1. An organic luminescence display device comprising:
one or more display elements;
at least one moisture detector placed in a predetermined location close to the display elements, the moisture detector including a material layer comprising metal formed between a first electrode and a second electrode; and
a first and second shields for encapsulating the display elements and the moisture detector therebetween,
wherein the material layer between the first and second electrodes of the moisture detector has a resistance that varies with a moisture level of an environment in which the display device is located.
2. The display device of claim 1 wherein the moisture detector is placed in the predetermined location of the device so that it does not affect an operation of the display elements.
3. The display device of claim 1 wherein a light transmissivity of the moisture detector varies with the moisture level of the environment in which the display elements are located.
4. The display device of claim 1 wherein the material layer comprises a metal compound.
5. The display device of claim 1, wherein each of the one or more display elements includes a cathode and an anode made of the same material as the first and second electrodes.
6. The display device of claim 1, wherein the material layer of the moisture detector contains a IA or IIA group earth metal.
7. The display device of claim 1, wherein the material layer has a thickness of 200 angstroms or more.
8. The display device of claim 1, wherein the display elements form an array, the moisture detector is located proximate to a column of display elements located at an edge of the array, and the moisture detector extends from a first position located proximate to a top edge of a top display element of the column of display elements to a second position located proximate to a bottom edge of a bottom display element of the column of display elements.
9. The display device of claim 1, wherein the display elements are disposed to form an array pattern comprising a plurality of element regions, and the moisture detector is disposed at an element region located at a corner of the array pattern.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A method for facilitating performing an altitude change maneuver within reduced spacings of an airplane (AC) flying at a current altitude level (Nc), according to a given course, for capturing a target altitude level (Na), said airplane (AC) being provided with receiving means (2) for information relating to aircrafts flying in an air environment in the vicinity of said airplane (AC),
comprising:
defining a target altitude level to be captured (Na);
determining a control volume (V) around said airplane (AC), a first dimension (h) of which is a function of the altitude difference between said current level (Nc) and said target level (Na), a second dimension (L) of which depends on a first distance threshold (s1) and a third dimension (1) of which depends on a second distance threshold (s2);
locating the presence of at least one aircraft (ACd1, ACd2, ACref) inside said control volume (V);
should at least one aircraft (ACd1, ACd2, ACref) be located in said control volume (V), checking whether the following activation conditions are met:
the distance separating said airplane (AC) from said located aircraft is strictly lower than said first distance threshold (s1) and is at least equal to a third distance threshold (dITP); and
the angle formed between the course of said airplane (AC) and the course of said located aircraft is at the most equal to a predefined angle threshold; and
when said located aircraft (ACref) meets said activation conditions, from information from said located aircraft (ACref) received by said reception means (2), determining a performing time range, during which said altitude change maneuver is able to be performed.
2. A method according to claim 1,
wherein said time range is determined only when at least one and at the most two aircrafts (ACref) are located in said control volume (V) and they each meet said activation conditions.
3. A method according to claim 1,
wherein said performing time range is determined from the relative velocity of said airplane (AC) with respect to said located aircraft (ACref) meeting said activation conditions and the relative position of said airplane (AC) with respect to said aircraft (ACref).
4. A method according to claim 1,
wherein a performing authorization request is generated automatically, intended for being transmitted, on pilots’ order, to the air traffic control (5).
5. A method according to claim 4,
wherein said authorization request comprises relative position information of said airplane (AC) with respect to said located aircraft (ACref) meeting said activation conditions, as well as information relating to the desired altitude change maneuver within reduced spacings.
6. A method according to claim 1,
wherein said control volume (V) has the form of a rectangular parallelepiped with the height thereof (h) corresponding to said first dimension.
7. A device for facilitating performing an altitude change maneuver within reduced spacings of an airplane (AC) flying at a current altitude level (Nc), according to a given course, for capturing a target altitude level (Na), said airplane (AC) being provided with receiving means (2) for information relating to aircrafts flying in an air environment in the vicinity of said airplane (AC),
comprising:
means (4) for defining a target altitude level (Na) to be captured;
means (7) for determining a control volume (V) around said airplane (AC), a first dimension (h) of which is a function of the altitude difference between said current level (Nc) and said target level (Na), a second dimension (L) of which depends on a first distance threshold (s1) and a third dimension (1) of which depends on a second distance threshold (s2);
means (8) for locating the presence of at least one aircraft (ACd1, ACd2, ACref) inside said control volume (V);
means (9) for checking, should at least one aircraft (ACd1, ACd2, ACref) be located in said control volume (V), that the following activation conditions are met:
the distance separating said airplane (AC) from said located aircraft is strictly lower than said distance threshold and is at least equal to a third distance threshold (dITP); and
the angle formed between the course of said airplane (AC) and the course of said located aircraft is at the most equal to a predefined angle threshold; and
means (10) for determining, from information from said located aircraft (ACref) received by said receiving means (2), a performing time range during which said altitude change maneuver is able to be performed, said means (10) being activated when said located aircraft (ACref) meets said activation conditions.
8. A device according to claim 7,
wherein it comprises means (11) for automatically generating a performing authorization request to be transmitted, on pilots’ order, to the air traffic control (5).
9. An airplane,
comprising a device (1) such as specified according to claim 7.