Abstract: The combustion engine using several kinds of fuels is provided with intake and exhaust valves and an injection device which may be electronically adjusted. It is comprised of at least one working cylinder (1, 1a) at the upper part of which is provided a fuel supply device (4), an intake valve (5) and an ignition device (6); these elements being all electronically adjustable. In the working cylinder (1, 1a) there is provided a piston (9) which is in communication with a pressure accumulator device. This connection device may be comprised of a hydraulic, pneumatic accumulator or even a spring accumulator. The piston rod (12), provided with a blocking device (11) is connected to a transmission shaft (15), (15a). To regulate the running of this engine, there is provided an indicator (3) of the cylinder temperature, a piston position indicator (34) and an electronically programmable adjusting and control device (20), such device (20) possibly being a microprocessor (20a).

Abstract: A control system for controlling, for example, the operation of an aircraft or any other system requiring a flow of data back and forth between controlling and controlled units of the system, comprises a passive, multiply intermeshed conductor network (20, 24) of light conductors (11, 12). This network transmits control signals in the form of digital light signals from a control signal source, such as a control stick (9) in the cockpit of an aircraft or spacecraft, to respective controlled servo-units (14). The transmission system includes signal processors (10) including mixers (15) and information devices (16, 17, 18) interposed between the control signal source and the network (24) which is connected to the addressable controlled units, e.g., servo-units. The system is powered by a power supply device comprising several energy sources which may be switched on selectively as required.

Abstract: The present apparatus is used for ascertaining the individual weight of any type of load including that of passengers and of hand baggage, that is added to the total payload of an aircraft. Each individual weight is ascertained and, if desired, displayed and added up to ascertain the total weight. For this purpose a weight sensing device such as a group of load cells or the like including a platform is arranged at the entrance to the freight or baggage compartment and, in a passenger aircraft at each passenger entrance door inside the aircraft. The weight sensing device provides an electrical signal for each weight unit that passes the platform into the aircraft. The weight representing electrical signal is supplied to an adder and to a display unit where the individual weights are displayed as well as the total weight.

Abstract: A passenger buys his ticket at a station from a device which registers his destination and transmits the information to a central computer using the destination data to plot a travel path for a fleet of buses or other mass-transit vehicles. The arrival time of the next vehicle is indicated at each station; as the user boards such vehicle his destination is entered in a register therein. The central computer reads the vehicular memories by radio communication to modify, if necessary, the instructions given to the driver. Traffic density, average vehicular speed and the rhythm of traffic lights are also read into the central computer by way of supplemental information.