
John W. Eldred
Examiner (ID: 10195)
| Most Active Art Unit | 3641 |
| Art Unit(s) | 3644, 3641, 2201, 2899 |
| Total Applications | 3389 |
| Issued Applications | 2819 |
| Pending Applications | 192 |
| Abandoned Applications | 398 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 1511879
[patent_doc_number] => 06419190
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-16
[patent_title] => 'Airborne cleaning and painting robot'
[patent_app_type] => B1
[patent_app_number] => 09/684382
[patent_app_country] => US
[patent_app_date] => 2000-10-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 15
[patent_no_of_words] => 2042
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/419/06419190.pdf
[firstpage_image] =>[orig_patent_app_number] => 09684382
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/684382 | Airborne cleaning and painting robot | Oct 9, 2000 | Issued |
Array
(
[id] => 1473750
[patent_doc_number] => 06450453
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-17
[patent_title] => 'Active steering of an appendage on a spacecraft using piezoelectric actuators'
[patent_app_type] => B1
[patent_app_number] => 09/684225
[patent_app_country] => US
[patent_app_date] => 2000-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2285
[patent_no_of_claims] => 20
[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/06/450/06450453.pdf
[firstpage_image] =>[orig_patent_app_number] => 09684225
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/684225 | Active steering of an appendage on a spacecraft using piezoelectric actuators | Oct 5, 2000 | Issued |
Array
(
[id] => 1434393
[patent_doc_number] => 06354032
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-12
[patent_title] => 'Trigger stop'
[patent_app_type] => B1
[patent_app_number] => 09/680917
[patent_app_country] => US
[patent_app_date] => 2000-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 1830
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/354/06354032.pdf
[firstpage_image] =>[orig_patent_app_number] => 09680917
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/680917 | Trigger stop | Oct 5, 2000 | Issued |
Array
(
[id] => 1577083
[patent_doc_number] => 06422510
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Shimmy-free aircraft tail wheel conversion'
[patent_app_type] => B1
[patent_app_number] => 09/679965
[patent_app_country] => US
[patent_app_date] => 2000-10-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2350
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 150
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/422/06422510.pdf
[firstpage_image] =>[orig_patent_app_number] => 09679965
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/679965 | Shimmy-free aircraft tail wheel conversion | Oct 4, 2000 | Issued |
Array
(
[id] => 1577101
[patent_doc_number] => 06422516
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
[patent_app_type] => B1
[patent_app_number] => 09/672061
[patent_app_country] => US
[patent_app_date] => 2000-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 19
[patent_no_of_words] => 16679
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 25
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/422/06422516.pdf
[firstpage_image] =>[orig_patent_app_number] => 09672061
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/672061 | Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith | Sep 28, 2000 | Issued |
Array
(
[id] => 4309962
[patent_doc_number] => 06328264
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-12-11
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
[patent_app_type] => 1
[patent_app_number] => 9/672062
[patent_app_country] => US
[patent_app_date] => 2000-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 19
[patent_no_of_words] => 17137
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/328/06328264.pdf
[firstpage_image] =>[orig_patent_app_number] => 672062
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/672062 | Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith | Sep 28, 2000 | Issued |
Array
(
[id] => 1148402
[patent_doc_number] => 06764049
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-07-20
[patent_title] => 'Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith'
[patent_app_type] => B1
[patent_app_number] => 09/672951
[patent_app_country] => US
[patent_app_date] => 2000-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 19
[patent_no_of_words] => 16681
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/764/06764049.pdf
[firstpage_image] =>[orig_patent_app_number] => 09672951
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/672951 | Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith | Sep 28, 2000 | Issued |
Array
(
[id] => 1567923
[patent_doc_number] => 06497390
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-24
[patent_title] => 'Thermal protection system especially for space vehicles'
[patent_app_type] => B1
[patent_app_number] => 09/669128
[patent_app_country] => US
[patent_app_date] => 2000-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 2899
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/497/06497390.pdf
[firstpage_image] =>[orig_patent_app_number] => 09669128
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/669128 | Thermal protection system especially for space vehicles | Sep 24, 2000 | Issued |
| 09/666387 | Articulated set of sequentially opened solar generator panels | Sep 19, 2000 | Abandoned |
Array
(
[id] => 1396636
[patent_doc_number] => 06517029
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-11
[patent_title] => 'Friction and stiction compensation for spacecraft attitude control'
[patent_app_type] => B1
[patent_app_number] => 09/660749
[patent_app_country] => US
[patent_app_date] => 2000-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5327
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/517/06517029.pdf
[firstpage_image] =>[orig_patent_app_number] => 09660749
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/660749 | Friction and stiction compensation for spacecraft attitude control | Sep 12, 2000 | Issued |
Array
(
[id] => 1555342
[patent_doc_number] => 06435455
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-20
[patent_title] => 'Flow-efficient, static pressure-shielding, fire-resistant decompression panel assembly'
[patent_app_type] => B1
[patent_app_number] => 09/658837
[patent_app_country] => US
[patent_app_date] => 2000-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 21
[patent_no_of_words] => 5771
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/435/06435455.pdf
[firstpage_image] =>[orig_patent_app_number] => 09658837
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/658837 | Flow-efficient, static pressure-shielding, fire-resistant decompression panel assembly | Sep 7, 2000 | Issued |
Array
(
[id] => 1558070
[patent_doc_number] => 06360991
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-26
[patent_title] => 'Motorized paraglider with automatic steering system for preventing upset'
[patent_app_type] => B1
[patent_app_number] => 09/658630
[patent_app_country] => US
[patent_app_date] => 2000-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1706
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/360/06360991.pdf
[firstpage_image] =>[orig_patent_app_number] => 09658630
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/658630 | Motorized paraglider with automatic steering system for preventing upset | Sep 7, 2000 | Issued |
Array
(
[id] => 1405885
[patent_doc_number] => 06505795
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-01-14
[patent_title] => 'Application of carbon fiber mesh for space and airborne platform applications'
[patent_app_type] => B1
[patent_app_number] => 09/654924
[patent_app_country] => US
[patent_app_date] => 2000-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 18
[patent_no_of_words] => 3121
[patent_no_of_claims] => 32
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/505/06505795.pdf
[firstpage_image] =>[orig_patent_app_number] => 09654924
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/654924 | Application of carbon fiber mesh for space and airborne platform applications | Sep 4, 2000 | Issued |
Array
(
[id] => 1511883
[patent_doc_number] => 06419191
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-16
[patent_title] => 'Electrodynamic tether control'
[patent_app_type] => B1
[patent_app_number] => 09/651557
[patent_app_country] => US
[patent_app_date] => 2000-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 35
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[patent_no_of_words] => 45405
[patent_no_of_claims] => 51
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[pdf_file] => patents/06/419/06419191.pdf
[firstpage_image] =>[orig_patent_app_number] => 09651557
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/651557 | Electrodynamic tether control | Aug 29, 2000 | Issued |
Array
(
[id] => 1558069
[patent_doc_number] => 06360990
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-26
[patent_title] => 'Landing gear'
[patent_app_type] => B1
[patent_app_number] => 09/651486
[patent_app_country] => US
[patent_app_date] => 2000-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 5606
[patent_no_of_claims] => 27
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[pdf_file] => patents/06/360/06360990.pdf
[firstpage_image] =>[orig_patent_app_number] => 09651486
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/651486 | Landing gear | Aug 29, 2000 | Issued |
Array
(
[id] => 4250716
[patent_doc_number] => 06305642
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-23
[patent_title] => 'Glider launching device'
[patent_app_type] => 1
[patent_app_number] => 9/649649
[patent_app_country] => US
[patent_app_date] => 2000-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/305/06305642.pdf
[firstpage_image] =>[orig_patent_app_number] => 649649
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/649649 | Glider launching device | Aug 28, 2000 | Issued |
Array
(
[id] => 4392167
[patent_doc_number] => 06264138
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-07-24
[patent_title] => 'Propeller gearbox'
[patent_app_type] => 1
[patent_app_number] => 9/650378
[patent_app_country] => US
[patent_app_date] => 2000-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/264/06264138.pdf
[firstpage_image] =>[orig_patent_app_number] => 650378
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/650378 | Propeller gearbox | Aug 28, 2000 | Issued |
Array
(
[id] => 7641514
[patent_doc_number] => 06394393
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-05-28
[patent_title] => 'Crashworthy aircraft seat'
[patent_app_type] => B1
[patent_app_number] => 09/648841
[patent_app_country] => US
[patent_app_date] => 2000-08-25
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/394/06394393.pdf
[firstpage_image] =>[orig_patent_app_number] => 09648841
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/648841 | Crashworthy aircraft seat | Aug 24, 2000 | Issued |
Array
(
[id] => 7636134
[patent_doc_number] => 06380526
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-04-30
[patent_title] => 'Employing booster trajectory in a payload inertial measurement unit'
[patent_app_type] => B1
[patent_app_number] => 09/644728
[patent_app_country] => US
[patent_app_date] => 2000-08-23
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/380/06380526.pdf
[firstpage_image] =>[orig_patent_app_number] => 09644728
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/644728 | Employing booster trajectory in a payload inertial measurement unit | Aug 22, 2000 | Issued |
Array
(
[id] => 4380958
[patent_doc_number] => 06296204
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-02
[patent_title] => 'Restraint system for a flight helmet'
[patent_app_type] => 1
[patent_app_number] => 9/644161
[patent_app_country] => US
[patent_app_date] => 2000-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/296/06296204.pdf
[firstpage_image] =>[orig_patent_app_number] => 644161
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/644161 | Restraint system for a flight helmet | Aug 21, 2000 | Issued |