Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 30 [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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 306 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 11 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 2409 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 432 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 79 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 1921 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 26 [patent_no_of_words] => 7125 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 20 [patent_no_of_words] => 4569 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2001-04-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 4075 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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' [patent_app_type] => new [patent_app_number] => 09/816439 [patent_app_country] => US [patent_app_date] => 2001-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2365 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0134/20020134890.pdf [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' [patent_app_type] => new [patent_app_number] => 09/813075 [patent_app_country] => US [patent_app_date] => 2001-03-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1641 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 50 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 8061 [patent_no_of_claims] => 34 [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/06/499/06499696.pdf [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' [patent_app_type] => new [patent_app_number] => 09/802754 [patent_app_country] => US [patent_app_date] => 2001-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 2214 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 21 [patent_words_short_claim] => 23 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0125/20020125365.pdf [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 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2001-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6143 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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
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