Robert P. Swiatek

Array ( [id] => 4253221 [patent_doc_number] => 06244537 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-06-12 [patent_title] => 'Apparatus for operating a wing in three modes and system of use' [patent_app_type] => 1 [patent_app_number] => 9/247423 [patent_app_country] => US [patent_app_date] => 1999-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 4715 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/244/06244537.pdf [firstpage_image] =>[orig_patent_app_number] => 247423 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4338678 [patent_doc_number] => 06199797 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-03-13 [patent_title] => 'Aircraft float and system utilizing the same' [patent_app_type] => 1 [patent_app_number] => 9/247226 [patent_app_country] => US [patent_app_date] => 1999-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2476 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/199/06199797.pdf [firstpage_image] =>[orig_patent_app_number] => 247226 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4334561 [patent_doc_number] => 06216981 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-17 [patent_title] => 'Environmental control system' [patent_app_type] => 1 [patent_app_number] => 9/246846 [patent_app_country] => US [patent_app_date] => 1999-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1957 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/216/06216981.pdf [firstpage_image] =>[orig_patent_app_number] => 246846 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4070459 [patent_doc_number] => 06161802 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-12-19 [patent_title] => 'Trapped vortex airfoil nose' [patent_app_type] => 1 [patent_app_number] => 9/250220 [patent_app_country] => US [patent_app_date] => 1999-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2130 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/161/06161802.pdf [firstpage_image] =>[orig_patent_app_number] => 250220 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4329116 [patent_doc_number] => 06213428 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-10 [patent_title] => 'Aircraft fore structure' [patent_app_type] => 1 [patent_app_number] => 9/245842 [patent_app_country] => US [patent_app_date] => 1999-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2703 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/213/06213428.pdf [firstpage_image] =>[orig_patent_app_number] => 245842 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4310030 [patent_doc_number] => 06318668 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-11-20 [patent_title] => 'Thrust vectoring techniques' [patent_app_type] => 1 [patent_app_number] => 9/246426 [patent_app_country] => US [patent_app_date] => 1999-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 19 [patent_no_of_words] => 11731 [patent_no_of_claims] => 53 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/318/06318668.pdf [firstpage_image] =>[orig_patent_app_number] => 246426 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4137535 [patent_doc_number] => 06113033 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-09-05 [patent_title] => 'Combined flywheel energy storage and attitude control apparatus for spacecraft' [patent_app_type] => 1 [patent_app_number] => 9/244695 [patent_app_country] => US [patent_app_date] => 1999-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3785 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/113/06113033.pdf [firstpage_image] =>[orig_patent_app_number] => 244695 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4267761 [patent_doc_number] => 06209822 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-03 [patent_title] => 'Device for attaching an engine to an aircraft strut' [patent_app_type] => 1 [patent_app_number] => 9/244629 [patent_app_country] => US [patent_app_date] => 1999-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 4264 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/209/06209822.pdf [firstpage_image] =>[orig_patent_app_number] => 244629 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4407269 [patent_doc_number] => 06224021 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-05-01 [patent_title] => 'Thrust control apparatus and method for an airplane' [patent_app_type] => 1 [patent_app_number] => 9/238280 [patent_app_country] => US [patent_app_date] => 1999-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 11892 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/224/06224021.pdf [firstpage_image] =>[orig_patent_app_number] => 238280 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4058360 [patent_doc_number] => 06068216 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-05-30 [patent_title] => 'Device for treating the exterior of an aircraft' [patent_app_type] => 1 [patent_app_number] => 9/237388 [patent_app_country] => US [patent_app_date] => 1999-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2725 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/068/06068216.pdf [firstpage_image] =>[orig_patent_app_number] => 237388 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4217523 [patent_doc_number] => 06142414 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-11-07 [patent_title] => 'Rotor--aerostat composite aircraft' [patent_app_type] => 1 [patent_app_number] => 9/237110 [patent_app_country] => US [patent_app_date] => 1999-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 5128 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 200 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/142/06142414.pdf [firstpage_image] =>[orig_patent_app_number] => 237110 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4388402 [patent_doc_number] => 06231010 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-05-15 [patent_title] => 'Advanced structural and inflatable hybrid spacecraft module' [patent_app_type] => 1 [patent_app_number] => 9/236785 [patent_app_country] => US [patent_app_date] => 1999-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 20 [patent_no_of_words] => 10520 [patent_no_of_claims] => 45 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 59 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/231/06231010.pdf [firstpage_image] =>[orig_patent_app_number] => 236785 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4276589 [patent_doc_number] => 06182923 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-02-06 [patent_title] => 'Helicopter with control by displacement of its center gravity' [patent_app_type] => 1 [patent_app_number] => 9/235277 [patent_app_country] => US [patent_app_date] => 1999-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3543 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/182/06182923.pdf [firstpage_image] =>[orig_patent_app_number] => 235277 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4389564 [patent_doc_number] => 06170781 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-01-09 [patent_title] => 'Door edge gap and radar signature mitigation door seal' [patent_app_type] => 1 [patent_app_number] => 9/235083 [patent_app_country] => US [patent_app_date] => 1999-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 4002 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/170/06170781.pdf [firstpage_image] =>[orig_patent_app_number] => 235083 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4329101 [patent_doc_number] => 06213427 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-04-10 [patent_title] => 'Airliner life protection module' [patent_app_type] => 1 [patent_app_number] => 9/232620 [patent_app_country] => US [patent_app_date] => 1999-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 14 [patent_no_of_words] => 2500 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/213/06213427.pdf [firstpage_image] =>[orig_patent_app_number] => 232620 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4284933 [patent_doc_number] => 06186444 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2001-02-13 [patent_title] => 'Sliding pocket door for aircraft use capable of nondestructive blow-out and easy access' [patent_app_type] => 1 [patent_app_number] => 9/232100 [patent_app_country] => US [patent_app_date] => 1999-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 21 [patent_no_of_words] => 5465 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/186/06186444.pdf [firstpage_image] =>[orig_patent_app_number] => 232100 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4217634 [patent_doc_number] => 06142421 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-11-07 [patent_title] => 'Vehicle refueling system' [patent_app_type] => 1 [patent_app_number] => 9/231368 [patent_app_country] => US [patent_app_date] => 1999-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 25 [patent_no_of_words] => 7638 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 37 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/142/06142421.pdf [firstpage_image] =>[orig_patent_app_number] => 231368 [rel_patent_id] =>[rel_patent_doc_number] =>)