ALEXANDRIA, Va., Nov. 18 -- United States Patent no. 12,473,864, issued on Nov. 18, was assigned to HAMILTON SUNDSTRAND Corp. (Charlotte, N.C.).
"Integrated turbine engine bleed system" was invented by Myles Kelly (Willimantic, Conn.).
According to the abstract* released by the U.S. Patent & Trademark Office: "A turbine engine for an aircraft includes a compressor with a low-pressure spool including a low-pressure tap and a high-pressure spool including a high-pressure tap and a combustor connected to the compressor. The engine includes a turbine connected to the combustor and that includes an inlet section connected to the outlet portion of the combustor and an outlet section. The engine also includes an integrated engine bleed system co...