Alyssa L Cepluch
Examiner (ID: 3666, Phone: (571)270-5752 , Office: P/1772 )
Most Active Art Unit | 1772 |
Art Unit(s) | 1722, 1772 |
Total Applications | 540 |
Issued Applications | 299 |
Pending Applications | 73 |
Abandoned Applications | 168 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 3686489
[patent_doc_number] => 05660523
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-08-26
[patent_title] => 'Turbine blade squealer tip peripheral end wall with cooling passage arrangement'
[patent_app_type] => 1
[patent_app_number] => 7/829641
[patent_app_country] => US
[patent_app_date] => 1992-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2738
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/660/05660523.pdf
[firstpage_image] =>[orig_patent_app_number] => 829641
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/829641 | Turbine blade squealer tip peripheral end wall with cooling passage arrangement | Feb 2, 1992 | Issued |
Array
(
[id] => 3676226
[patent_doc_number] => 05690472
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-11-25
[patent_title] => 'Internal cooling of turbine airfoil wall using mesh cooling hole arrangement'
[patent_app_type] => 1
[patent_app_number] => 7/830145
[patent_app_country] => US
[patent_app_date] => 1992-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 3166
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 301
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/690/05690472.pdf
[firstpage_image] =>[orig_patent_app_number] => 830145
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/830145 | Internal cooling of turbine airfoil wall using mesh cooling hole arrangement | Feb 2, 1992 | Issued |
Array
(
[id] => 3762484
[patent_doc_number] => 05816777
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-10-06
[patent_title] => 'Turbine blade cooling'
[patent_app_type] => 1
[patent_app_number] => 7/799650
[patent_app_country] => US
[patent_app_date] => 1991-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 1553
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 155
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/816/05816777.pdf
[firstpage_image] =>[orig_patent_app_number] => 799650
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/799650 | Turbine blade cooling | Nov 28, 1991 | Issued |
Array
(
[id] => 3688911
[patent_doc_number] => 05653110
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-08-05
[patent_title] => 'Film cooling of jet engine components'
[patent_app_type] => 1
[patent_app_number] => 7/733892
[patent_app_country] => US
[patent_app_date] => 1991-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2140
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/653/05653110.pdf
[firstpage_image] =>[orig_patent_app_number] => 733892
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/733892 | Film cooling of jet engine components | Jul 21, 1991 | Issued |
Array
(
[id] => 3397493
[patent_doc_number] => 05437190
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-08-01
[patent_title] => 'Method for determining the effects of stress'
[patent_app_type] => 1
[patent_app_number] => 7/706680
[patent_app_country] => US
[patent_app_date] => 1991-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3144
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/437/05437190.pdf
[firstpage_image] =>[orig_patent_app_number] => 706680
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/706680 | Method for determining the effects of stress | May 28, 1991 | Issued |
Array
(
[id] => 3435902
[patent_doc_number] => 05419512
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-05-30
[patent_title] => 'Towed fiber optic data link payout system'
[patent_app_type] => 1
[patent_app_number] => 7/579002
[patent_app_country] => US
[patent_app_date] => 1990-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 2270
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 33
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/419/05419512.pdf
[firstpage_image] =>[orig_patent_app_number] => 579002
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/579002 | Towed fiber optic data link payout system | Sep 5, 1990 | Issued |
Array
(
[id] => 3690663
[patent_doc_number] => 05674050
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-10-07
[patent_title] => 'Turbine blade'
[patent_app_type] => 1
[patent_app_number] => 7/279632
[patent_app_country] => US
[patent_app_date] => 1988-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 5
[patent_no_of_words] => 1078
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 204
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/674/05674050.pdf
[firstpage_image] =>[orig_patent_app_number] => 279632
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/279632 | Turbine blade | Dec 4, 1988 | Issued |
Array
(
[id] => 3746584
[patent_doc_number] => 05720431
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-02-24
[patent_title] => 'Cooled blades for a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/236092
[patent_app_country] => US
[patent_app_date] => 1988-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 2910
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/720/05720431.pdf
[firstpage_image] =>[orig_patent_app_number] => 236092
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/236092 | Cooled blades for a gas turbine engine | Aug 23, 1988 | Issued |
Array
(
[id] => 3653229
[patent_doc_number] => 05667359
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-09-16
[patent_title] => 'Clearance control for the turbine of a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/236094
[patent_app_country] => US
[patent_app_date] => 1988-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 2324
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/667/05667359.pdf
[firstpage_image] =>[orig_patent_app_number] => 236094
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/236094 | Clearance control for the turbine of a gas turbine engine | Aug 23, 1988 | Issued |
Array
(
[id] => 3716520
[patent_doc_number] => 05700131
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-23
[patent_title] => 'Cooled blades for a gas turbine engine'
[patent_app_type] => 1
[patent_app_number] => 7/236093
[patent_app_country] => US
[patent_app_date] => 1988-08-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 2105
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 192
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/700/05700131.pdf
[firstpage_image] =>[orig_patent_app_number] => 236093
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/236093 | Cooled blades for a gas turbine engine | Aug 23, 1988 | Issued |
Array
(
[id] => 3835763
[patent_doc_number] => 05712442
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-01-27
[patent_title] => 'Method for launching projectiles with hydrogen gas'
[patent_app_type] => 1
[patent_app_number] => 7/199879
[patent_app_country] => US
[patent_app_date] => 1988-05-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 5555
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/712/05712442.pdf
[firstpage_image] =>[orig_patent_app_number] => 199879
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/199879 | Method for launching projectiles with hydrogen gas | May 26, 1988 | Issued |
Array
(
[id] => 3508536
[patent_doc_number] => 05539960
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-30
[patent_title] => 'Cylindrical convex doorknob termination'
[patent_app_type] => 1
[patent_app_number] => 7/150360
[patent_app_country] => US
[patent_app_date] => 1987-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 1638
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/539/05539960.pdf
[firstpage_image] =>[orig_patent_app_number] => 150360
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/150360 | Cylindrical convex doorknob termination | Dec 21, 1987 | Issued |
Array
(
[id] => 3499205
[patent_doc_number] => 05562409
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-10-08
[patent_title] => 'Air cooled gas turbine aerofoil'
[patent_app_type] => 1
[patent_app_number] => 6/820268
[patent_app_country] => US
[patent_app_date] => 1985-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1213
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/562/05562409.pdf
[firstpage_image] =>[orig_patent_app_number] => 820268
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/820268 | Air cooled gas turbine aerofoil | Nov 26, 1985 | Issued |
Array
(
[id] => 3475464
[patent_doc_number] => 05438906
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-08-08
[patent_title] => 'Unitized shock absorbing pad with looped fiber ring'
[patent_app_type] => 1
[patent_app_number] => 6/640426
[patent_app_country] => US
[patent_app_date] => 1984-08-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 1286
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/438/05438906.pdf
[firstpage_image] =>[orig_patent_app_number] => 640426
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/640426 | Unitized shock absorbing pad with looped fiber ring | Aug 12, 1984 | Issued |
Array
(
[id] => 3542373
[patent_doc_number] => 05571262
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-11-05
[patent_title] => 'Supersonic nozzle for a turbojet engine'
[patent_app_type] => 1
[patent_app_number] => 6/573700
[patent_app_country] => US
[patent_app_date] => 1984-01-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4447
[patent_no_of_claims] => 16
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[patent_words_short_claim] => 227
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/571/05571262.pdf
[firstpage_image] =>[orig_patent_app_number] => 573700
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/573700 | Supersonic nozzle for a turbojet engine | Jan 11, 1984 | Issued |
Array
(
[id] => 3480405
[patent_doc_number] => 05439233
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-08-08
[patent_title] => 'Large annular segmented seal with lock portions for missile launch tube'
[patent_app_type] => 1
[patent_app_number] => 6/530912
[patent_app_country] => US
[patent_app_date] => 1983-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 589
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/439/05439233.pdf
[firstpage_image] =>[orig_patent_app_number] => 530912
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/530912 | Large annular segmented seal with lock portions for missile launch tube | Sep 8, 1983 | Issued |
Array
(
[id] => 3716506
[patent_doc_number] => 05700130
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-12-23
[patent_title] => 'Device for cooling and gas turbine rotor'
[patent_app_type] => 1
[patent_app_number] => 6/474526
[patent_app_country] => US
[patent_app_date] => 1983-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4168
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/700/05700130.pdf
[firstpage_image] =>[orig_patent_app_number] => 474526
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/474526 | Device for cooling and gas turbine rotor | Mar 8, 1983 | Issued |
Array
(
[id] => 3467213
[patent_doc_number] => 05456179
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-10-10
[patent_title] => 'Infrared proximity detector device for flying missile and detector assembly for autorotating missile including such device'
[patent_app_type] => 1
[patent_app_number] => 6/325356
[patent_app_country] => US
[patent_app_date] => 1981-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1216
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[patent_words_short_claim] => 96
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/456/05456179.pdf
[firstpage_image] =>[orig_patent_app_number] => 325356
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/325356 | Infrared proximity detector device for flying missile and detector assembly for autorotating missile including such device | Oct 27, 1981 | Issued |
Array
(
[id] => 3411883
[patent_doc_number] => 05458298
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-10-17
[patent_title] => 'Device for optically guiding an autorotating missile'
[patent_app_type] => 1
[patent_app_number] => 6/325330
[patent_app_country] => US
[patent_app_date] => 1981-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/458/05458298.pdf
[firstpage_image] =>[orig_patent_app_number] => 325330
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/325330 | Device for optically guiding an autorotating missile | Oct 27, 1981 | Issued |
Array
(
[id] => 3972073
[patent_doc_number] => 05860619
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-01-19
[patent_title] => 'Seeker head'
[patent_app_type] => 1
[patent_app_number] => 6/178557
[patent_app_country] => US
[patent_app_date] => 1980-08-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 13
[patent_no_of_words] => 5280
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[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 210
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/860/05860619.pdf
[firstpage_image] =>[orig_patent_app_number] => 178557
[rel_patent_id] =>[rel_patent_doc_number] =>) 06/178557 | Seeker head | Aug 4, 1980 | Issued |