Power regulating device for an aircraft

An energy system for an aircraft;

• wherein the energy system comprises:
• a power regulating device for regulating hybrid energy sources for the aircraft;
• a first energy source with a first operating characteristic;
• a second energy source with a second operating characteristic;
• wherein the power regulating device is adapted such that a requirement of a required means of a consumer is measurable;
• wherein the power regulating device is adapted such that the first operating characteristic of the first energy source and the second operating characteristic of the second energy source are determinable;
• wherein by means of the first energy source a first requirement share can be generated, and by means of the second energy source a second requirement share of the required means can be generated;
• wherein the power regulating device is adapted for controlling the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means can be provided to the consumer;
• wherein the power regulating device is adapted such that depending on a flight phase the first operating characteristic and the second operating characteristic are determinable;
• wherein the power regulating device is adapted such that a requirement of a required means of the consumer is measurable;
• wherein the power regulating device is adapted such that the first operating characteristic and the second operating characteristic are determinable;
• wherein by means of the first energy source a first energy share and by means of the second energy source a second energy share of the required means can be generated;
• wherein the power regulating device is adapted to control the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means are profitable to the consumer;
• wherein the power regulating device is adapted such that depending on the flight phase the first operating characteristic and the second operating characteristic are determinable.

A method for regulating hybrid energy sources for an aircraft, wherein the method comprises:

• measuring the requirement of a required means of a consumer by means of a power regulating device;
• determining a first operating characteristic of a first energy source and a second operating characteristic of a second energy source by means of the power regulating device;
• generating a first requirement share of the required means by means of the first energy source and a second requirement share of the required means by means of the second energy source;
• regulating the first energy source and the second energy source by means of the power regulating device such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means are provided to the consumer;
• and
• determining the first operating characteristic and the second operating characteristic depending on a flight phase by means of the power regulating device

An aircraft comprising a power regulating device for regulating hybrid energy sources for the aircraft,

• wherein the power regulating device is adapted such that a requirement of a required means of a consumer is measurable;
• wherein the power regulating device is adapted such that a first operating characteristic of a first energy source and a second operating characteristic of a second energy source are determinable;
• wherein by means of the first energy source a first requirement share can be generated, and by means of the second energy source a second requirement share of the required means can be generated;
• wherein the power regulating device is adapted for controlling the first energy source and the second energy source such that depending on the first operating characteristic and on the second operating characteristic the first requirement share and the second requirement share of the required means can be provided to the consumer;
• and
• wherein the power regulating device is adapted such that depending on a flight phase the first operating characteristic and the second operating characteristic are determinable.