
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] => 6920503
[patent_doc_number] => 20010028020
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-10-11
[patent_title] => 'High-energy to low-energy orbit transfer vehicle'
[patent_app_type] => new
[patent_app_number] => 09/880605
[patent_app_country] => US
[patent_app_date] => 2001-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2929
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 98
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0028/20010028020.pdf
[firstpage_image] =>[orig_patent_app_number] => 09880605
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/880605 | High-energy to low-energy orbit transfer vehicle | Jun 12, 2001 | Issued |
Array
(
[id] => 6878977
[patent_doc_number] => 20010030262
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-10-18
[patent_title] => 'Soft link for connecting a group of parachute suspension lines to harness via risers'
[patent_app_type] => new
[patent_app_number] => 09/879419
[patent_app_country] => US
[patent_app_date] => 2001-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2126
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0030/20010030262.pdf
[firstpage_image] =>[orig_patent_app_number] => 09879419
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/879419 | Soft link for connecting a group of parachute suspension lines to harness via risers | Jun 11, 2001 | Abandoned |
Array
(
[id] => 1483894
[patent_doc_number] => 06427946
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-08-06
[patent_title] => 'Systems and methods for modifying ice adhesion strength'
[patent_app_type] => B1
[patent_app_number] => 09/857952
[patent_app_country] => US
[patent_app_date] => 2001-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 14
[patent_no_of_words] => 11355
[patent_no_of_claims] => 13
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/427/06427946.pdf
[firstpage_image] =>[orig_patent_app_number] => 09857952
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/857952 | Systems and methods for modifying ice adhesion strength | Jun 11, 2001 | Issued |
Array
(
[id] => 1473727
[patent_doc_number] => 06450446
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-09-17
[patent_title] => 'Counter rotating circular wing for aircraft'
[patent_app_type] => B1
[patent_app_number] => 09/875391
[patent_app_country] => US
[patent_app_date] => 2001-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 3211
[patent_no_of_claims] => 15
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/450/06450446.pdf
[firstpage_image] =>[orig_patent_app_number] => 09875391
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/875391 | Counter rotating circular wing for aircraft | Jun 4, 2001 | Issued |
Array
(
[id] => 6382499
[patent_doc_number] => 20020179770
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-05
[patent_title] => 'Flat balloon'
[patent_app_type] => new
[patent_app_number] => 09/681769
[patent_app_country] => US
[patent_app_date] => 2001-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 977
[patent_no_of_claims] => 18
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20020179770.pdf
[firstpage_image] =>[orig_patent_app_number] => 09681769
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/681769 | Flat balloon | May 31, 2001 | Abandoned |
Array
(
[id] => 1296831
[patent_doc_number] => 06619585
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-09-16
[patent_title] => 'Helicopter single-blade rotor'
[patent_app_type] => B1
[patent_app_number] => 09/857140
[patent_app_country] => US
[patent_app_date] => 2001-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2409
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/619/06619585.pdf
[firstpage_image] =>[orig_patent_app_number] => 09857140
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/857140 | Helicopter single-blade rotor | May 31, 2001 | Issued |
Array
(
[id] => 1311940
[patent_doc_number] => 06604710
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-08-12
[patent_title] => 'Light aircraft fuselage and structural frame connectors'
[patent_app_type] => B2
[patent_app_number] => 09/866246
[patent_app_country] => US
[patent_app_date] => 2001-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 21
[patent_no_of_words] => 5189
[patent_no_of_claims] => 33
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/604/06604710.pdf
[firstpage_image] =>[orig_patent_app_number] => 09866246
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/866246 | Light aircraft fuselage and structural frame connectors | May 28, 2001 | Issued |
Array
(
[id] => 1072795
[patent_doc_number] => 06837457
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-01-04
[patent_title] => 'Aircraft rotor and aircraft'
[patent_app_type] => utility
[patent_app_number] => 09/865540
[patent_app_country] => US
[patent_app_date] => 2001-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 28
[patent_no_of_words] => 6432
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/837/06837457.pdf
[firstpage_image] =>[orig_patent_app_number] => 09865540
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/865540 | Aircraft rotor and aircraft | May 28, 2001 | Issued |
Array
(
[id] => 6382533
[patent_doc_number] => 20020179774
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-05
[patent_title] => 'Clustered parachutes'
[patent_app_type] => new
[patent_app_number] => 09/867246
[patent_app_country] => US
[patent_app_date] => 2001-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2127
[patent_no_of_claims] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20020179774.pdf
[firstpage_image] =>[orig_patent_app_number] => 09867246
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/867246 | Method for providing gliding and trajectory control of a parachute cluster assembly | May 28, 2001 | Issued |
Array
(
[id] => 7063331
[patent_doc_number] => 20010042811
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2001-11-22
[patent_title] => 'Actuator apparatus, in particular for an aircraft flight control'
[patent_app_type] => new
[patent_app_number] => 09/860941
[patent_app_country] => US
[patent_app_date] => 2001-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2168
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0042/20010042811.pdf
[firstpage_image] =>[orig_patent_app_number] => 09860941
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/860941 | Actuator apparatus, in particular for an aircraft flight control | May 17, 2001 | Issued |
Array
(
[id] => 1309010
[patent_doc_number] => 06607168
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-08-19
[patent_title] => 'Bearing structure with reduced tip vortex'
[patent_app_type] => B1
[patent_app_number] => 09/787273
[patent_app_country] => US
[patent_app_date] => 2001-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 1921
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/607/06607168.pdf
[firstpage_image] =>[orig_patent_app_number] => 09787273
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/787273 | Bearing structure with reduced tip vortex | May 15, 2001 | Issued |
Array
(
[id] => 815947
[patent_doc_number] => 07410123
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-08-12
[patent_title] => 'Aircraft and hybrid with magnetic airfoil suspension and drive'
[patent_app_type] => utility
[patent_app_number] => 10/276884
[patent_app_country] => US
[patent_app_date] => 2001-05-15
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/410/07410123.pdf
[firstpage_image] =>[orig_patent_app_number] => 10276884
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/276884 | Aircraft and hybrid with magnetic airfoil suspension and drive | May 14, 2001 | Issued |
Array
(
[id] => 1213378
[patent_doc_number] => 06705569
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-03-16
[patent_title] => 'Axi-symmetric mixed compression inlet with variable geometry centerbody'
[patent_app_type] => B1
[patent_app_number] => 09/852129
[patent_app_country] => US
[patent_app_date] => 2001-05-09
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[pdf_file] => patents/06/705/06705569.pdf
[firstpage_image] =>[orig_patent_app_number] => 09852129
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/852129 | Axi-symmetric mixed compression inlet with variable geometry centerbody | May 8, 2001 | Issued |
Array
(
[id] => 1190646
[patent_doc_number] => 06729580
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-05-04
[patent_title] => 'Method and system for directing an object using gyroscopes'
[patent_app_type] => B2
[patent_app_number] => 09/828639
[patent_app_country] => US
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[patent_no_of_words] => 4075
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/729/06729580.pdf
[firstpage_image] =>[orig_patent_app_number] => 09828639
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/828639 | Method and system for directing an object using gyroscopes | Apr 4, 2001 | Issued |
| 09/720540 | Device and method for the targeted placement or reception of goods carried by aircraft | Mar 25, 2001 | Abandoned |
Array
(
[id] => 6505183
[patent_doc_number] => 20020134890
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-26
[patent_title] => 'Parachute with a controlled active lift'
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[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 09816439
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/816439 | Parachute with a controlled active lift | Mar 25, 2001 | Abandoned |
Array
(
[id] => 6716304
[patent_doc_number] => 20030027652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-06
[patent_title] => 'Portable balloon launcher system'
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[patent_app_number] => 09/813075
[patent_app_country] => US
[patent_app_date] => 2001-03-20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0027/20030027652.pdf
[firstpage_image] =>[orig_patent_app_number] => 09813075
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/813075 | Portable balloon launcher system | Mar 19, 2001 | Abandoned |
Array
(
[id] => 1514368
[patent_doc_number] => 06499696
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-12-31
[patent_title] => 'Rocket engine with reduced thrust and stagable venting system'
[patent_app_type] => B1
[patent_app_number] => 09/810850
[patent_app_country] => US
[patent_app_date] => 2001-03-16
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 09810850
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/810850 | Rocket engine with reduced thrust and stagable venting system | Mar 15, 2001 | Issued |
Array
(
[id] => 6413782
[patent_doc_number] => 20020125365
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-12
[patent_title] => 'Personal flight system'
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[firstpage_image] =>[orig_patent_app_number] => 09802754
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/802754 | Personal flight system | Mar 8, 2001 | Abandoned |
Array
(
[id] => 5856105
[patent_doc_number] => 20020121572
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[patent_kind] => A1
[patent_issue_date] => 2002-09-05
[patent_title] => 'INTEGRATED SYSTEM FOR PROVINDING 3-AXIS ATTITUDE-CONTROL, ENERGY-STORAGE, AND ELECTRICAL POWER'
[patent_app_type] => new
[patent_app_number] => 09/797241
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[pdf_file] => publications/A1/0121/20020121572.pdf
[firstpage_image] =>[orig_patent_app_number] => 09797241
[rel_patent_id] =>[rel_patent_doc_number] =>) 09/797241 | Integrated system for providing 3-axis attitude-control, energy-storage, and electrical power | Feb 26, 2001 | Issued |