
John W. Eldred
Examiner (ID: 597, Phone: (571)272-6901 , Office: P/3641 )
| Most Active Art Unit | 3641 |
| Art Unit(s) | 2899, 3644, 2201, 3641 |
| Total Applications | 3399 |
| Issued Applications | 2824 |
| Pending Applications | 195 |
| Abandoned Applications | 399 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 438293
[patent_doc_number] => 07258308
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-08-21
[patent_title] => 'Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface'
[patent_app_type] => utility
[patent_app_number] => 10/188988
[patent_app_country] => US
[patent_app_date] => 2002-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 19
[patent_no_of_words] => 4417
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 203
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/258/07258308.pdf
[firstpage_image] =>[orig_patent_app_number] => 10188988
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/188988 | Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface | Jul 1, 2002 | Issued |
Array
(
[id] => 1391133
[patent_doc_number] => 06523785
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-25
[patent_title] => 'Reaction wheel desaturation apparatus'
[patent_app_type] => B1
[patent_app_number] => 10/187234
[patent_app_country] => US
[patent_app_date] => 2002-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 6033
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 716
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/523/06523785.pdf
[firstpage_image] =>[orig_patent_app_number] => 10187234
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/187234 | Reaction wheel desaturation apparatus | Jul 1, 2002 | Issued |
Array
(
[id] => 1308982
[patent_doc_number] => 06607165
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-08-19
[patent_title] => 'Aircraft engine mount with single thrust link'
[patent_app_type] => B1
[patent_app_number] => 10/185922
[patent_app_country] => US
[patent_app_date] => 2002-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2406
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/607/06607165.pdf
[firstpage_image] =>[orig_patent_app_number] => 10185922
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/185922 | Aircraft engine mount with single thrust link | Jun 27, 2002 | Issued |
Array
(
[id] => 6733232
[patent_doc_number] => 20030010867
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-16
[patent_title] => 'Fasteners for attaching a windshield to the fuselage side frame of an aircraft viewing port'
[patent_app_type] => new
[patent_app_number] => 10/180484
[patent_app_country] => US
[patent_app_date] => 2002-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2307
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0010/20030010867.pdf
[firstpage_image] =>[orig_patent_app_number] => 10180484
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/180484 | Fasteners for attaching a windshield to the fuselage side frame of an aircraft viewing port | Jun 26, 2002 | Issued |
Array
(
[id] => 1364784
[patent_doc_number] => 06550716
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-04-22
[patent_title] => 'Power-driven ornithopter piloted by remote controller'
[patent_app_type] => B1
[patent_app_number] => 10/184352
[patent_app_country] => US
[patent_app_date] => 2002-06-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 4629
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/550/06550716.pdf
[firstpage_image] =>[orig_patent_app_number] => 10184352
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/184352 | Power-driven ornithopter piloted by remote controller | Jun 25, 2002 | Issued |
Array
(
[id] => 5862321
[patent_doc_number] => 20060096451
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-11
[patent_title] => 'Protective device for the confinement of explosive objects or objects suspected to be such'
[patent_app_type] => utility
[patent_app_number] => 10/519277
[patent_app_country] => US
[patent_app_date] => 2002-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3153
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0096/20060096451.pdf
[firstpage_image] =>[orig_patent_app_number] => 10519277
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/519277 | Protective device for the confinement of explosive objects or objects suspected to be such | Jun 24, 2002 | Issued |
Array
(
[id] => 1299741
[patent_doc_number] => 06616104
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-09-09
[patent_title] => 'Spacecraft configuration and attitude steering method for highly inclined orbit (HIO) communications'
[patent_app_type] => B1
[patent_app_number] => 10/177110
[patent_app_country] => US
[patent_app_date] => 2002-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4367
[patent_no_of_claims] => 45
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/616/06616104.pdf
[firstpage_image] =>[orig_patent_app_number] => 10177110
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/177110 | Spacecraft configuration and attitude steering method for highly inclined orbit (HIO) communications | Jun 23, 2002 | Issued |
Array
(
[id] => 1401058
[patent_doc_number] => 06511022
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-28
[patent_title] => 'Spacecraft solar panel spherical trickle charger'
[patent_app_type] => B1
[patent_app_number] => 10/179787
[patent_app_country] => US
[patent_app_date] => 2002-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 1751
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/511/06511022.pdf
[firstpage_image] =>[orig_patent_app_number] => 10179787
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/179787 | Spacecraft solar panel spherical trickle charger | Jun 23, 2002 | Issued |
Array
(
[id] => 1299691
[patent_doc_number] => 06616092
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-09-09
[patent_title] => 'Reusable flyback rocket booster and method for recovering same'
[patent_app_type] => B1
[patent_app_number] => 10/178428
[patent_app_country] => US
[patent_app_date] => 2002-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2624
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/616/06616092.pdf
[firstpage_image] =>[orig_patent_app_number] => 10178428
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/178428 | Reusable flyback rocket booster and method for recovering same | Jun 23, 2002 | Issued |
Array
(
[id] => 1274844
[patent_doc_number] => 06641084
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-11-04
[patent_title] => 'Solid oxide fuel cell as auxiliary power source installation in transport aircraft'
[patent_app_type] => B1
[patent_app_number] => 10/177427
[patent_app_country] => US
[patent_app_date] => 2002-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4465
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/641/06641084.pdf
[firstpage_image] =>[orig_patent_app_number] => 10177427
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/177427 | Solid oxide fuel cell as auxiliary power source installation in transport aircraft | Jun 20, 2002 | Issued |
Array
(
[id] => 1326605
[patent_doc_number] => 06592072
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-07-15
[patent_title] => 'Spanwise tailoring of divergent trailing edge wings'
[patent_app_type] => B1
[patent_app_number] => 10/175623
[patent_app_country] => US
[patent_app_date] => 2002-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3124
[patent_no_of_claims] => 25
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/592/06592072.pdf
[firstpage_image] =>[orig_patent_app_number] => 10175623
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/175623 | Spanwise tailoring of divergent trailing edge wings | Jun 19, 2002 | Issued |
Array
(
[id] => 6823697
[patent_doc_number] => 20030234318
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-25
[patent_title] => 'UNBALANCED GYROSCOPIC APPARATUS FOR PRODUCING UNIDIRECTIONAL THRUST'
[patent_app_type] => new
[patent_app_number] => 10/176259
[patent_app_country] => US
[patent_app_date] => 2002-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0234/20030234318.pdf
[firstpage_image] =>[orig_patent_app_number] => 10176259
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/176259 | Unbalanced gyroscopic apparatus for producing unidirectional thrust | Jun 19, 2002 | Issued |
Array
(
[id] => 7318568
[patent_doc_number] => 20040135032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-15
[patent_title] => 'Spanwise tailoring of a trailing edge wedge to a wing'
[patent_app_type] => new
[patent_app_number] => 10/175612
[patent_app_country] => US
[patent_app_date] => 2002-06-20
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 3138
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0135/20040135032.pdf
[firstpage_image] =>[orig_patent_app_number] => 10175612
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/175612 | Spanwise tailoring of a trailing edge wedge to a wing | Jun 19, 2002 | Abandoned |
Array
(
[id] => 6872693
[patent_doc_number] => 20030192990
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-16
[patent_title] => 'Single piece co-cure composite wing'
[patent_app_type] => new
[patent_app_number] => 10/175722
[patent_app_country] => US
[patent_app_date] => 2002-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 8875
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[pdf_file] => publications/A1/0192/20030192990.pdf
[firstpage_image] =>[orig_patent_app_number] => 10175722
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/175722 | Single piece co-cure composite wing | Jun 19, 2002 | Issued |
Array
(
[id] => 1341491
[patent_doc_number] => 06575409
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-06-10
[patent_title] => 'Fluoroluminescent lighted kite'
[patent_app_type] => B1
[patent_app_number] => 10/172437
[patent_app_country] => US
[patent_app_date] => 2002-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/575/06575409.pdf
[firstpage_image] =>[orig_patent_app_number] => 10172437
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/172437 | Fluoroluminescent lighted kite | Jun 16, 2002 | Issued |
Array
(
[id] => 1231521
[patent_doc_number] => 06688552
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-10
[patent_title] => 'Variable cycle propulsion system with mechanical transmission for a supersonic airplane'
[patent_app_type] => B2
[patent_app_number] => 10/170381
[patent_app_country] => US
[patent_app_date] => 2002-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/688/06688552.pdf
[firstpage_image] =>[orig_patent_app_number] => 10170381
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/170381 | Variable cycle propulsion system with mechanical transmission for a supersonic airplane | Jun 13, 2002 | Issued |
Array
(
[id] => 1361476
[patent_doc_number] => 06554225
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-04-29
[patent_title] => 'Commercial aircraft low cost, lightweight floor design'
[patent_app_type] => B1
[patent_app_number] => 10/171608
[patent_app_country] => US
[patent_app_date] => 2002-06-14
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/554/06554225.pdf
[firstpage_image] =>[orig_patent_app_number] => 10171608
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/171608 | Commercial aircraft low cost, lightweight floor design | Jun 13, 2002 | Issued |
Array
(
[id] => 1238588
[patent_doc_number] => 06682023
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-27
[patent_title] => 'Contiguous variable camber device'
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[patent_app_number] => 10/172153
[patent_app_country] => US
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[pdf_file] => patents/06/682/06682023.pdf
[firstpage_image] =>[orig_patent_app_number] => 10172153
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/172153 | Contiguous variable camber device | Jun 13, 2002 | Issued |
Array
(
[id] => 1381740
[patent_doc_number] => 06530541
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-03-11
[patent_title] => 'Compressed air engine and flying object equipped therewith'
[patent_app_type] => B1
[patent_app_number] => 10/167728
[patent_app_country] => US
[patent_app_date] => 2002-06-11
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/530/06530541.pdf
[firstpage_image] =>[orig_patent_app_number] => 10167728
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/167728 | Compressed air engine and flying object equipped therewith | Jun 10, 2002 | Issued |
Array
(
[id] => 1351524
[patent_doc_number] => 06565037
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-05-20
[patent_title] => 'Hybrid aircraft and methods of flying'
[patent_app_type] => B1
[patent_app_number] => 10/161915
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/565/06565037.pdf
[firstpage_image] =>[orig_patent_app_number] => 10161915
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/161915 | Hybrid aircraft and methods of flying | Jun 3, 2002 | Issued |