David M Gray

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Array ( [id] => 6553710 [patent_doc_number] => 20100288881 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-18 [patent_title] => 'SECURED COCKPIT HAVING AN INTEGRATED ACCOMMODATION AREA AND LAVATORY FACILITIES' [patent_app_type] => utility [patent_app_number] => 12/675238 [patent_app_country] => US [patent_app_date] => 2008-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6555 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0288/20100288881.pdf [firstpage_image] =>[orig_patent_app_number] => 12675238 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6445253 [patent_doc_number] => 20100038482 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'COMBINATION VENTILATION AND OVERHEAD STOWAGE BIN SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/190691 [patent_app_country] => US [patent_app_date] => 2008-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2510 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038482.pdf [firstpage_image] =>[orig_patent_app_number] => 12190691 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5364601 [patent_doc_number] => 20090302160 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-10 [patent_title] => 'SYSTEM FOR REFUELLING OPERATIONS' [patent_app_type] => utility [patent_app_number] => 12/187802 [patent_app_country] => US [patent_app_date] => 2008-08-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2664 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0302/20090302160.pdf [firstpage_image] =>[orig_patent_app_number] => 12187802 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6263494 [patent_doc_number] => 20100252673 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-10-07 [patent_title] => 'AERIAL DEVICE' [patent_app_type] => utility [patent_app_number] => 12/670572 [patent_app_country] => US [patent_app_date] => 2008-07-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4961 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0252/20100252673.pdf [firstpage_image] =>[orig_patent_app_number] => 12670572 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6224262 [patent_doc_number] => 20100181419 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-22 [patent_title] => 'ENGINE MOUNTING STRUCTURE FOR AIRCRAFT HAVING A BEAM SPREADER CONNECTED AT FOUR POINTS' [patent_app_type] => utility [patent_app_number] => 12/668030 [patent_app_country] => US [patent_app_date] => 2008-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6376 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0181/20100181419.pdf [firstpage_image] =>[orig_patent_app_number] => 12668030 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8493038 [patent_doc_number] => 20120292445 [patent_country] => US [patent_kind] => A9 [patent_issue_date] => 2012-11-22 [patent_title] => 'MODULAR HATRACK FOR A PASSENGER COMPARTMENT OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/665993 [patent_app_country] => US [patent_app_date] => 2008-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4662 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12665993 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 6602616 [patent_doc_number] => 20100170989 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-08 [patent_title] => 'ELONGATE COMPOSITE STRUCTURAL MEMBERS AND IMPROVEMENTS THEREIN' [patent_app_type] => utility [patent_app_number] => 12/602160 [patent_app_country] => US [patent_app_date] => 2008-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8567 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0170/20100170989.pdf [firstpage_image] =>[orig_patent_app_number] => 12602160 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6396610 [patent_doc_number] => 20100178453 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'ELONGATE COMPOSITE STRUCTURAL MEMBER' [patent_app_type] => utility [patent_app_number] => 12/602163 [patent_app_country] => US [patent_app_date] => 2008-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8621 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0178/20100178453.pdf [firstpage_image] =>[orig_patent_app_number] => 12602163 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 6224264 [patent_doc_number] => 20100181421 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-22 [patent_title] => 'TWO-STAGE AIRBAG INFLATION SYSTEM WITH PYROTECHNIC DELAY' [patent_app_type] => utility [patent_app_number] => 12/666757 [patent_app_country] => US [patent_app_date] => 2008-06-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3252 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0181/20100181421.pdf [firstpage_image] =>[orig_patent_app_number] => 12666757 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 6391039 [patent_doc_number] => 20100163671 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-01 [patent_title] => 'A MOUNTING ELEMENT FOR A GAS TURBINE ENGINE, AND A STRUCTURE AND AN AIRCRAFT WITH SUCH A MOUNTING ELEMENT' [patent_app_type] => utility [patent_app_number] => 12/600534 [patent_app_country] => US [patent_app_date] => 2008-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4785 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0163/20100163671.pdf [firstpage_image] =>[orig_patent_app_number] => 12600534 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6224260 [patent_doc_number] => 20100181418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-22 [patent_title] => 'SECURING PLATE AND LONGITUDINAL HANDLING MEMBER FOR A ONE-PIECE AIRCRAFT PROPULSION UNIT' [patent_app_type] => utility [patent_app_number] => 12/666122 [patent_app_country] => US [patent_app_date] => 2008-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2003 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0181/20100181418.pdf [firstpage_image] =>[orig_patent_app_number] => 12666122 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6381989 [patent_doc_number] => 20100176239 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'DEVICE FOR MOUNTING AN AIRCRAFT TURBOPROP ENGINE COMPRISING HYDRAULIC ATTACHMENTS' [patent_app_type] => utility [patent_app_number] => 12/602110 [patent_app_country] => US [patent_app_date] => 2008-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5374 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0176/20100176239.pdf [firstpage_image] =>[orig_patent_app_number] => 12602110 [rel_patent_id] =>[rel_patent_doc_number] =>)

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