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] => 511039
[patent_doc_number] => 07188804
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-03-13
[patent_title] => 'Float retractable landing gear'
[patent_app_type] => utility
[patent_app_number] => 10/876042
[patent_app_country] => US
[patent_app_date] => 2004-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 16
[patent_no_of_words] => 5189
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 70
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/188/07188804.pdf
[firstpage_image] =>[orig_patent_app_number] => 10876042
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/876042 | Float retractable landing gear | Jun 24, 2004 | Issued |
Array
(
[id] => 495753
[patent_doc_number] => 07204460
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-17
[patent_title] => 'Orbital debris shield'
[patent_app_type] => utility
[patent_app_number] => 10/875710
[patent_app_country] => US
[patent_app_date] => 2004-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2240
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/204/07204460.pdf
[firstpage_image] =>[orig_patent_app_number] => 10875710
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/875710 | Orbital debris shield | Jun 23, 2004 | Issued |
Array
(
[id] => 7219673
[patent_doc_number] => 20050077431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-14
[patent_title] => 'Reinforcing material for parachutes and methods for reinforcing parachutes'
[patent_app_type] => utility
[patent_app_number] => 10/875980
[patent_app_country] => US
[patent_app_date] => 2004-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2445
[patent_no_of_claims] => 7
[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/A1/0077/20050077431.pdf
[firstpage_image] =>[orig_patent_app_number] => 10875980
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/875980 | Reinforcing material for parachutes and methods for reinforcing parachutes | Jun 22, 2004 | Issued |
Array
(
[id] => 7219672
[patent_doc_number] => 20050077430
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-14
[patent_title] => 'Construction materials and methods for parafoils and parachutes'
[patent_app_type] => utility
[patent_app_number] => 10/875653
[patent_app_country] => US
[patent_app_date] => 2004-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 3611
[patent_no_of_claims] => 19
[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/A1/0077/20050077430.pdf
[firstpage_image] =>[orig_patent_app_number] => 10875653
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/875653 | Construction materials and methods for parafoils and parachutes | Jun 22, 2004 | Abandoned |
Array
(
[id] => 6980933
[patent_doc_number] => 20050151001
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-14
[patent_title] => 'Compound helicopter'
[patent_app_type] => utility
[patent_app_number] => 10/871028
[patent_app_country] => US
[patent_app_date] => 2004-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 5501
[patent_no_of_claims] => 20
[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/A1/0151/20050151001.pdf
[firstpage_image] =>[orig_patent_app_number] => 10871028
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/871028 | Compound helicopter | Jun 20, 2004 | Abandoned |
Array
(
[id] => 6963665
[patent_doc_number] => 20050230562
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-20
[patent_title] => 'Payload fairing separation system'
[patent_app_type] => utility
[patent_app_number] => 10/868402
[patent_app_country] => US
[patent_app_date] => 2004-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4135
[patent_no_of_claims] => 24
[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/A1/0230/20050230562.pdf
[firstpage_image] =>[orig_patent_app_number] => 10868402
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/868402 | Payload fairing separation system | Jun 13, 2004 | Abandoned |
Array
(
[id] => 453911
[patent_doc_number] => 07243881
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-17
[patent_title] => 'Multi-function trailing edge devices and associated methods'
[patent_app_type] => utility
[patent_app_number] => 10/860438
[patent_app_country] => US
[patent_app_date] => 2004-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 29
[patent_no_of_words] => 6739
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 260
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/243/07243881.pdf
[firstpage_image] =>[orig_patent_app_number] => 10860438
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/860438 | Multi-function trailing edge devices and associated methods | Jun 2, 2004 | Issued |
Array
(
[id] => 7360044
[patent_doc_number] => 20040216727
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'Paintball guns'
[patent_app_type] => new
[patent_app_number] => 10/856193
[patent_app_country] => US
[patent_app_date] => 2004-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2969
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 3
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0216/20040216727.pdf
[firstpage_image] =>[orig_patent_app_number] => 10856193
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/856193 | Paintball guns | May 27, 2004 | Issued |
Array
(
[id] => 7086413
[patent_doc_number] => 20050006525
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-01-13
[patent_title] => 'Unmanned aerial vehicle for logistical delivery'
[patent_app_type] => utility
[patent_app_number] => 10/856360
[patent_app_country] => US
[patent_app_date] => 2004-05-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 29
[patent_no_of_words] => 10822
[patent_no_of_claims] => 25
[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/A1/0006/20050006525.pdf
[firstpage_image] =>[orig_patent_app_number] => 10856360
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/856360 | Unmanned aerial vehicle for logistical delivery | May 26, 2004 | Issued |
Array
(
[id] => 540916
[patent_doc_number] => 07159821
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-01-09
[patent_title] => 'Integrated transport system for overhead stowage'
[patent_app_type] => utility
[patent_app_number] => 10/709777
[patent_app_country] => US
[patent_app_date] => 2004-05-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 26
[patent_no_of_words] => 5269
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 421
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/159/07159821.pdf
[firstpage_image] =>[orig_patent_app_number] => 10709777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/709777 | Integrated transport system for overhead stowage | May 26, 2004 | Issued |
Array
(
[id] => 7205199
[patent_doc_number] => 20050258306
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-24
[patent_title] => 'Delta-winged hybrid airship'
[patent_app_type] => utility
[patent_app_number] => 10/853299
[patent_app_country] => US
[patent_app_date] => 2004-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6577
[patent_no_of_claims] => 41
[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/A1/0258/20050258306.pdf
[firstpage_image] =>[orig_patent_app_number] => 10853299
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/853299 | Delta-winged hybrid airship | May 23, 2004 | Issued |
Array
(
[id] => 622115
[patent_doc_number] => 07137592
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-11-21
[patent_title] => 'High-aspect ratio hybrid airship'
[patent_app_type] => utility
[patent_app_number] => 10/853300
[patent_app_country] => US
[patent_app_date] => 2004-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 6230
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/137/07137592.pdf
[firstpage_image] =>[orig_patent_app_number] => 10853300
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/853300 | High-aspect ratio hybrid airship | May 23, 2004 | Issued |
Array
(
[id] => 670540
[patent_doc_number] => 07090169
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-15
[patent_title] => 'Retaining clamp for alignment of risers when packing a parachute'
[patent_app_type] => utility
[patent_app_number] => 10/848858
[patent_app_country] => US
[patent_app_date] => 2004-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1893
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 257
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/090/07090169.pdf
[firstpage_image] =>[orig_patent_app_number] => 10848858
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/848858 | Retaining clamp for alignment of risers when packing a parachute | May 19, 2004 | Issued |
Array
(
[id] => 460235
[patent_doc_number] => 07237752
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-07-03
[patent_title] => 'System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping'
[patent_app_type] => utility
[patent_app_number] => 10/849268
[patent_app_country] => US
[patent_app_date] => 2004-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 19
[patent_no_of_words] => 8067
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/237/07237752.pdf
[firstpage_image] =>[orig_patent_app_number] => 10849268
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/849268 | System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping | May 17, 2004 | Issued |
10/709493 | AN AIRCRAFT USING ENGINE-POWERED, SWIPING ROTATING-BODIES TO FLY | May 9, 2004 | Abandoned |
Array
(
[id] => 7338018
[patent_doc_number] => 20040245395
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Aircraft ice protection system'
[patent_app_type] => new
[patent_app_number] => 10/842401
[patent_app_country] => US
[patent_app_date] => 2004-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1610
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 65
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245395.pdf
[firstpage_image] =>[orig_patent_app_number] => 10842401
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/842401 | Aircraft ice protection system | May 9, 2004 | Abandoned |
Array
(
[id] => 784013
[patent_doc_number] => 06988692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-01-24
[patent_title] => 'Rear fastening device for aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 10/838243
[patent_app_country] => US
[patent_app_date] => 2004-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2721
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/988/06988692.pdf
[firstpage_image] =>[orig_patent_app_number] => 10838243
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/838243 | Rear fastening device for aircraft engine | May 4, 2004 | Issued |
Array
(
[id] => 7132588
[patent_doc_number] => 20050178920
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Spacecraft propulsion system'
[patent_app_type] => utility
[patent_app_number] => 10/834681
[patent_app_country] => US
[patent_app_date] => 2004-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2636
[patent_no_of_claims] => 23
[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/A1/0178/20050178920.pdf
[firstpage_image] =>[orig_patent_app_number] => 10834681
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/834681 | Spacecraft propulsion system | Apr 28, 2004 | Abandoned |
Array
(
[id] => 741207
[patent_doc_number] => 07025304
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-04-11
[patent_title] => 'Helicopter messenger cable illumination'
[patent_app_type] => utility
[patent_app_number] => 10/834154
[patent_app_country] => US
[patent_app_date] => 2004-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 1319
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 159
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/025/07025304.pdf
[firstpage_image] =>[orig_patent_app_number] => 10834154
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/834154 | Helicopter messenger cable illumination | Apr 22, 2004 | Issued |
Array
(
[id] => 6936314
[patent_doc_number] => 20050109875
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-26
[patent_title] => 'VERTICAL TAKEOFF AND LANDING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 10/829757
[patent_app_country] => US
[patent_app_date] => 2004-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 8425
[patent_no_of_claims] => 35
[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/A1/0109/20050109875.pdf
[firstpage_image] =>[orig_patent_app_number] => 10829757
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/829757 | Vertical takeoff and landing aircraft | Apr 21, 2004 | Issued |