Patent ID: 11891951
Assignee: UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 6:
7. An isolator for a scramjet comprising:
a housing having a longitudinal length extending between a forward end and an aft end;
wherein the forward end receives airflow from an air inlet;
wherein the aft end discharges airflow to a combustor;
a plurality of separate flow channels formed internal to the housing configured to direct airflow therethrough;
wherein the plurality of separate flow channels are formed by solid walls that prevents fluid from passing therethrough;
a plurality of internal channel walls configured to form the plurality of separate flow channels within the housing; and
a pointed tip extending from the plurality of internal channel walls toward the forward end of the housing.