Steph Calogero
Examiner (ID: 7642)
Most Active Art Unit | 2509 |
Art Unit(s) | 2509 |
Total Applications | 104 |
Issued Applications | 82 |
Pending Applications | 1 |
Abandoned Applications | 21 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 1070696
[patent_doc_number] => 06840478
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-01-11
[patent_title] => 'Aircraft internal wing and design'
[patent_app_type] => utility
[patent_app_number] => 10/046957
[patent_app_country] => US
[patent_app_date] => 2002-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 15
[patent_no_of_words] => 4006
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 228
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/840/06840478.pdf
[firstpage_image] =>[orig_patent_app_number] => 10046957
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/046957 | Aircraft internal wing and design | Jan 13, 2002 | Issued |
Array
(
[id] => 957758
[patent_doc_number] => 06952995
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-10-11
[patent_title] => 'Apparatus and method for passive venting of rocket motor or ordnance case'
[patent_app_type] => utility
[patent_app_number] => 10/042391
[patent_app_country] => US
[patent_app_date] => 2002-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1487
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/952/06952995.pdf
[firstpage_image] =>[orig_patent_app_number] => 10042391
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/042391 | Apparatus and method for passive venting of rocket motor or ordnance case | Jan 10, 2002 | Issued |
Array
(
[id] => 6854063
[patent_doc_number] => 20030127564
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-10
[patent_title] => 'AERODYNAMIC CONTROL FOR SEPARATION OF UNSTABLE BODIES'
[patent_app_type] => new
[patent_app_number] => 10/041042
[patent_app_country] => US
[patent_app_date] => 2002-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1060
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0127/20030127564.pdf
[firstpage_image] =>[orig_patent_app_number] => 10041042
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/041042 | Aerodynamic control for separation of unstable bodies | Jan 8, 2002 | Issued |
Array
(
[id] => 6758677
[patent_doc_number] => 20030122038
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-03
[patent_title] => 'Method of lift control of aircraft and system therefor'
[patent_app_type] => new
[patent_app_number] => 10/026881
[patent_app_country] => US
[patent_app_date] => 2001-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7539
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 32
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20030122038.pdf
[firstpage_image] =>[orig_patent_app_number] => 10026881
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/026881 | Method of lift control of aircraft and system therefor | Dec 26, 2001 | Issued |
Array
(
[id] => 1271360
[patent_doc_number] => 06644596
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-11-11
[patent_title] => 'Deployment system for inflatable structures'
[patent_app_type] => B1
[patent_app_number] => 10/023749
[patent_app_country] => US
[patent_app_date] => 2001-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3228
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/644/06644596.pdf
[firstpage_image] =>[orig_patent_app_number] => 10023749
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/023749 | Deployment system for inflatable structures | Dec 20, 2001 | Issued |
Array
(
[id] => 6680188
[patent_doc_number] => 20030116052
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-26
[patent_title] => 'Electrically actuatable initiator with output charge'
[patent_app_type] => new
[patent_app_number] => 10/036905
[patent_app_country] => US
[patent_app_date] => 2001-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5336
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20030116052.pdf
[firstpage_image] =>[orig_patent_app_number] => 10036905
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/036905 | Electrically actuatable initiator with output charge | Dec 20, 2001 | Issued |
Array
(
[id] => 6680816
[patent_doc_number] => 20030116680
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-26
[patent_title] => 'Payload transfer and release system'
[patent_app_type] => new
[patent_app_number] => 10/023981
[patent_app_country] => US
[patent_app_date] => 2001-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2910
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20030116680.pdf
[firstpage_image] =>[orig_patent_app_number] => 10023981
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/023981 | Payload transfer and release system | Dec 20, 2001 | Abandoned |
Array
(
[id] => 6300041
[patent_doc_number] => 20020092952
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-18
[patent_title] => 'Parachutes'
[patent_app_type] => new
[patent_app_number] => 10/013834
[patent_app_country] => US
[patent_app_date] => 2001-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1177
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0092/20020092952.pdf
[firstpage_image] =>[orig_patent_app_number] => 10013834
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/013834 | Parachutes | Dec 12, 2001 | Abandoned |
Array
(
[id] => 5917709
[patent_doc_number] => 20020113165
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-22
[patent_title] => 'Aircraft and control system'
[patent_app_type] => new
[patent_app_number] => 10/017908
[patent_app_country] => US
[patent_app_date] => 2001-12-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 8852
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0113/20020113165.pdf
[firstpage_image] =>[orig_patent_app_number] => 10017908
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/017908 | Aircraft and control system | Dec 12, 2001 | Abandoned |
Array
(
[id] => 1190638
[patent_doc_number] => 06729577
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-05-04
[patent_title] => 'Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom'
[patent_app_type] => B2
[patent_app_number] => 10/006505
[patent_app_country] => US
[patent_app_date] => 2001-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 69
[patent_no_of_words] => 13908
[patent_no_of_claims] => 47
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 29
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/729/06729577.pdf
[firstpage_image] =>[orig_patent_app_number] => 10006505
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/006505 | Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom | Dec 5, 2001 | Issued |
Array
(
[id] => 1347836
[patent_doc_number] => 06564716
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-05-20
[patent_title] => 'Fuzes having centrifugal arming lock for a munition'
[patent_app_type] => B1
[patent_app_number] => 10/006739
[patent_app_country] => US
[patent_app_date] => 2001-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 12
[patent_no_of_words] => 2719
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 137
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/564/06564716.pdf
[firstpage_image] =>[orig_patent_app_number] => 10006739
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/006739 | Fuzes having centrifugal arming lock for a munition | Dec 4, 2001 | Issued |
Array
(
[id] => 1372509
[patent_doc_number] => 06536351
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-03-25
[patent_title] => 'Warhead'
[patent_app_type] => B2
[patent_app_number] => 09/989755
[patent_app_country] => US
[patent_app_date] => 2001-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1223
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/536/06536351.pdf
[firstpage_image] =>[orig_patent_app_number] => 09989755
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/989755 | Warhead | Nov 20, 2001 | Issued |
Array
(
[id] => 995495
[patent_doc_number] => 06913225
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-07-05
[patent_title] => 'Construction and method of use in a carrier rocket or satellite'
[patent_app_type] => utility
[patent_app_number] => 10/432763
[patent_app_country] => US
[patent_app_date] => 2001-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 4361
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/913/06913225.pdf
[firstpage_image] =>[orig_patent_app_number] => 10432763
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/432763 | Construction and method of use in a carrier rocket or satellite | Nov 13, 2001 | Issued |
Array
(
[id] => 5869710
[patent_doc_number] => 20020046673
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-04-25
[patent_title] => 'Pyrotechnic initiation delay means'
[patent_app_type] => new
[patent_app_number] => 09/986780
[patent_app_country] => US
[patent_app_date] => 2001-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2811
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0046/20020046673.pdf
[firstpage_image] =>[orig_patent_app_number] => 09986780
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/986780 | Pyrotechnic initiation delay means | Nov 8, 2001 | Issued |
Array
(
[id] => 6819504
[patent_doc_number] => 20030217664
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-11-27
[patent_title] => 'Priming device for the explosive charge of a submunition'
[patent_app_type] => new
[patent_app_number] => 10/415531
[patent_app_country] => US
[patent_app_date] => 2003-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3078
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0217/20030217664.pdf
[firstpage_image] =>[orig_patent_app_number] => 10415531
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/415531 | Priming device for the explosive charge of a sub-munition | Nov 5, 2001 | Issued |
Array
(
[id] => 1132361
[patent_doc_number] => 06779460
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-24
[patent_title] => 'Support vessel for self-burying mines'
[patent_app_type] => B2
[patent_app_number] => 10/001502
[patent_app_country] => US
[patent_app_date] => 2001-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1199
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/779/06779460.pdf
[firstpage_image] =>[orig_patent_app_number] => 10001502
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/001502 | Support vessel for self-burying mines | Oct 31, 2001 | Issued |
Array
(
[id] => 1501969
[patent_doc_number] => 06439119
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-27
[patent_title] => 'Lockable electro-optical high voltage apparatus and method for slapper detonators'
[patent_app_type] => B1
[patent_app_number] => 09/985957
[patent_app_country] => US
[patent_app_date] => 2001-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2966
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/439/06439119.pdf
[firstpage_image] =>[orig_patent_app_number] => 09985957
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/985957 | Lockable electro-optical high voltage apparatus and method for slapper detonators | Oct 29, 2001 | Issued |
Array
(
[id] => 1323736
[patent_doc_number] => 06591733
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-07-15
[patent_title] => 'Loading system'
[patent_app_type] => B1
[patent_app_number] => 09/889690
[patent_app_country] => US
[patent_app_date] => 2001-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 3056
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 165
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/591/06591733.pdf
[firstpage_image] =>[orig_patent_app_number] => 09889690
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/889690 | Loading system | Oct 15, 2001 | Issued |
Array
(
[id] => 6121353
[patent_doc_number] => 20020073869
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-06-20
[patent_title] => 'Ultra sensitive magnetic field sensors'
[patent_app_type] => new
[patent_app_number] => 09/969946
[patent_app_country] => US
[patent_app_date] => 2001-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 5856
[patent_no_of_claims] => 46
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 11
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0073/20020073869.pdf
[firstpage_image] =>[orig_patent_app_number] => 09969946
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/969946 | Ultra sensitive magnetic field sensors | Oct 1, 2001 | Abandoned |
Array
(
[id] => 7618265
[patent_doc_number] => 06945174
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-09-20
[patent_title] => 'Method for connecting ignitors in an ignition system'
[patent_app_type] => utility
[patent_app_number] => 10/398075
[patent_app_country] => US
[patent_app_date] => 2001-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 3116
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 299
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/945/06945174.pdf
[firstpage_image] =>[orig_patent_app_number] => 10398075
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/398075 | Method for connecting ignitors in an ignition system | Sep 27, 2001 | Issued |