| Application number | Title of the application | Filing Date | Status |
|---|
Array
(
[id] => 3506166
[patent_doc_number] => 05505409
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-04-09
[patent_title] => 'Supercavitating airframe'
[patent_app_type] => 1
[patent_app_number] => 8/246447
[patent_app_country] => US
[patent_app_date] => 1994-05-20
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[pdf_file] => patents/05/505/05505409.pdf
[firstpage_image] =>[orig_patent_app_number] => 246447
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/246447 | Supercavitating airframe | May 19, 1994 | Issued |
| 08/245178 | MODULAR LAUNCH PAD SYSTEM | May 16, 1994 | Abandoned |
Array
(
[id] => 3521748
[patent_doc_number] => 05556058
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-09-17
[patent_title] => 'Spacecraft attitude determination using sun sensor, earth sensor, and space-to-ground link'
[patent_app_type] => 1
[patent_app_number] => 8/243669
[patent_app_country] => US
[patent_app_date] => 1994-05-16
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[pdf_file] => patents/05/556/05556058.pdf
[firstpage_image] =>[orig_patent_app_number] => 243669
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/243669 | Spacecraft attitude determination using sun sensor, earth sensor, and space-to-ground link | May 15, 1994 | Issued |
Array
(
[id] => 3549581
[patent_doc_number] => 05499784
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-03-19
[patent_title] => 'Flight refuelling system'
[patent_app_type] => 1
[patent_app_number] => 8/241018
[patent_app_country] => US
[patent_app_date] => 1994-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => patents/05/499/05499784.pdf
[firstpage_image] =>[orig_patent_app_number] => 241018
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/241018 | Flight refuelling system | May 10, 1994 | Issued |
Array
(
[id] => 3547966
[patent_doc_number] => 05501414
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-03-26
[patent_title] => 'Structure having an aerodynamic surface for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/240827
[patent_app_country] => US
[patent_app_date] => 1994-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 4599
[patent_no_of_claims] => 7
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[pdf_file] => patents/05/501/05501414.pdf
[firstpage_image] =>[orig_patent_app_number] => 240827
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/240827 | Structure having an aerodynamic surface for an aircraft | May 10, 1994 | Issued |
Array
(
[id] => 3611910
[patent_doc_number] => 05641135
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-06-24
[patent_title] => 'Inflatable torus and collapsible hinged disc spacecraft designs for satellite communication system'
[patent_app_type] => 1
[patent_app_number] => 8/238568
[patent_app_country] => US
[patent_app_date] => 1994-05-05
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[pdf_file] => patents/05/641/05641135.pdf
[firstpage_image] =>[orig_patent_app_number] => 238568
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/238568 | Inflatable torus and collapsible hinged disc spacecraft designs for satellite communication system | May 4, 1994 | Issued |
Array
(
[id] => 3514537
[patent_doc_number] => 05503352
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-04-02
[patent_title] => 'Light-duty box-wing aeroplane'
[patent_app_type] => 1
[patent_app_number] => 8/238707
[patent_app_country] => US
[patent_app_date] => 1994-05-05
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[firstpage_image] =>[orig_patent_app_number] => 238707
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/238707 | Light-duty box-wing aeroplane | May 4, 1994 | Issued |
Array
(
[id] => 3484178
[patent_doc_number] => 05531404
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-02
[patent_title] => 'Underframe for a passenger aircraft seat, and a seat including such an underframe'
[patent_app_type] => 1
[patent_app_number] => 8/237396
[patent_app_country] => US
[patent_app_date] => 1994-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3299
[patent_no_of_claims] => 20
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[patent_words_short_claim] => 180
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/531/05531404.pdf
[firstpage_image] =>[orig_patent_app_number] => 237396
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/237396 | Underframe for a passenger aircraft seat, and a seat including such an underframe | May 2, 1994 | Issued |
| 08/236298 | MODULAR LAUNCH PAD SYSTEM | May 1, 1994 | Abandoned |
Array
(
[id] => 3543893
[patent_doc_number] => 05542626
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-08-06
[patent_title] => 'Multi-deck passenger aircraft having impact energy absorbing structures'
[patent_app_type] => 1
[patent_app_number] => 8/232387
[patent_app_country] => US
[patent_app_date] => 1994-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4956
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/542/05542626.pdf
[firstpage_image] =>[orig_patent_app_number] => 232387
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/232387 | Multi-deck passenger aircraft having impact energy absorbing structures | Apr 24, 1994 | Issued |
Array
(
[id] => 3586715
[patent_doc_number] => 05558299
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-09-24
[patent_title] => 'Wing fold push-pin locking assembly'
[patent_app_type] => 1
[patent_app_number] => 8/229637
[patent_app_country] => US
[patent_app_date] => 1994-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => patents/05/558/05558299.pdf
[firstpage_image] =>[orig_patent_app_number] => 229637
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/229637 | Wing fold push-pin locking assembly | Apr 18, 1994 | Issued |
| 08/226954 | FLAME ARRESTER | Apr 12, 1994 | Abandoned |
Array
(
[id] => 3542126
[patent_doc_number] => 05518210
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-05-21
[patent_title] => 'Seal plate for aircraft movable flight control surfaces'
[patent_app_type] => 1
[patent_app_number] => 8/225739
[patent_app_country] => US
[patent_app_date] => 1994-04-11
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/518/05518210.pdf
[firstpage_image] =>[orig_patent_app_number] => 225739
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/225739 | Seal plate for aircraft movable flight control surfaces | Apr 10, 1994 | Issued |
| 08/226015 | AUTOGYRO AIRCRAFT | Apr 10, 1994 | Issued |
Array
(
[id] => 3515097
[patent_doc_number] => 05540404
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-30
[patent_title] => 'Double-decked aircraft with plug door'
[patent_app_type] => 1
[patent_app_number] => 8/224684
[patent_app_country] => US
[patent_app_date] => 1994-04-08
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/540/05540404.pdf
[firstpage_image] =>[orig_patent_app_number] => 224684
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/224684 | Double-decked aircraft with plug door | Apr 7, 1994 | Issued |
| 08/223299 | METHOD AND APPARATUS FOR ACTUATING A MOMENTUM WHEEL WITH HIGH VIBRATION ISOLATION | Apr 4, 1994 | Abandoned |
Array
(
[id] => 3470848
[patent_doc_number] => 05456426
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-10-10
[patent_title] => 'Attachment fitting for a wall of a flexible structure'
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[patent_app_country] => US
[patent_app_date] => 1994-04-04
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[firstpage_image] =>[orig_patent_app_number] => 223419
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/223419 | Attachment fitting for a wall of a flexible structure | Apr 3, 1994 | Issued |
Array
(
[id] => 3515145
[patent_doc_number] => 05489074
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-02-06
[patent_title] => 'Thermal protection device, in particular for an aerospace vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/220807
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[pdf_file] => patents/05/489/05489074.pdf
[firstpage_image] =>[orig_patent_app_number] => 220807
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/220807 | Thermal protection device, in particular for an aerospace vehicle | Mar 30, 1994 | Issued |
Array
(
[id] => 3493082
[patent_doc_number] => 05513821
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-05-07
[patent_title] => 'Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored'
[patent_app_type] => 1
[patent_app_number] => 8/219329
[patent_app_country] => US
[patent_app_date] => 1994-03-29
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/513/05513821.pdf
[firstpage_image] =>[orig_patent_app_number] => 219329
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/219329 | Aircraft steering system and method for large aircraft having main landing gear steering during low taxi speed while nose gear is castored | Mar 28, 1994 | Issued |
Array
(
[id] => 3528882
[patent_doc_number] => 05480110
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-01-02
[patent_title] => 'Transport plane with stub tail'
[patent_app_type] => 1
[patent_app_number] => 8/218057
[patent_app_country] => US
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[pdf_file] => patents/05/480/05480110.pdf
[firstpage_image] =>[orig_patent_app_number] => 218057
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/218057 | Transport plane with stub tail | Mar 24, 1994 | Issued |