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Gas-turbine engine
John Barber · 1791
John Barber’s 1791 gas-turbine patent describes a continuous-flow internal combustion engine with compressor, combustor, and turbine — the first to integrate all three in a self-contained gas-generator core. It operates on the Brayton cycle. No evidence exists that it was built or ran. It changes how we classify engines — distinguishing true gas turbines from exhaust-driven devices — but delivers no working performance, no efficiency data, and no engineering resolution of ignition, heat tolerance, or rotational balance. Its significance is taxonomic, not operational.