
Amanda Lee Bailey
Examiner (ID: 4785)
| Most Active Art Unit | 3673 |
| Art Unit(s) | 3673 |
| Total Applications | 468 |
| Issued Applications | 245 |
| Pending Applications | 48 |
| Abandoned Applications | 191 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6747842
[patent_doc_number] => 20030042362
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-06
[patent_title] => 'Remediation of fan source production of smoke in an aircraft cabin'
[patent_app_type] => new
[patent_app_number] => 10/222494
[patent_app_country] => US
[patent_app_date] => 2002-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1640
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0042/20030042362.pdf
[firstpage_image] =>[orig_patent_app_number] => 10222494
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/222494 | Remediation of fan source production of smoke in an aircraft cabin | Aug 14, 2002 | Issued |
Array
(
[id] => 7367763
[patent_doc_number] => 20040026567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-12
[patent_title] => 'Fluid delivery system for heat exchange garments'
[patent_app_type] => new
[patent_app_number] => 10/215428
[patent_app_country] => US
[patent_app_date] => 2002-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 8663
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0026/20040026567.pdf
[firstpage_image] =>[orig_patent_app_number] => 10215428
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/215428 | Fluid delivery system for heat exchange garments | Aug 8, 2002 | Abandoned |
Array
(
[id] => 6713685
[patent_doc_number] => 20030025033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-06
[patent_title] => 'Device for the attachment of an engine to an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/208884
[patent_app_country] => US
[patent_app_date] => 2002-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4126
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20030025033.pdf
[firstpage_image] =>[orig_patent_app_number] => 10208884
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/208884 | Device for the attachment of an engine to an aircraft | Jul 28, 2002 | Issued |
Array
(
[id] => 7387610
[patent_doc_number] => 20040016847
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-29
[patent_title] => 'Luggage bins and aircraft passenger cabin ceilings'
[patent_app_type] => new
[patent_app_number] => 10/206777
[patent_app_country] => US
[patent_app_date] => 2002-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5237
[patent_no_of_claims] => 102
[patent_no_of_ind_claims] => 10
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0016/20040016847.pdf
[firstpage_image] =>[orig_patent_app_number] => 10206777
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/206777 | Luggage bins and aircraft passenger cabin ceilings | Jul 25, 2002 | Issued |
Array
(
[id] => 7387620
[patent_doc_number] => 20040016848
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-29
[patent_title] => 'STORE EJECTION SYSTEM WITH REPLACEABLE PRESSURE VESSEL'
[patent_app_type] => new
[patent_app_number] => 10/205570
[patent_app_country] => US
[patent_app_date] => 2002-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5452
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 156
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0016/20040016848.pdf
[firstpage_image] =>[orig_patent_app_number] => 10205570
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/205570 | Store ejection system with replaceable pressure vessel | Jul 24, 2002 | Issued |
Array
(
[id] => 1102300
[patent_doc_number] => 06811122
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-11-02
[patent_title] => 'Flame arrestor to cover aircraft engines'
[patent_app_type] => B2
[patent_app_number] => 10/201763
[patent_app_country] => US
[patent_app_date] => 2002-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1868
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 307
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/811/06811122.pdf
[firstpage_image] =>[orig_patent_app_number] => 10201763
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/201763 | Flame arrestor to cover aircraft engines | Jul 22, 2002 | Issued |
Array
(
[id] => 7387633
[patent_doc_number] => 20040016852
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-29
[patent_title] => 'System and methods for integrating a payload with a launch vehicle'
[patent_app_type] => new
[patent_app_number] => 10/201620
[patent_app_country] => US
[patent_app_date] => 2002-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4103
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 48
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0016/20040016852.pdf
[firstpage_image] =>[orig_patent_app_number] => 10201620
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/201620 | System and methods for integrating a payload with a launch vehicle | Jul 22, 2002 | Issued |
Array
(
[id] => 7347787
[patent_doc_number] => 20040011921
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-22
[patent_title] => 'Rotopter hovering and flying by means of circulating wings'
[patent_app_type] => new
[patent_app_number] => 10/199069
[patent_app_country] => US
[patent_app_date] => 2002-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4984
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 15
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0011/20040011921.pdf
[firstpage_image] =>[orig_patent_app_number] => 10199069
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/199069 | Rotopter hovering and flying by means of circulating wings | Jul 21, 2002 | Abandoned |
Array
(
[id] => 6840994
[patent_doc_number] => 20030146341
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-07
[patent_title] => 'Shock ( Wave) Absorber'
[patent_app_type] => new
[patent_app_number] => 10/198369
[patent_app_country] => US
[patent_app_date] => 2002-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 242
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 34
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0146/20030146341.pdf
[firstpage_image] =>[orig_patent_app_number] => 10198369
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/198369 | Shock ( Wave) Absorber | Jul 17, 2002 | Abandoned |
Array
(
[id] => 7259279
[patent_doc_number] => 20040149858
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-05
[patent_title] => 'Airplane security system'
[patent_app_type] => new
[patent_app_number] => 10/196700
[patent_app_country] => US
[patent_app_date] => 2002-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2912
[patent_no_of_claims] => 48
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 32
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0149/20040149858.pdf
[firstpage_image] =>[orig_patent_app_number] => 10196700
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/196700 | Airplane security system | Jul 15, 2002 | Abandoned |
Array
(
[id] => 1084592
[patent_doc_number] => 06830214
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-12-14
[patent_title] => 'Rotary-wing aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/194672
[patent_app_country] => US
[patent_app_date] => 2002-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 6247
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 190
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/830/06830214.pdf
[firstpage_image] =>[orig_patent_app_number] => 10194672
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/194672 | Rotary-wing aircraft | Jul 11, 2002 | Issued |
Array
(
[id] => 7420648
[patent_doc_number] => 20040000614
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-01
[patent_title] => 'Method and apparatus for lifting and propelling rotorcraft'
[patent_app_type] => new
[patent_app_number] => 10/184240
[patent_app_country] => US
[patent_app_date] => 2002-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1166
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0000/20040000614.pdf
[firstpage_image] =>[orig_patent_app_number] => 10184240
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/184240 | Method and apparatus for lifting and propelling rotorcraft | Jun 26, 2002 | Abandoned |
Array
(
[id] => 6823702
[patent_doc_number] => 20030234323
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-25
[patent_title] => 'Evacuation slide having trapezoidal outline'
[patent_app_type] => new
[patent_app_number] => 10/177190
[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] => 1629
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 229
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0234/20030234323.pdf
[firstpage_image] =>[orig_patent_app_number] => 10177190
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/177190 | Evacuation slide having trapezoidal outline | Jun 20, 2002 | Issued |
Array
(
[id] => 6316457
[patent_doc_number] => 20020195520
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-26
[patent_title] => 'Missile spiralling mechanism -2'
[patent_app_type] => new
[patent_app_number] => 10/173633
[patent_app_country] => US
[patent_app_date] => 2002-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 21
[patent_no_of_words] => 3140
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20020195520.pdf
[firstpage_image] =>[orig_patent_app_number] => 10173633
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/173633 | Missile spiralling mechanism -2 | Jun 18, 2002 | Abandoned |
Array
(
[id] => 6753268
[patent_doc_number] => 20030001044
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-02
[patent_title] => 'Hybrid air vehicle'
[patent_app_type] => new
[patent_app_number] => 10/175237
[patent_app_country] => US
[patent_app_date] => 2002-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3058
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 23
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0001/20030001044.pdf
[firstpage_image] =>[orig_patent_app_number] => 10175237
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/175237 | Hybrid air vehicle having air cushion landing gear | Jun 17, 2002 | Issued |
Array
(
[id] => 7967553
[patent_doc_number] => 06679458
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-20
[patent_title] => 'Split detent tactile cueing vehicle control system'
[patent_app_type] => B2
[patent_app_number] => 10/166796
[patent_app_country] => US
[patent_app_date] => 2002-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 4192
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/679/06679458.pdf
[firstpage_image] =>[orig_patent_app_number] => 10166796
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/166796 | Split detent tactile cueing vehicle control system | Jun 9, 2002 | Issued |
Array
(
[id] => 6794583
[patent_doc_number] => 20030173456
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'DEVICE FOR RECOVERY OF FORCES GENERATED BY AN AIRCRAFT ENGINE'
[patent_app_type] => new
[patent_app_number] => 10/165563
[patent_app_country] => US
[patent_app_date] => 2002-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2496
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 90
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173456.pdf
[firstpage_image] =>[orig_patent_app_number] => 10165563
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/165563 | Device for recovery of forces generated by an aircraft engine | Jun 6, 2002 | Issued |
Array
(
[id] => 6699299
[patent_doc_number] => 20030222179
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-04
[patent_title] => 'METHOD AND SYSTEM FOR CONTROLLING THE ECCENTRICITY OF A NEAR-CIRCULAR ORBIT'
[patent_app_type] => new
[patent_app_number] => 10/162484
[patent_app_country] => US
[patent_app_date] => 2002-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3275
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 42
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0222/20030222179.pdf
[firstpage_image] =>[orig_patent_app_number] => 10162484
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/162484 | Method and system for controlling the eccentricity of a near-circular orbit | Jun 2, 2002 | Issued |
Array
(
[id] => 1334909
[patent_doc_number] => 06581877
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-06-24
[patent_title] => 'Aircraft with ventral fairing and seal for such an aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/158008
[patent_app_country] => US
[patent_app_date] => 2002-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2272
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/581/06581877.pdf
[firstpage_image] =>[orig_patent_app_number] => 10158008
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/158008 | Aircraft with ventral fairing and seal for such an aircraft | May 30, 2002 | Issued |
Array
(
[id] => 6699290
[patent_doc_number] => 20030222170
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-04
[patent_title] => 'Derivative aircraft and methods for their manufacture'
[patent_app_type] => new
[patent_app_number] => 10/160363
[patent_app_country] => US
[patent_app_date] => 2002-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5684
[patent_no_of_claims] => 69
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0222/20030222170.pdf
[firstpage_image] =>[orig_patent_app_number] => 10160363
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/160363 | Derivative aircraft and methods for their manufacture | May 30, 2002 | Issued |