EP 2250080 A1 20101117 - REVERSE MECHANISM FOR A JET SYSTEM
Title (en)
REVERSE MECHANISM FOR A JET SYSTEM
Title (de)
UMKEHRMECHANISMUS FÜR EIN STRAHLSYSTEM
Title (fr)
MECANISME DE RENVERSEMENT DE MARCHE POUR SYSTEME A JET
Publication
Application
Priority
- US 2009033534 W 20090209
- US 2724008 P 20080208
Abstract (en)
[origin: US2009203270A1] A jet propulsion system includes an inlet receiving a fluid, and a housing defining a discharge nozzle through which fluid is discharged to provide propulsion of a vehicle in a first direction. The jet propulsion system also includes a reverse mechanism movable between a deployed position redirecting fluid from the discharge nozzle toward the first direction and providing propulsion of the vehicle in a second direction substantially opposite the first direction and a non-deployed position allowing fluid to exit the discharge nozzle and provide propulsion of the vehicle in the first direction. The reverse mechanism produces a flow entrainment that enhances forward thrust while the reverse mechanism is in the non-deployed position which results in a net thrust gain over the thrust attributed to the discharge nozzle alone.
IPC 8 full level
B63H 11/11 (2006.01); B63H 11/10 (2006.01); B63H 11/107 (2006.01)
CPC (source: EP US)
B63H 11/11 (2013.01 - EP US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK TR
Designated extension state (EPC)
AL BA RS
DOCDB simple family (publication)
US 2009203270 A1 20090813; EP 2250080 A1 20101117; EP 2250080 A4 20120523; WO 2009100418 A1 20090813
DOCDB simple family (application)
US 36792309 A 20090209; EP 09707662 A 20090209; US 2009033534 W 20090209