
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] => 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
[patent_figures_cnt] => 4
[patent_no_of_words] => 3615
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 9
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[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
[patent_effective_date] => 0000-00-00
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[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] => 1432845
[patent_doc_number] => 06340133
[patent_country] => US
[patent_kind] => B1
[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
[patent_app_country] => US
[patent_app_date] => 2000-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => patents/06/340/06340133.pdf
[firstpage_image] =>[orig_patent_app_number] => 09581312
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/581312 | 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 | Jun 11, 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'
[patent_app_type] => B1
[patent_app_number] => 09/591879
[patent_app_country] => US
[patent_app_date] => 2000-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[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] => 1463401
[patent_doc_number] => 06457680
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-10-01
[patent_title] => 'Auxiliary airfoil for aircraft main wings'
[patent_app_type] => B1
[patent_app_number] => 09/587279
[patent_app_country] => US
[patent_app_date] => 2000-06-05
[patent_effective_date] => 0000-00-00
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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
[patent_app_country] => US
[patent_app_date] => 2000-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => patents/06/519/06519307.pdf
[firstpage_image] =>[orig_patent_app_number] => 09580407
[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
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-17
[patent_title] => 'Fly back booster'
[patent_app_type] => B1
[patent_app_number] => 09/578321
[patent_app_country] => US
[patent_app_date] => 2000-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => patents/06/450/06450452.pdf
[firstpage_image] =>[orig_patent_app_number] => 09578321
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/578321 | Fly back booster | May 23, 2000 | Issued |
Array
(
[id] => 4294003
[patent_doc_number] => 06315243
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-11-13
[patent_title] => 'Regional aircraft boarding pier and method of using'
[patent_app_type] => 1
[patent_app_number] => 9/575222
[patent_app_country] => US
[patent_app_date] => 2000-05-22
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/315/06315243.pdf
[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
(
[id] => 1480821
[patent_doc_number] => 06364251
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-04-02
[patent_title] => 'Airwing structure'
[patent_app_type] => B1
[patent_app_number] => 09/574281
[patent_app_country] => US
[patent_app_date] => 2000-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
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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 |
Array
(
[id] => 1562697
[patent_doc_number] => 06338454
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-01-15
[patent_title] => 'Aircraft flight control device'
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[firstpage_image] =>[orig_patent_app_number] => 09572439
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/572439 | Aircraft flight control device | May 16, 2000 | Issued |
Array
(
[id] => 4409798
[patent_doc_number] => 06176452
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 2001-01-23
[patent_title] => 'Hybrid fuel containment structure'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/564185 | Hybrid fuel containment structure | May 3, 2000 | Issued |
Array
(
[id] => 1480833
[patent_doc_number] => 06364253
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-04-02
[patent_title] => 'Remote piloted vehicle powered by beamed radiation'
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[firstpage_image] =>[orig_patent_app_number] => 09558999
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/558999 | Remote piloted vehicle powered by beamed radiation | Apr 24, 2000 | Issued |
Array
(
[id] => 1546769
[patent_doc_number] => 06345787
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[patent_title] => 'Aircraft landing gear'
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[firstpage_image] =>[orig_patent_app_number] => 09529381
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/529381 | Aircraft landing gear | Apr 12, 2000 | Issued |
Array
(
[id] => 4350288
[patent_doc_number] => 06273369
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[patent_issue_date] => 2001-08-14
[patent_title] => 'Kite control and quick release system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/545999 | Kite control and quick release system | Apr 9, 2000 | Issued |
Array
(
[id] => 4364574
[patent_doc_number] => 06260809
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[patent_title] => 'Ovate loop for rotary-wing blades'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/543869 | Ovate loop for rotary-wing blades | Apr 4, 2000 | Issued |
Array
(
[id] => 1558065
[patent_doc_number] => 06360988
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[patent_issue_date] => 2002-03-26
[patent_title] => 'Personnel lift device and amusement use thereof'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/542725 | Personnel lift device and amusement use thereof | Apr 3, 2000 | Issued |
Array
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Array
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Array
(
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[patent_title] => 'Method and apparatus for building a metal/composite hybrid airplane component'
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[firstpage_image] =>[orig_patent_app_number] => 09521910
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/521910 | Method and apparatus for building a metal/composite hybrid airplane component | Mar 8, 2000 | Issued |