Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 122 [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 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 3124 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 17 [patent_no_of_words] => 3422 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 324 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3138 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 8875 [patent_no_of_claims] => 57 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 30 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 835 [patent_no_of_claims] => 2 [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/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 [patent_figures_cnt] => 2 [patent_no_of_words] => 2324 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 249 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4441 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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' [patent_app_type] => B2 [patent_app_number] => 10/172153 [patent_app_country] => US [patent_app_date] => 2002-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 3697 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 18 [patent_no_of_words] => 4140 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_date] => 2002-06-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 4816 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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