Energy supply system for an electrical seat device in an aircraft or spacecraft
First Claim
1. An energy supply system for an electrical seat device in an aircraft or spacecraft, the energy supply system comprising:
- a control unit connected to the seat device;
an energy supply which is configured to supply the control unit with electrical energy; and
an energy storage device which is configured to store electrical energy in a rechargeable manner and which is coupled to the control unit such that said energy storage device can be charged by the energy supply and such that the charging and discharging of said energy storage device can be controlled by the control unit;
wherein the control unit is configured to use, as required, the electrical energy stored by the energy storage device to operate the seat device.
1 Assignment
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Accused Products
Abstract
An energy supply system for an electrical seat device in an aircraft or spacecraft comprises a control unit connected to the seat device, an energy supply which is configured to supply the control unit with electrical energy and an energy storage device which is configured to store electrical energy in a rechargeable manner and which is coupled to the control unit such that said energy storage device can be charged by the energy supply and such that the charging and discharging of said energy storage device can be controlled by the control unit, wherein the control unit is configured to use, as required, the electrical energy stored by the energy storage device to operate the seat device.
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Citations
12 Claims
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1. An energy supply system for an electrical seat device in an aircraft or spacecraft, the energy supply system comprising:
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a control unit connected to the seat device; an energy supply which is configured to supply the control unit with electrical energy; and an energy storage device which is configured to store electrical energy in a rechargeable manner and which is coupled to the control unit such that said energy storage device can be charged by the energy supply and such that the charging and discharging of said energy storage device can be controlled by the control unit; wherein the control unit is configured to use, as required, the electrical energy stored by the energy storage device to operate the seat device. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. An electrical seat device for an aircraft or spacecraft, comprising an energy supply system comprising:
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a control unit connected to the seat device; an energy supply which is configured to supply the control unit with electrical energy; and an energy storage device which is configured to store electrical energy in a rechargeable manner and which is coupled to the control unit such that said energy storage device can be charged by the energy supply and such that the charging and discharging of said energy storage device can be controlled by the control unit; wherein the control unit is configured to use, as required, the electrical energy stored by the energy storage device to operate the seat device. - View Dependent Claims (11)
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12. An aircraft or spacecraft comprising at least one electrical seat device, comprising an energy supply system comprising:
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a control unit connected to the seat device; an energy supply which is configured to supply the control unit with electrical energy; and an energy storage device which is configured to store electrical energy in a rechargeable manner and which is coupled to the control unit such that said energy storage device can be charged by the energy supply and such that the charging and discharging of said energy storage device can be controlled by the control unit; wherein the control unit is configured to use, as required, the electrical energy stored by the energy storage device to operate the seat device.
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Specification