_type] => utility
[patent_app_number] => 11/007855
[patent_app_country] => US
[patent_app_date] => 2004-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 4811
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/234/07234667.pdf
[firstpage_image] =>[orig_patent_app_number] => 11007855
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/007855 | Modular aerospace plane | Dec 8, 2004 | Issued |
Array
(
[id] => 5703004
[patent_doc_number] => 20060192051
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-31
[patent_title] => 'Reconfigurable interior sidewall'
[patent_app_type] => utility
[patent_app_number] => 11/004292
[patent_app_country] => US
[patent_app_date] => 2004-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4740
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0192/20060192051.pdf
[firstpage_image] =>[orig_patent_app_number] => 11004292
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/004292 | Reconfigurable interior sidewall | Dec 2, 2004 | Issued |
Array
(
[id] => 653568
[patent_doc_number] => 07108229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-19
[patent_title] => 'Arrangement and method for the generation of water on board an aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/999052
[patent_app_country] => US
[patent_app_date] => 2004-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3120
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/108/07108229.pdf
[firstpage_image] =>[orig_patent_app_number] => 10999052
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/999052 | Arrangement and method for the generation of water on board an aircraft | Nov 28, 2004 | Issued |
Array
(
[id] => 427640
[patent_doc_number] => 07267303
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-09-11
[patent_title] => 'Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy'
[patent_app_type] => utility
[patent_app_number] => 10/990393
[patent_app_country] => US
[patent_app_date] => 2004-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 20
[patent_no_of_words] => 8782
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/267/07267303.pdf
[firstpage_image] =>[orig_patent_app_number] => 10990393
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/990393 | Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy | Nov 17, 2004 | Issued |
Array
(
[id] => 5773678
[patent_doc_number] => 20060102791
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-18
[patent_title] => 'Interoperable aerial refueling apparatus and methods'
[patent_app_type] => utility
[patent_app_number] => 10/992153
[patent_app_country] => US
[patent_app_date] => 2004-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2994
[patent_no_of_claims] => 44
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0102/20060102791.pdf
[firstpage_image] =>[orig_patent_app_number] => 10992153
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/992153 | Interoperable aerial refueling apparatus and methods | Nov 17, 2004 | Issued |
Array
(
[id] => 7139769
[patent_doc_number] => 20050116093
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Mounting structure for mounting a turboprop under an aircraft wing'
[patent_app_type] => utility
[patent_app_number] => 10/987151
[patent_app_country] => US
[patent_app_date] => 2004-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6248
[patent_no_of_claims] => 11
[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/A1/0116/20050116093.pdf
[firstpage_image] =>[orig_patent_app_number] => 10987151
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/987151 | Mounting structure for mounting a turboprop under an aircraft wing | Nov 14, 2004 | Issued |
Array
(
[id] => 5908584
[patent_doc_number] => 20060124801
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-15
[patent_title] => 'Shape changing structure'
[patent_app_type] => utility
[patent_app_number] => 10/988292
[patent_app_country] => US
[patent_app_date] => 2004-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5245
[patent_no_of_claims] => 29
[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/A1/0124/20060124801.pdf
[firstpage_image] =>[orig_patent_app_number] => 10988292
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/988292 | Shape changing structure | Nov 11, 2004 | Issued |
Array
(
[id] => 417674
[patent_doc_number] => 07275722
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-10-02
[patent_title] => 'Wing tip device'
[patent_app_type] => utility
[patent_app_number] => 10/986451
[patent_app_country] => US
[patent_app_date] => 2004-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 6590
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 219
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/275/07275722.pdf
[firstpage_image] =>[orig_patent_app_number] => 10986451
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/986451 | Wing tip device | Nov 9, 2004 | Issued |
Array
(
[id] => 440937
[patent_doc_number] => 07255305
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-14
[patent_title] => 'Flying device utilizing natural principles'
[patent_app_type] => utility
[patent_app_number] => 10/979046
[patent_app_country] => US
[patent_app_date] => 2004-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 27
[patent_no_of_words] => 10857
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 235
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/255/07255305.pdf
[firstpage_image] =>[orig_patent_app_number] => 10979046
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/979046 | Flying device utilizing natural principles | Nov 1, 2004 | Issued |
Array
(
[id] => 5804906
[patent_doc_number] => 20060091258
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-04
[patent_title] => 'Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV)'
[patent_app_type] => utility
[patent_app_number] => 10/976153
[patent_app_country] => US
[patent_app_date] => 2004-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 7561
[patent_no_of_claims] => 29
[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/A1/0091/20060091258.pdf
[firstpage_image] =>[orig_patent_app_number] => 10976153
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/976153 | Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV) | Oct 28, 2004 | Issued |
Array
(
[id] => 466358
[patent_doc_number] => 07232096
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-06-19
[patent_title] => 'Positive lock seat device'
[patent_app_type] => utility
[patent_app_number] => 10/973829
[patent_app_country] => US
[patent_app_date] => 2004-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1814
[patent_no_of_claims] => 44
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/232/07232096.pdf
[firstpage_image] =>[orig_patent_app_number] => 10973829
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/973829 | Positive lock seat device | Oct 25, 2004 | Issued |