Abstract: A method and a system are provided herein for calculating whether or not a specific aerial vehicle at a specified point of time can maneuver over a given location in the terrain while complying with terrain clearance requirements. The system may include a computer memory configured to store a 3D model representing at least a portion of a terrain located in a vicinity of an aerial vehicle; a computer processor configured to map said portion of the terrain into at least two types: a first type indicative of a potential of the aerial vehicle to maneuver over a respective terrain while complying with terrain clearance, and a second type indicative of a non-potential of said aerial vehicle to maneuver over a respective terrain, wherein the mapping is carried out based on said parameters, the 3D model and given predefined performance of the aerial vehicle.

Abstract: A thermal energy storage unit is disclosed. The system comprising: a tube having at least one inlet and at least one outlet for a first fluid; a plurality of plate-shaped or box-shaped capsules having a second fluid therein, wherein the plurality of capsules is arranged inside the tube to form a plurality of stacks of capsules; wherein: the first fluid is a heat transfer fluid for exchanging heat with the second fluid; the second fluid is a phase-change medium; wherein a plurality of defined narrow flow paths for the first fluid is provided between the capsules. The defined flow paths increase the efficiency of the system.

Abstract: A thermal energy storage unit is disclosed. The system comprising: a tube having at least one inlet and at least one outlet for a first fluid; a plurality of plate-shaped or box-shaped capsules having a second fluid therein, wherein the plurality of capsules is arranged inside the tube to form a plurality of stacks of capsules; wherein: the first fluid is a heat transfer fluid for exchanging heat with the second fluid; the second fluid is a phase-change medium; wherein a plurality of defined narrow flow paths for the first fluid is provided between the capsules. The defined flow paths increase the efficiency of the system.

Abstract: A method of flattening electric energy demand from an electric grid including during less-than-peak electricity demand periods, freezing Phase Change Material (PCM) in a Thermal Energy Storage (TES) system, and during peak electricity demand periods, using the TES to cool air conditioning refrigerant fluid. A system of flattening electric energy demand of an air-conditioner from an electric grid including an air conditioner, a Thermal Energy Storage system, and a controller, wherein the controller is programmed to implement the above method. A method of freezing Phase Change Material (PCM) in a Thermal Energy Storage (TES) system including setting a temperature of heat exchange fluid at a temperature higher than ?10 degrees Celsius when directed to ice bricks containing water and an ice nucleation agent. A Thermal Energy Storage (TES) system controller programmed to discharge more than 50% of a heat capacity of the TES. Related apparatus and methods are also described.

Abstract: A thermal-storage container used in a thermal-storage system to exchange heat by fluid flow though phase-changing material disposed inside the thermal-storage container, including a thermal-storage container housing, a fluid inlet and a fluid outlet, and one or more capsules containing the phase-change material, wherein the housing is shaped as an elongate container, a ratio of length to width of the housing is between 2 and 20. Related apparatus and methods are also described.

Abstract: A thermal-storage container used in thermal systems to exchange heat by fluid flow though phase-changing material disposed inside the thermal-storage container, including a thermal-storage container housing, a fluid inlet and a fluid outlet, and one or more capsules containing the phase-change material, and defining a plurality of passages configured to direct the flow of the fluid at different portions inside the housing, wherein an actual fluid flow length from the fluid inlet to the fluid outlet is longer than a direct length measured between the fluid inlet and the fluid outlet through all sections through which the fluid flows. Related apparatus and methods are also described.

Abstract: A method and a system are provided herein for calculating whether or not a specific aerial vehicle at a specified point of time can maneuver over a given location in the terrain while complying with terrain clearance requirements. The system may include a computer memory configured to store a 3D model representing at least a portion of a terrain located in a vicinity of an aerial vehicle; a computer processor configured to map said portion of the terrain into at least two types: a first type indicative of a potential of the aerial vehicle to maneuver over a respective terrain while complying with terrain clearance, and a second type indicative of a non-potential of said aerial vehicle to maneuver over a respective terrain, wherein the mapping is carried out based on said parameters, the 3D model and given predefined performance of the aerial vehicle.

Abstract: A method and a system are provided herein for calculating whether or not a specific aerial vehicle at a specified point of time can maneuver over a given location in the terrain while complying with terrain clearance requirements. The system may include a computer memory configured to store a 3D model representing at least a portion of a terrain located in a vicinity of an aerial vehicle; a computer processor configured to map said portion of the terrain into at least two types: a first type indicative of a potential of the aerial vehicle to maneuver over a respective terrain while complying with terrain clearance, and a second type indicative of a non potential of said aerial vehicle to maneuver over a respective terrain, wherein the mapping is carried out based on said parameters, the 3D model and given predefined performance of the aerial vehicle.

Abstract: A thermal energy storage unit is disclosed. The system comprising: a tube having at least one inlet and at least one outlet for a first fluid; a plurality of plate-shaped or box-shaped capsules having a second fluid therein, wherein the plurality of capsules is arranged inside the tube to form a plurality of stacks of capsules; wherein: the first fluid is a heat transfer fluid for exchanging heat with the second fluid; the second fluid is a phase-change medium; wherein a plurality of defined narrow flow paths for the first fluid is provided between the capsules. The defined flow paths increase the efficiency of the system.

Abstract: A method and a system are provided herein for calculating whether or not a specific aerial vehicle at a specified point of time can maneuver over a given location in the terrain while complying with terrain clearance requirements. The system may include a computer memory configured to store a 3D model representing at least a portion of a terrain located in a vicinity of an aerial vehicle; a computer processor configured to map said portion of the terrain into at least two types: a first type indicative of a potential of the aerial vehicle to maneuver over a respective terrain while complying with terrain clearance, and a second type indicative of a non-potential of said aerial vehicle to maneuver over a respective terrain, wherein the mapping is carried out based on said parameters, the 3D model and given predefined performance of the aerial vehicle.

Abstract: A method and a system are provided herein for calculating whether or not a specific aerial vehicle at a specified point of time can maneuver over a given location in the terrain while complying with terrain clearance requirements. The system may include a computer memory configured to store a 3D model representing at least a portion of a terrain located in a vicinity of an aerial vehicle; a computer processor configured to map said portion of the terrain into at least two types: a first type indicative of a potential of the aerial vehicle to maneuver over a respective terrain while complying with terrain clearance, and a second type indicative of a non-potential of said aerial vehicle to maneuver over a respective terrain, wherein the mapping is carried out based on said parameters, the 3D model and given predefined performance of the aerial vehicle.

Abstract: Presented herein is a grooming device for the removal of hair and for eyebrow care and maintenance, said device comprising a pair of tweezers and a brush head disposed on said tweezers. Some embodiments of the grooming device of the present invention further comprise a protective storage case comprising a receiving member and a cover member that has a mirror disposed thereon. Some embodiments of the grooming device of the present invention further comprise a light assembly disposed on the tweezers.