
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] => 1577092
[patent_doc_number] => 06422513
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Inflatable restraint systems for ejection flight vests'
[patent_app_type] => B1
[patent_app_number] => 09/644162
[patent_app_country] => US
[patent_app_date] => 2000-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2786
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/422/06422513.pdf
[firstpage_image] =>[orig_patent_app_number] => 09644162
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/644162 | Inflatable restraint systems for ejection flight vests | Aug 21, 2000 | Issued |
Array
(
[id] => 1400839
[patent_doc_number] => 06513758
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-04
[patent_title] => 'High altitude platform control system'
[patent_app_type] => B1
[patent_app_number] => 09/644226
[patent_app_country] => US
[patent_app_date] => 2000-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1244
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/513/06513758.pdf
[firstpage_image] =>[orig_patent_app_number] => 09644226
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/644226 | High altitude platform control system | Aug 20, 2000 | Issued |
Array
(
[id] => 601483
[patent_doc_number] => 07431240
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2008-10-07
[patent_title] => 'Hybrid deicing system and method of operation'
[patent_app_type] => utility
[patent_app_number] => 09/640063
[patent_app_country] => US
[patent_app_date] => 2000-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 5130
[patent_no_of_claims] => 53
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/431/07431240.pdf
[firstpage_image] =>[orig_patent_app_number] => 09640063
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/640063 | Hybrid deicing system and method of operation | Aug 16, 2000 | Issued |
Array
(
[id] => 1301788
[patent_doc_number] => 06612398
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-09-02
[patent_title] => 'Methods for measurement, analysis and assessment of ground structure'
[patent_app_type] => B1
[patent_app_number] => 09/638681
[patent_app_country] => US
[patent_app_date] => 2000-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3673
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/612/06612398.pdf
[firstpage_image] =>[orig_patent_app_number] => 09638681
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/638681 | Methods for measurement, analysis and assessment of ground structure | Aug 14, 2000 | Issued |
Array
(
[id] => 1584320
[patent_doc_number] => 06481671
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-11-19
[patent_title] => 'Spacecraft sunshield for use in performing solar torque balancing'
[patent_app_type] => B1
[patent_app_number] => 09/638841
[patent_app_country] => US
[patent_app_date] => 2000-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 4724
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/481/06481671.pdf
[firstpage_image] =>[orig_patent_app_number] => 09638841
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/638841 | Spacecraft sunshield for use in performing solar torque balancing | Aug 13, 2000 | Issued |
Array
(
[id] => 4393384
[patent_doc_number] => 06299104
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-10-09
[patent_title] => 'Method and apparatus for evaluating parachutes under load'
[patent_app_type] => 1
[patent_app_number] => 9/631541
[patent_app_country] => US
[patent_app_date] => 2000-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 3671
[patent_no_of_claims] => 36
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/299/06299104.pdf
[firstpage_image] =>[orig_patent_app_number] => 631541
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/631541 | Method and apparatus for evaluating parachutes under load | Aug 2, 2000 | Issued |
Array
(
[id] => 4314079
[patent_doc_number] => 06330988
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-12-18
[patent_title] => 'System for star catalog equalization to enhance attitude determination'
[patent_app_type] => 1
[patent_app_number] => 9/628779
[patent_app_country] => US
[patent_app_date] => 2000-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3072
[patent_no_of_claims] => 21
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/330/06330988.pdf
[firstpage_image] =>[orig_patent_app_number] => 628779
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/628779 | System for star catalog equalization to enhance attitude determination | Jul 28, 2000 | Issued |
Array
(
[id] => 1550732
[patent_doc_number] => 06347770
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-02-19
[patent_title] => 'Dual-control stick for aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/625759
[patent_app_country] => US
[patent_app_date] => 2000-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 6789
[patent_no_of_claims] => 20
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[pdf_file] => patents/06/347/06347770.pdf
[firstpage_image] =>[orig_patent_app_number] => 09625759
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/625759 | Dual-control stick for aircraft | Jul 25, 2000 | Issued |
Array
(
[id] => 1577096
[patent_doc_number] => 06422514
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-07-23
[patent_title] => 'Common bulkhead cryogenic propellant tank'
[patent_app_type] => B1
[patent_app_number] => 09/626251
[patent_app_country] => US
[patent_app_date] => 2000-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2459
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[pdf_file] => patents/06/422/06422514.pdf
[firstpage_image] =>[orig_patent_app_number] => 09626251
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/626251 | Common bulkhead cryogenic propellant tank | Jul 25, 2000 | Issued |
Array
(
[id] => 1400797
[patent_doc_number] => 06513757
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-04
[patent_title] => 'Wing of composite material and method of fabricating the same'
[patent_app_type] => B1
[patent_app_number] => 09/616399
[patent_app_country] => US
[patent_app_date] => 2000-07-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 10132
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[pdf_file] => patents/06/513/06513757.pdf
[firstpage_image] =>[orig_patent_app_number] => 09616399
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/616399 | Wing of composite material and method of fabricating the same | Jul 13, 2000 | Issued |
Array
(
[id] => 1503072
[patent_doc_number] => 06439503
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-27
[patent_title] => 'Pulse detonation cluster engine'
[patent_app_type] => B1
[patent_app_number] => 09/612727
[patent_app_country] => US
[patent_app_date] => 2000-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => patents/06/439/06439503.pdf
[firstpage_image] =>[orig_patent_app_number] => 09612727
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/612727 | Pulse detonation cluster engine | Jul 9, 2000 | Issued |
Array
(
[id] => 1571082
[patent_doc_number] => 06467726
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-10-22
[patent_title] => 'Aircraft and torque transmission'
[patent_app_type] => B1
[patent_app_number] => 09/605411
[patent_app_country] => US
[patent_app_date] => 2000-06-28
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[pdf_file] => patents/06/467/06467726.pdf
[firstpage_image] =>[orig_patent_app_number] => 09605411
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/605411 | Aircraft and torque transmission | Jun 27, 2000 | Issued |
Array
(
[id] => 4254681
[patent_doc_number] => 06322021
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-11-27
[patent_title] => 'Deployable wing with propulsion for range extension'
[patent_app_type] => 1
[patent_app_number] => 9/593229
[patent_app_country] => US
[patent_app_date] => 2000-06-14
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[pdf_file] => patents/06/322/06322021.pdf
[firstpage_image] =>[orig_patent_app_number] => 593229
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/593229 | Deployable wing with propulsion for range extension | Jun 13, 2000 | Issued |
Array
(
[id] => 1446587
[patent_doc_number] => 06454209
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-24
[patent_title] => 'Comfort and illumination apparatus for a passenger space'
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[patent_app_number] => 09/591879
[patent_app_country] => US
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[pdf_file] => patents/06/454/06454209.pdf
[firstpage_image] =>[orig_patent_app_number] => 09591879
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/591879 | Comfort and illumination apparatus for a passenger space | Jun 11, 2000 | Issued |
Array
(
[id] => 1432845
[patent_doc_number] => 06340133
[patent_country] => US
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[patent_issue_date] => 2002-01-22
[patent_title] => 'System to transform a horizontal take-off and self-sustained horizontal flight airplane into self-sustained horizontal flight, vertical landing and take-off, hybrid integrated airplane'
[patent_app_type] => B1
[patent_app_number] => 09/581312
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Array
(
[id] => 1463401
[patent_doc_number] => 06457680
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[patent_issue_date] => 2002-10-01
[patent_title] => 'Auxiliary airfoil for aircraft main wings'
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[pdf_file] => patents/06/457/06457680.pdf
[firstpage_image] =>[orig_patent_app_number] => 09587279
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/587279 | Auxiliary airfoil for aircraft main wings | Jun 4, 2000 | Issued |
Array
(
[id] => 1429003
[patent_doc_number] => 06519307
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-02-11
[patent_title] => 'Ventilated overpack apparatus and method for storing spent nuclear fuel'
[patent_app_type] => B1
[patent_app_number] => 09/580407
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/580407 | Ventilated overpack apparatus and method for storing spent nuclear fuel | May 29, 2000 | Issued |
Array
(
[id] => 1473749
[patent_doc_number] => 06450452
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[patent_issue_date] => 2002-09-17
[patent_title] => 'Fly back booster'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/578321 | Fly back booster | May 23, 2000 | Issued |
Array
(
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[patent_title] => 'Regional aircraft boarding pier and method of using'
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[firstpage_image] =>[orig_patent_app_number] => 575222
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/575222 | Regional aircraft boarding pier and method of using | May 21, 2000 | Issued |
Array
(
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[pdf_file] => patents/06/364/06364251.pdf
[firstpage_image] =>[orig_patent_app_number] => 09574281
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/574281 | Airwing structure | May 18, 2000 | Issued |