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
08/366821 FLUIDIC CONTROL THRUST VECTORING NOZZLE Dec 29, 1994 Abandoned
Array ( [id] => 3704810 [patent_doc_number] => 05615848 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-04-01 [patent_title] => 'Rescue and ambulance helicopter' [patent_app_type] => 1 [patent_app_number] => 8/363155 [patent_app_country] => US [patent_app_date] => 1994-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 11 [patent_no_of_words] => 2142 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/615/05615848.pdf [firstpage_image] =>[orig_patent_app_number] => 363155 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/363155
Rescue and ambulance helicopter Dec 22, 1994 Issued
Array ( [id] => 3575035 [patent_doc_number] => 05549258 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-08-27 [patent_title] => 'Retrofit luggage bin assembly compatible with existing aircraft bin supports' [patent_app_type] => 1 [patent_app_number] => 8/363765 [patent_app_country] => US [patent_app_date] => 1994-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3414 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 230 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/549/05549258.pdf [firstpage_image] =>[orig_patent_app_number] => 363765 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/363765
Retrofit luggage bin assembly compatible with existing aircraft bin supports Dec 22, 1994 Issued
Array ( [id] => 3717702 [patent_doc_number] => 05664743 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-09-09 [patent_title] => 'Device for gripping, guiding and transporting wheeled helicopters particularly for ship\'s decks' [patent_app_type] => 1 [patent_app_number] => 8/362154 [patent_app_country] => US [patent_app_date] => 1994-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 12 [patent_no_of_words] => 2282 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 280 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/664/05664743.pdf [firstpage_image] =>[orig_patent_app_number] => 362154 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/362154
Device for gripping, guiding and transporting wheeled helicopters particularly for ship's decks Dec 21, 1994 Issued
Array ( [id] => 3611820 [patent_doc_number] => 05607122 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-03-04 [patent_title] => 'Tail rotor authority control for a helicopter' [patent_app_type] => 1 [patent_app_number] => 8/362245 [patent_app_country] => US [patent_app_date] => 1994-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 30 [patent_no_of_words] => 14920 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/607/05607122.pdf [firstpage_image] =>[orig_patent_app_number] => 362245 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/362245
Tail rotor authority control for a helicopter Dec 21, 1994 Issued
Array ( [id] => 3611737 [patent_doc_number] => 05641123 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-06-24 [patent_title] => 'Expandable nozzle mechanism for a rocket engine' [patent_app_type] => 1 [patent_app_number] => 8/360421 [patent_app_country] => US [patent_app_date] => 1994-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 22 [patent_no_of_words] => 6594 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/641/05641123.pdf [firstpage_image] =>[orig_patent_app_number] => 360421 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/360421
Expandable nozzle mechanism for a rocket engine Dec 20, 1994 Issued
Array ( [id] => 3586750 [patent_doc_number] => 05558301 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-09-24 [patent_title] => 'Aircraft and in particular rotary-wing aircraft seat having an energy absorption device automatically adjustable as a function of the size of the occupant' [patent_app_type] => 1 [patent_app_number] => 8/360564 [patent_app_country] => US [patent_app_date] => 1994-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3713 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/558/05558301.pdf [firstpage_image] =>[orig_patent_app_number] => 360564 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/360564
Aircraft and in particular rotary-wing aircraft seat having an energy absorption device automatically adjustable as a function of the size of the occupant Dec 20, 1994 Issued
Array ( [id] => 3569298 [patent_doc_number] => 05580013 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-12-03 [patent_title] => 'Economical construction and assembly method for a modular permanent orbiting space station' [patent_app_type] => 1 [patent_app_number] => 8/359644 [patent_app_country] => US [patent_app_date] => 1994-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 28 [patent_no_of_words] => 4742 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 275 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/580/05580013.pdf [firstpage_image] =>[orig_patent_app_number] => 359644 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/359644
Economical construction and assembly method for a modular permanent orbiting space station Dec 19, 1994 Issued
Array ( [id] => 3575879 [patent_doc_number] => 05584447 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-12-17 [patent_title] => 'Noise control using a plate radiator and an acoustic resonator' [patent_app_type] => 1 [patent_app_number] => 8/359165 [patent_app_country] => US [patent_app_date] => 1994-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2982 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 208 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/584/05584447.pdf [firstpage_image] =>[orig_patent_app_number] => 359165 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/359165
Noise control using a plate radiator and an acoustic resonator Dec 18, 1994 Issued
Array ( [id] => 3654868 [patent_doc_number] => 05598990 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-02-04 [patent_title] => 'Supersonic vortex generator' [patent_app_type] => 1 [patent_app_number] => 8/356646 [patent_app_country] => US [patent_app_date] => 1994-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 19 [patent_no_of_words] => 5245 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 279 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/598/05598990.pdf [firstpage_image] =>[orig_patent_app_number] => 356646 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/356646
Supersonic vortex generator Dec 14, 1994 Issued
Array ( [id] => 3540752 [patent_doc_number] => 05573205 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-11-12 [patent_title] => 'Pull cord tension transmitting device using dual rack-pinion' [patent_app_type] => 1 [patent_app_number] => 8/352234 [patent_app_country] => US [patent_app_date] => 1994-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 1060 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 247 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/573/05573205.pdf [firstpage_image] =>[orig_patent_app_number] => 352234 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/352234
Pull cord tension transmitting device using dual rack-pinion Dec 7, 1994 Issued
Array ( [id] => 3608226 [patent_doc_number] => 05613651 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-03-25 [patent_title] => 'Landing gear axle steering without walking beam' [patent_app_type] => 1 [patent_app_number] => 8/352326 [patent_app_country] => US [patent_app_date] => 1994-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 610 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/613/05613651.pdf [firstpage_image] =>[orig_patent_app_number] => 352326 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/352326
Landing gear axle steering without walking beam Dec 7, 1994 Issued
Array ( [id] => 3609181 [patent_doc_number] => 05593112 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-01-14 [patent_title] => 'Nacelle air pump for vector nozzles for aircraft' [patent_app_type] => 1 [patent_app_number] => 8/349844 [patent_app_country] => US [patent_app_date] => 1994-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2160 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/593/05593112.pdf [firstpage_image] =>[orig_patent_app_number] => 349844 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/349844
Nacelle air pump for vector nozzles for aircraft Dec 5, 1994 Issued
Array ( [id] => 3586703 [patent_doc_number] => 05558298 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-09-24 [patent_title] => 'Active noise control of aircraft engine discrete tonal noise' [patent_app_type] => 1 [patent_app_number] => 8/349285 [patent_app_country] => US [patent_app_date] => 1994-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3049 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/558/05558298.pdf [firstpage_image] =>[orig_patent_app_number] => 349285 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/349285
Active noise control of aircraft engine discrete tonal noise Dec 4, 1994 Issued
08/350046 METHOD OF CONTROLLING A PLURALITY OF SATELLITES Nov 28, 1994 Abandoned
Array ( [id] => 3503266 [patent_doc_number] => 05575441 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-11-19 [patent_title] => 'Fuel liquid/vapor vent containment/recovery system' [patent_app_type] => 1 [patent_app_number] => 8/345182 [patent_app_country] => US [patent_app_date] => 1994-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 1469 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/575/05575441.pdf [firstpage_image] =>[orig_patent_app_number] => 345182 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/345182
Fuel liquid/vapor vent containment/recovery system Nov 27, 1994 Issued
Array ( [id] => 3503254 [patent_doc_number] => 05575440 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-11-19 [patent_title] => 'Procedure and devices to determine the severity of icing conditions for an aircraft' [patent_app_type] => 1 [patent_app_number] => 8/348086 [patent_app_country] => US [patent_app_date] => 1994-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2370 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/575/05575440.pdf [firstpage_image] =>[orig_patent_app_number] => 348086 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/348086
Procedure and devices to determine the severity of icing conditions for an aircraft Nov 24, 1994 Issued
Array ( [id] => 3503238 [patent_doc_number] => 05575439 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-11-19 [patent_title] => 'Fastening of a thermal insulation structure' [patent_app_type] => 1 [patent_app_number] => 8/344112 [patent_app_country] => US [patent_app_date] => 1994-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3051 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 267 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/575/05575439.pdf [firstpage_image] =>[orig_patent_app_number] => 344112 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/344112
Fastening of a thermal insulation structure Nov 22, 1994 Issued
Array ( [id] => 3645741 [patent_doc_number] => 05626310 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-05-06 [patent_title] => 'Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft' [patent_app_type] => 1 [patent_app_number] => 8/342596 [patent_app_country] => US [patent_app_date] => 1994-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 15 [patent_no_of_words] => 5578 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/626/05626310.pdf [firstpage_image] =>[orig_patent_app_number] => 342596 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/342596
Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft Nov 20, 1994 Issued
Array ( [id] => 3538738 [patent_doc_number] => 05547148 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1996-08-20 [patent_title] => 'Crashworthy landing gear' [patent_app_type] => 1 [patent_app_number] => 8/341786 [patent_app_country] => US [patent_app_date] => 1994-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 5103 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 349 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/547/05547148.pdf [firstpage_image] =>[orig_patent_app_number] => 341786 [rel_patent_id] =>[rel_patent_doc_number] =>)
08/341786
Crashworthy landing gear Nov 17, 1994 Issued
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