Application

15901365 · CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC AIRCRAFT AND METHOD FOR ADJUSTING THE NOZZLE THROAT SURFACE IN A NOZZLE OF A TURBOFAN ENGINE

Filed 2018-02-21 · Granted · Patent 10738735 (2020-08-11) The official file ↗The patent and its PDF ↗ · Art unit 3741 · Examiner Colin J Paulauskas Easy · CPC F02K 1/08 · Rolls-Royce Deutschland Ltd & Co KG · SHUTTLEWORTH & INGERSOLL, P.L.C.

Office actions

first was Non-final rejection

RCEs

no appeal

To first action

21.1 mo

to disposition 29.6 mo

Statutes raised

102 112

1 actions read

Unlock the prosecution timelineIncluded in Pro, from $29 a month. Cancel any time.