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WO2020226708A2
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Fluidic propulsive system
|
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US2020324891A1
|
|
Adaptive vertical take-off and landing propulsion system
|
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US2020324890A1
|
|
Adaptive vertical take-off and landing propulsion system
|
|
AU2019279873A1
|
|
Streamline airframe with boundary ingestion fluidic propulsive elements
|
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BR112020023319A2
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|
combination of compressed fluid ejector and propeller propulsion system
|
|
WO2019014386A1
|
|
Gimballed augmentation shroud
|
|
US2018305007A1
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|
Configuration for vertical take-off and landing system for aerial vehicles
|
|
KR20200043980A
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Configuration for vertical take-off and landing systems for aviation vehicles
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BR112019026384A2
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winglet ejector settings
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US2018003128A1
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|
Variable geometry thruster
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KR20190058488A
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|
Variable geometry thruster
|
|
CN109715913A
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Pipe fluid remover system is discharged in internal combustion engine
|
|
US2017350309A1
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|
Internal combustion engine exhaust pipe fluidic purger system
|
|
US2017321638A1
|
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Internal combustion engine intake power booster system
|
|
AU2017305160A1
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|
Internal combustion engine intake power booster system
|
|
US2017283080A1
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Winglet ejector configurations
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|
CA3017263A1
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Configuration for vertical take-off and landing system for aerial vehicles
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US2017240275A1
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Configuration for vertical take-off and landing system for aerial vehicles
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KR20180088708A
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Micro-turbine gas generator and propulsion system
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EP3363732A1
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Ejector and airfoil configurations
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