
Theresa M. Wesson
Examiner (ID: 7927)
| Most Active Art Unit | 3641 |
| Art Unit(s) | 2201, 3641 |
| Total Applications | 494 |
| Issued Applications | 431 |
| Pending Applications | 37 |
| Abandoned Applications | 26 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 3926014
[patent_doc_number] => 05914459
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-22
[patent_title] => 'Acceleration/deceleration sensing switch for munitions'
[patent_app_type] => 1
[patent_app_number] => 8/905173
[patent_app_country] => US
[patent_app_date] => 1997-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3960
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/914/05914459.pdf
[firstpage_image] =>[orig_patent_app_number] => 905173
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/905173 | Acceleration/deceleration sensing switch for munitions | Jul 31, 1997 | Issued |
Array
(
[id] => 3890160
[patent_doc_number] => 06000340
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-14
[patent_title] => 'Rocket launching system employing thermal-acoustic detection for rocket ignition'
[patent_app_type] => 1
[patent_app_number] => 8/902893
[patent_app_country] => US
[patent_app_date] => 1997-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1995
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/000/06000340.pdf
[firstpage_image] =>[orig_patent_app_number] => 902893
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/902893 | Rocket launching system employing thermal-acoustic detection for rocket ignition | Jul 29, 1997 | Issued |
Array
(
[id] => 3958899
[patent_doc_number] => 05947417
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-09-07
[patent_title] => 'Fairing for an expandable bay'
[patent_app_type] => 1
[patent_app_number] => 8/900636
[patent_app_country] => US
[patent_app_date] => 1997-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 1273
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/947/05947417.pdf
[firstpage_image] =>[orig_patent_app_number] => 900636
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/900636 | Fairing for an expandable bay | Jul 24, 1997 | Issued |
Array
(
[id] => 3911632
[patent_doc_number] => 05913494
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-22
[patent_title] => 'Blade seal for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/900634
[patent_app_country] => US
[patent_app_date] => 1997-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 961
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 30
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/913/05913494.pdf
[firstpage_image] =>[orig_patent_app_number] => 900634
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/900634 | Blade seal for an aircraft | Jul 24, 1997 | Issued |
Array
(
[id] => 3866700
[patent_doc_number] => 05775589
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-07
[patent_title] => 'Cooling apparatus for aircraft gas turbine engine exhaust nozzles'
[patent_app_type] => 1
[patent_app_number] => 8/898744
[patent_app_country] => US
[patent_app_date] => 1997-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 3747
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/775/05775589.pdf
[firstpage_image] =>[orig_patent_app_number] => 898744
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/898744 | Cooling apparatus for aircraft gas turbine engine exhaust nozzles | Jul 22, 1997 | Issued |
Array
(
[id] => 3909996
[patent_doc_number] => 05875993
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-03-02
[patent_title] => 'Flight control of an airborne vehicle at low velocity'
[patent_app_type] => 1
[patent_app_number] => 8/891040
[patent_app_country] => US
[patent_app_date] => 1997-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3385
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/875/05875993.pdf
[firstpage_image] =>[orig_patent_app_number] => 891040
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/891040 | Flight control of an airborne vehicle at low velocity | Jul 9, 1997 | Issued |
Array
(
[id] => 4021034
[patent_doc_number] => 05855339
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-01-05
[patent_title] => 'System and method for simultaneously guiding multiple missiles'
[patent_app_type] => 1
[patent_app_number] => 8/888963
[patent_app_country] => US
[patent_app_date] => 1997-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3323
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/855/05855339.pdf
[firstpage_image] =>[orig_patent_app_number] => 888963
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/888963 | System and method for simultaneously guiding multiple missiles | Jul 6, 1997 | Issued |
Array
(
[id] => 3725174
[patent_doc_number] => 05799899
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-09-01
[patent_title] => 'Error detector apparatus with digital coordinate transformation'
[patent_app_type] => 1
[patent_app_number] => 8/888613
[patent_app_country] => US
[patent_app_date] => 1997-07-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 3173
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 11
[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/799/05799899.pdf
[firstpage_image] =>[orig_patent_app_number] => 888613
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/888613 | Error detector apparatus with digital coordinate transformation | Jul 6, 1997 | Issued |
Array
(
[id] => 3810854
[patent_doc_number] => 05831206
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-03
[patent_title] => 'Ring vortex depth charge'
[patent_app_type] => 1
[patent_app_number] => 8/903215
[patent_app_country] => US
[patent_app_date] => 1997-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 3792
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 325
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/831/05831206.pdf
[firstpage_image] =>[orig_patent_app_number] => 903215
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/903215 | Ring vortex depth charge | Jul 1, 1997 | Issued |
| 08/884718 | LASER-IGNITABLE IGNITION COMPOSITION AND INITIATOR DEVICES AND ASSEMBLIES COMPRISING THE SAME | Jun 29, 1997 | Abandoned |
Array
(
[id] => 3783316
[patent_doc_number] => 05826819
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-27
[patent_title] => 'Weapon system employing a transponder bomb and guidance method thereof'
[patent_app_type] => 1
[patent_app_number] => 8/883941
[patent_app_country] => US
[patent_app_date] => 1997-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3383
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/826/05826819.pdf
[firstpage_image] =>[orig_patent_app_number] => 883941
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/883941 | Weapon system employing a transponder bomb and guidance method thereof | Jun 26, 1997 | Issued |
Array
(
[id] => 3804511
[patent_doc_number] => 05782031
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-07-21
[patent_title] => 'Firearm piercing tool attachment device'
[patent_app_type] => 1
[patent_app_number] => 8/881837
[patent_app_country] => US
[patent_app_date] => 1997-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2261
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/782/05782031.pdf
[firstpage_image] =>[orig_patent_app_number] => 881837
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/881837 | Firearm piercing tool attachment device | Jun 24, 1997 | Issued |
Array
(
[id] => 3963077
[patent_doc_number] => 05904133
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-18
[patent_title] => 'Paintball gun air reservoir'
[patent_app_type] => 1
[patent_app_number] => 8/882672
[patent_app_country] => US
[patent_app_date] => 1997-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1013
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/904/05904133.pdf
[firstpage_image] =>[orig_patent_app_number] => 882672
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/882672 | Paintball gun air reservoir | Jun 24, 1997 | Issued |
Array
(
[id] => 3843212
[patent_doc_number] => 05847307
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-08
[patent_title] => 'Missile launcher apparatus'
[patent_app_type] => 1
[patent_app_number] => 8/881642
[patent_app_country] => US
[patent_app_date] => 1997-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 1774
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/847/05847307.pdf
[firstpage_image] =>[orig_patent_app_number] => 881642
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/881642 | Missile launcher apparatus | Jun 23, 1997 | Issued |
Array
(
[id] => 3872517
[patent_doc_number] => 05837917
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-17
[patent_title] => 'Cooling apparatus for a missile launcher system'
[patent_app_type] => 1
[patent_app_number] => 8/881641
[patent_app_country] => US
[patent_app_date] => 1997-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 16
[patent_no_of_words] => 2483
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/837/05837917.pdf
[firstpage_image] =>[orig_patent_app_number] => 881641
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/881641 | Cooling apparatus for a missile launcher system | Jun 23, 1997 | Issued |
Array
(
[id] => 3907705
[patent_doc_number] => 05944285
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-31
[patent_title] => 'Vent valve with pressure relief'
[patent_app_type] => 1
[patent_app_number] => 8/879839
[patent_app_country] => US
[patent_app_date] => 1997-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4357
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 224
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/944/05944285.pdf
[firstpage_image] =>[orig_patent_app_number] => 879839
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/879839 | Vent valve with pressure relief | Jun 18, 1997 | Issued |
Array
(
[id] => 4068573
[patent_doc_number] => 05866837
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-02
[patent_title] => 'Method for safe flight testing of high velocity interceptor missiles'
[patent_app_type] => 1
[patent_app_number] => 8/878124
[patent_app_country] => US
[patent_app_date] => 1997-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1881
[patent_no_of_claims] => 19
[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/05/866/05866837.pdf
[firstpage_image] =>[orig_patent_app_number] => 878124
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/878124 | Method for safe flight testing of high velocity interceptor missiles | Jun 17, 1997 | Issued |
Array
(
[id] => 4085179
[patent_doc_number] => 06047926
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-11
[patent_title] => 'Hybrid deicing system and method of operation'
[patent_app_type] => 1
[patent_app_number] => 8/877272
[patent_app_country] => US
[patent_app_date] => 1997-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 4799
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/047/06047926.pdf
[firstpage_image] =>[orig_patent_app_number] => 877272
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/877272 | Hybrid deicing system and method of operation | Jun 16, 1997 | Issued |
Array
(
[id] => 3757696
[patent_doc_number] => 05819460
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-13
[patent_title] => 'Repeater mechanism for rifles having a straight breech'
[patent_app_type] => 1
[patent_app_number] => 8/874513
[patent_app_country] => US
[patent_app_date] => 1997-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1814
[patent_no_of_claims] => 5
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[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/819/05819460.pdf
[firstpage_image] =>[orig_patent_app_number] => 874513
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/874513 | Repeater mechanism for rifles having a straight breech | Jun 12, 1997 | Issued |
Array
(
[id] => 3756101
[patent_doc_number] => 05848764
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-15
[patent_title] => 'Body fixed terminal guidance system for a missile'
[patent_app_type] => 1
[patent_app_number] => 8/876080
[patent_app_country] => US
[patent_app_date] => 1997-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 2053
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 182
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/848/05848764.pdf
[firstpage_image] =>[orig_patent_app_number] => 876080
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/876080 | Body fixed terminal guidance system for a missile | Jun 12, 1997 | Issued |