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] => 1152335
[patent_doc_number] => 06758142
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-07-06
[patent_title] => 'Pneumatic stage separation system for two stage launch vehicle'
[patent_app_type] => B1
[patent_app_number] => 10/352518
[patent_app_country] => US
[patent_app_date] => 2003-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2373
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 159
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/758/06758142.pdf
[firstpage_image] =>[orig_patent_app_number] => 10352518
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/352518 | Pneumatic stage separation system for two stage launch vehicle | Jan 27, 2003 | Issued |
Array
(
[id] => 6655505
[patent_doc_number] => 20030132343
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-17
[patent_title] => 'Method and system for setting hull parameter of airship and method of adjusting ascension rate of the same'
[patent_app_type] => new
[patent_app_number] => 10/337998
[patent_app_country] => US
[patent_app_date] => 2003-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 4659
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0132/20030132343.pdf
[firstpage_image] =>[orig_patent_app_number] => 10337998
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/337998 | Method and system for setting hull parameter of airship and method of adjusting ascension rate of the same | Jan 7, 2003 | Issued |
Array
(
[id] => 6763994
[patent_doc_number] => 20030098392
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-29
[patent_title] => 'Aircraft kite'
[patent_app_type] => new
[patent_app_number] => 10/339200
[patent_app_country] => US
[patent_app_date] => 2003-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4872
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 23
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0098/20030098392.pdf
[firstpage_image] =>[orig_patent_app_number] => 10339200
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/339200 | Aircraft kite | Jan 7, 2003 | Issued |
Array
(
[id] => 7304737
[patent_doc_number] => 20040140396
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-22
[patent_title] => 'Toy aircraft'
[patent_app_type] => new
[patent_app_number] => 10/336987
[patent_app_country] => US
[patent_app_date] => 2003-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2414
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0140/20040140396.pdf
[firstpage_image] =>[orig_patent_app_number] => 10336987
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/336987 | Toy aircraft | Jan 5, 2003 | Abandoned |
Array
(
[id] => 1079673
[patent_doc_number] => 06834829
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-12-28
[patent_title] => 'Vertical lift aircraft having an enclosed rotary wing'
[patent_app_type] => B2
[patent_app_number] => 10/334727
[patent_app_country] => US
[patent_app_date] => 2003-01-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 7604
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 203
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/834/06834829.pdf
[firstpage_image] =>[orig_patent_app_number] => 10334727
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/334727 | Vertical lift aircraft having an enclosed rotary wing | Jan 1, 2003 | Issued |
Array
(
[id] => 7286176
[patent_doc_number] => 20040108417
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-06-10
[patent_title] => 'Ram air parachute with tensioned top skin'
[patent_app_type] => new
[patent_app_number] => 10/315555
[patent_app_country] => US
[patent_app_date] => 2002-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2496
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0108/20040108417.pdf
[firstpage_image] =>[orig_patent_app_number] => 10315555
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/315555 | Ram air parachute with tensioned top skin | Dec 8, 2002 | Issued |
Array
(
[id] => 7392702
[patent_doc_number] => 20040103577
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-06-03
[patent_title] => 'Accessory rail mount adapter for rifles and carbines'
[patent_app_type] => new
[patent_app_number] => 10/305967
[patent_app_country] => US
[patent_app_date] => 2002-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4065
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0103/20040103577.pdf
[firstpage_image] =>[orig_patent_app_number] => 10305967
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/305967 | Accessory rail mount adapter for rifles and carbines | Nov 28, 2002 | Issued |
Array
(
[id] => 1067337
[patent_doc_number] => 06843446
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-01-18
[patent_title] => 'Apparatus and methods for in-space satellite operations'
[patent_app_type] => utility
[patent_app_number] => 10/304210
[patent_app_country] => US
[patent_app_date] => 2002-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 6163
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 254
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/843/06843446.pdf
[firstpage_image] =>[orig_patent_app_number] => 10304210
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/304210 | Apparatus and methods for in-space satellite operations | Nov 24, 2002 | Issued |
Array
(
[id] => 7458252
[patent_doc_number] => 20040094659
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-20
[patent_title] => 'Laminar-flow airfoil'
[patent_app_type] => new
[patent_app_number] => 10/299660
[patent_app_country] => US
[patent_app_date] => 2002-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3204
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 48
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0094/20040094659.pdf
[firstpage_image] =>[orig_patent_app_number] => 10299660
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/299660 | Laminar-flow airfoil | Nov 19, 2002 | Issued |
Array
(
[id] => 6758672
[patent_doc_number] => 20030122033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-03
[patent_title] => 'Ring-shaped wing helicopter'
[patent_app_type] => new
[patent_app_number] => 10/295796
[patent_app_country] => US
[patent_app_date] => 2002-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1983
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20030122033.pdf
[firstpage_image] =>[orig_patent_app_number] => 10295796
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/295796 | Ring-shaped wing helicopter | Nov 14, 2002 | Abandoned |
Array
(
[id] => 7458342
[patent_doc_number] => 20040094671
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-20
[patent_title] => 'Automatic inflation system for evacuation slide'
[patent_app_type] => new
[patent_app_number] => 10/295505
[patent_app_country] => US
[patent_app_date] => 2002-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2460
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0094/20040094671.pdf
[firstpage_image] =>[orig_patent_app_number] => 10295505
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/295505 | Automatic inflation system for evacuation slide | Nov 14, 2002 | Issued |
Array
(
[id] => 7204077
[patent_doc_number] => 20040069895
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-15
[patent_title] => 'Aircraft lightning strike protection and grounding technique'
[patent_app_type] => new
[patent_app_number] => 10/269194
[patent_app_country] => US
[patent_app_date] => 2002-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1456
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 70
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0069/20040069895.pdf
[firstpage_image] =>[orig_patent_app_number] => 10269194
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/269194 | Aircraft lightning strike protection and grounding technique | Oct 10, 2002 | Issued |
Array
(
[id] => 1243661
[patent_doc_number] => 06676073
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-13
[patent_title] => 'Pivoting power transmission unit with peripheral face toothed gearwheels of the face gear type'
[patent_app_type] => B2
[patent_app_number] => 10/262824
[patent_app_country] => US
[patent_app_date] => 2002-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4390
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/676/06676073.pdf
[firstpage_image] =>[orig_patent_app_number] => 10262824
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/262824 | Pivoting power transmission unit with peripheral face toothed gearwheels of the face gear type | Oct 1, 2002 | Issued |
Array
(
[id] => 6713080
[patent_doc_number] => 20030024427
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-06
[patent_title] => 'Safety system for a projectile fuse'
[patent_app_type] => new
[patent_app_number] => 10/254194
[patent_app_country] => US
[patent_app_date] => 2002-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6856
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 6
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0024/20030024427.pdf
[firstpage_image] =>[orig_patent_app_number] => 10254194
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/254194 | Safety system for a projectile fuse | Sep 24, 2002 | Issued |
Array
(
[id] => 7267626
[patent_doc_number] => 20040056144
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-25
[patent_title] => 'Dual-flight mode tandem rotor wing'
[patent_app_type] => new
[patent_app_number] => 10/253179
[patent_app_country] => US
[patent_app_date] => 2002-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3752
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0056/20040056144.pdf
[firstpage_image] =>[orig_patent_app_number] => 10253179
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/253179 | Dual-flight mode tandem rotor wing | Sep 23, 2002 | Issued |
Array
(
[id] => 7266788
[patent_doc_number] => 20040055501
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-25
[patent_title] => 'Penetrator and method for using same'
[patent_app_type] => new
[patent_app_number] => 10/251423
[patent_app_country] => US
[patent_app_date] => 2002-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 4199
[patent_no_of_claims] => 60
[patent_no_of_ind_claims] => 5
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0055/20040055501.pdf
[firstpage_image] =>[orig_patent_app_number] => 10251423
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/251423 | Penetrator and method for using same | Sep 19, 2002 | Abandoned |
Array
(
[id] => 6717911
[patent_doc_number] => 20030051598
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-20
[patent_title] => 'Seating unit in a combat vehicle that is protected against mines'
[patent_app_type] => new
[patent_app_number] => 10/243527
[patent_app_country] => US
[patent_app_date] => 2002-09-13
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0051/20030051598.pdf
[firstpage_image] =>[orig_patent_app_number] => 10243527
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/243527 | Seating unit in a combat vehicle that is protected against mines | Sep 12, 2002 | Issued |
Array
(
[id] => 7613693
[patent_doc_number] => 06902137
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-06-07
[patent_title] => 'Aircraft door latch/lock mechanism with pneumatic decompression override'
[patent_app_type] => utility
[patent_app_number] => 10/241283
[patent_app_country] => US
[patent_app_date] => 2002-09-09
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/902/06902137.pdf
[firstpage_image] =>[orig_patent_app_number] => 10241283
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/241283 | Aircraft door latch/lock mechanism with pneumatic decompression override | Sep 8, 2002 | Issued |
Array
(
[id] => 7339940
[patent_doc_number] => 20040045207
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-11
[patent_title] => 'Electrical discharge weapon for use as forend grip of rifles'
[patent_app_type] => new
[patent_app_number] => 10/237275
[patent_app_country] => US
[patent_app_date] => 2002-09-09
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0045/20040045207.pdf
[firstpage_image] =>[orig_patent_app_number] => 10237275
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/237275 | Electric discharge weapon for use as forend grip of rifles | Sep 8, 2002 | Issued |
Array
(
[id] => 1033102
[patent_doc_number] => 06874730
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-05
[patent_title] => 'Covering element for the interior of a vehicle, particularly an aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/232392
[patent_app_country] => US
[patent_app_date] => 2002-09-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 4496
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/874/06874730.pdf
[firstpage_image] =>[orig_patent_app_number] => 10232392
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/232392 | Covering element for the interior of a vehicle, particularly an aircraft | Sep 2, 2002 | Issued |