
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] => 4138827
[patent_doc_number] => 06123296
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-09-26
[patent_title] => 'Self-actuated flow control system'
[patent_app_type] => 1
[patent_app_number] => 9/082995
[patent_app_country] => US
[patent_app_date] => 1998-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 3192
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/123/06123296.pdf
[firstpage_image] =>[orig_patent_app_number] => 082995
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/082995 | Self-actuated flow control system | May 20, 1998 | Issued |
Array
(
[id] => 1522305
[patent_doc_number] => 06352222
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-03-05
[patent_title] => 'Satellite, satellite control method and satellite communication system'
[patent_app_type] => B1
[patent_app_number] => 09/081551
[patent_app_country] => US
[patent_app_date] => 1998-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 19
[patent_no_of_words] => 17426
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/352/06352222.pdf
[firstpage_image] =>[orig_patent_app_number] => 09081551
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/081551 | Satellite, satellite control method and satellite communication system | May 19, 1998 | Issued |
Array
(
[id] => 4113525
[patent_doc_number] => 06145787
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-11-14
[patent_title] => 'Device and method for heating and deicing wind energy turbine blades'
[patent_app_type] => 1
[patent_app_number] => 9/082079
[patent_app_country] => US
[patent_app_date] => 1998-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 5114
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/145/06145787.pdf
[firstpage_image] =>[orig_patent_app_number] => 082079
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/082079 | Device and method for heating and deicing wind energy turbine blades | May 19, 1998 | Issued |
Array
(
[id] => 4007321
[patent_doc_number] => 05906191
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-05-25
[patent_title] => 'Compressed gas-operated shooting weapon'
[patent_app_type] => 1
[patent_app_number] => 9/068709
[patent_app_country] => US
[patent_app_date] => 1998-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3204
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 224
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/906/05906191.pdf
[firstpage_image] =>[orig_patent_app_number] => 068709
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/068709 | Compressed gas-operated shooting weapon | May 13, 1998 | Issued |
Array
(
[id] => 4167575
[patent_doc_number] => 06019316
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-02-01
[patent_title] => 'Device for suspending an aircraft tank'
[patent_app_type] => 1
[patent_app_number] => 9/078269
[patent_app_country] => US
[patent_app_date] => 1998-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 2262
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 137
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/019/06019316.pdf
[firstpage_image] =>[orig_patent_app_number] => 078269
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/078269 | Device for suspending an aircraft tank | May 12, 1998 | Issued |
Array
(
[id] => 4054826
[patent_doc_number] => 06067975
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-05-30
[patent_title] => 'Pulsating toy gun having reciprocating barrels'
[patent_app_type] => 1
[patent_app_number] => 9/073225
[patent_app_country] => US
[patent_app_date] => 1998-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 3043
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/067/06067975.pdf
[firstpage_image] =>[orig_patent_app_number] => 073225
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/073225 | Pulsating toy gun having reciprocating barrels | May 4, 1998 | Issued |
| 09/068206 | SUPERSONIC AIRCRAFT | May 1, 1998 | Abandoned |
Array
(
[id] => 3924081
[patent_doc_number] => 05996933
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-12-07
[patent_title] => 'Aircraft'
[patent_app_type] => 1
[patent_app_number] => 9/068067
[patent_app_country] => US
[patent_app_date] => 1998-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 3356
[patent_no_of_claims] => 11
[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/05/996/05996933.pdf
[firstpage_image] =>[orig_patent_app_number] => 068067
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/068067 | Aircraft | Apr 27, 1998 | Issued |
| 09/064336 | EMERGENCY EXIT INDICATOR | Apr 21, 1998 | Abandoned |
Array
(
[id] => 3903443
[patent_doc_number] => 05944006
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-31
[patent_title] => 'Toy gun with a selectively extendable barrel'
[patent_app_type] => 1
[patent_app_number] => 9/058626
[patent_app_country] => US
[patent_app_date] => 1998-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 12
[patent_no_of_words] => 4236
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/944/05944006.pdf
[firstpage_image] =>[orig_patent_app_number] => 058626
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/058626 | Toy gun with a selectively extendable barrel | Apr 8, 1998 | Issued |
Array
(
[id] => 3914483
[patent_doc_number] => 05988152
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-23
[patent_title] => 'Toy gun for sequentially firing a plurality of projectiles'
[patent_app_type] => 1
[patent_app_number] => 9/053483
[patent_app_country] => US
[patent_app_date] => 1998-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 3590
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/988/05988152.pdf
[firstpage_image] =>[orig_patent_app_number] => 053483
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/053483 | Toy gun for sequentially firing a plurality of projectiles | Mar 31, 1998 | Issued |
Array
(
[id] => 712441
[patent_doc_number] => 07051982
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-05-30
[patent_title] => 'Fairing arrangements for aircraft'
[patent_app_type] => utility
[patent_app_number] => 09/048838
[patent_app_country] => US
[patent_app_date] => 1998-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 12
[patent_no_of_words] => 2535
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/051/07051982.pdf
[firstpage_image] =>[orig_patent_app_number] => 09048838
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/048838 | Fairing arrangements for aircraft | Mar 26, 1998 | Issued |
Array
(
[id] => 4062879
[patent_doc_number] => 06053157
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-04-25
[patent_title] => 'Fluid propulsion device for use in a projectile launching system'
[patent_app_type] => 1
[patent_app_number] => 9/049658
[patent_app_country] => US
[patent_app_date] => 1998-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4092
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/053/06053157.pdf
[firstpage_image] =>[orig_patent_app_number] => 049658
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/049658 | Fluid propulsion device for use in a projectile launching system | Mar 22, 1998 | Issued |
Array
(
[id] => 4394300
[patent_doc_number] => 06308916
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-30
[patent_title] => 'Dual mode positioner for an aircraft landing gear axle beam'
[patent_app_type] => 1
[patent_app_number] => 9/044359
[patent_app_country] => US
[patent_app_date] => 1998-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2908
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/308/06308916.pdf
[firstpage_image] =>[orig_patent_app_number] => 044359
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/044359 | Dual mode positioner for an aircraft landing gear axle beam | Mar 18, 1998 | Issued |
Array
(
[id] => 3921514
[patent_doc_number] => 05975468
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-11-02
[patent_title] => 'Rotary actuator using shape memory'
[patent_app_type] => 1
[patent_app_number] => 9/042532
[patent_app_country] => US
[patent_app_date] => 1998-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2398
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/975/05975468.pdf
[firstpage_image] =>[orig_patent_app_number] => 042532
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/042532 | Rotary actuator using shape memory | Mar 16, 1998 | Issued |
Array
(
[id] => 3978076
[patent_doc_number] => 05909860
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-06-08
[patent_title] => 'Deployment sequencer'
[patent_app_type] => 1
[patent_app_number] => 9/031310
[patent_app_country] => US
[patent_app_date] => 1998-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4030
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/909/05909860.pdf
[firstpage_image] =>[orig_patent_app_number] => 031310
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/031310 | Deployment sequencer | Feb 25, 1998 | Issued |
Array
(
[id] => 4204737
[patent_doc_number] => 06039288
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-03-21
[patent_title] => 'Floor unit'
[patent_app_type] => 1
[patent_app_number] => 9/030753
[patent_app_country] => US
[patent_app_date] => 1998-02-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/039/06039288.pdf
[firstpage_image] =>[orig_patent_app_number] => 030753
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/030753 | Floor unit | Feb 24, 1998 | Issued |
Array
(
[id] => 4166383
[patent_doc_number] => 06158693
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2000-12-12
[patent_title] => 'Recoverable booster stage and recovery method'
[patent_app_type] => 1
[patent_app_number] => 9/030724
[patent_app_country] => US
[patent_app_date] => 1998-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/158/06158693.pdf
[firstpage_image] =>[orig_patent_app_number] => 030724
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/030724 | Recoverable booster stage and recovery method | Feb 24, 1998 | Issued |
| 90/004923 | SYSTEM AND METHOD FOR INDIRECTLY DETERMINING INCLINATION AT THE BIT | Feb 19, 1998 | Issued |
Array
(
[id] => 3932386
[patent_doc_number] => 05954296
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-09-21
[patent_title] => 'Aircraft canopy fracture system'
[patent_app_type] => 1
[patent_app_number] => 9/025479
[patent_app_country] => US
[patent_app_date] => 1998-02-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/954/05954296.pdf
[firstpage_image] =>[orig_patent_app_number] => 025479
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/025479 | Aircraft canopy fracture system | Feb 17, 1998 | Issued |