Wissler
Gerald Wissler, Mainhausen DE
Patent application number | Description | Published |
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20100168326 | RTV TWO-COMPONENT SILICONE RUBBER - RTV two-component silicone rubber which contains structurally modified hydrophobic fumed silicas which have vinyl groups fixed on the surface, further hydrophobic groups, such as trimethylsilyl and/or dimethylsilyl and/or monomethylsilyl groups, additionally being fixed on the surface. | 07-01-2010 |
John B. Wissler, Waltham, MA US
Patent application number | Description | Published |
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20150323932 | AUTONOMOUS CARGO DELIVERY SYSTEM - The present invention is directed to a system and methods of providing platform-agnostic systems and methods capable of providing an integrated processor and sensor suite with supervisory control software and interfaces to perform small unit rapid response resupply and CASEVAC into hazardous and unpredictable environments. | 11-12-2015 |
John Brooke Wissler, Waltham, MA US
Patent application number | Description | Published |
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20130206921 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE - A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | 08-15-2013 |
20150021430 | SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE - A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends. | 01-22-2015 |
Monika Wissler, Ahrensburg DE
Patent application number | Description | Published |
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20130060065 | Process for the Dehydration of Substituted 4-Dimethylamino-2-aryl-butan-2-ol Compounds and Process for the Preparation of Substituted Dimethyl-(3-aryl-butyl)- Amine Compounds by Heterogeneous Catalysis - Process for the preparation of substituted dimethyl-(3-aryl-butyl)-amine compounds. The process comprises dehydration by heterogeneous catalysis of substituted 4-dimethylamino-2-aryl-butan-2-ol compounds, to form substituted dimethyl-(3-aryl-but-3-enyl)-amine intermediates, which are then converted by hydrogenation with hydrogen to substituted dimethyl-(3-aryl-butyl)-amine compounds. | 03-07-2013 |