Abstract: Improvements to an engine comprise an air compressor cylinder with a piston, a combustion chamber cylinder with a piston. An engine has added an expansion chamber cylinder with a piston. Pistons each have a connecting rod and connecting rod head and associated parts adapted for reciprocating motion via combustion products, and a transmission associated with the engine. Improvements are to the piston seals, ignition assembly, valve shape and stem/rocker, valve operating mechanism, construction of head, heat management/heat shield, connecting rod/piston rotator, engine balancing, fuel pump placement, and a machining process.

Abstract: Improvements to an engine comprise an air compressor cylinder with a piston, a combustion chamber cylinder with a piston. An engine has added an expansion chamber cylinder with a piston. Pistons each have a connecting rod and connecting rod head and associated parts adapted for reciprocating motion via combustion products, and a transmission associated with the engine. Improvements are to the piston seals, ignition assembly, valve shape and stem/rocker, valve operating mechanism, construction of head, heat management/heat shield, connecting rod/piston rotator, engine balancing, fuel pump placement, and a machining process.

Abstract: A vapor generating system for supplying vapor energy to power a motor and employing the energy in the vapor exhausted by the motor to operate an air pump for supplying air to mix with a source of fuel in a combustion space in a chamber which collects vapor under pressure for release through a transmission connected to the motor. The vapor exhausted from the motor is delivered to a condenser where it resumes a liquid so the resulting liquid is able to be reused for maintaining a supply of vapor energy.

Abstract: An airborne sonar system includes a transducer with both projecting elements and receiving elements designed for echo ranging at a moderately high frequency. Carried on the transducer housing is an additional hydrophone which is sensitive to sonar input signals at low frequency and, hence, which has a capability of responding to signals from much longer range than can the receiving elements of the echo ranging transducer. This low frequency hydrophone is sensitive to the frequency of much of the noise and vibration imparted to the transducer housing by the supporting aircraft and so, in operation, the hydrophone is suspended on a very compliant mounting consisting of a plurality of strips of light rubber tubing.