Betekenis van:
navigation light

Voorbeeldzinnen

1. “navigation lights” light appearances of navigation lights for the identification of craft;’
2. “navigation lights” light appearances of navigation lights for the identification of craft;’ ‘97b.
3. light appearances of navigation lights for the identification of craft;’
4. The Council, acting unanimously, will as necessary review and refine the rules and procedures set out in Articles 2 and 3 of this Joint Action in the light of the development of the European satellite radio-navigation system.
5. It is appropriate to provide for a simple procedure for the Council to update certain important technical elements of this Regulation in particular in the light of an assessment of its impact on transport of live animals within an enlarged Community and establish the specifications of the Navigation System to be used for all means of transport by road in the light of the future technological developments in the area such as the coming into fruition of the Galileo system.
6. At least one lifebuoy on each side shall be equipped with a buoyant lifeline equal in length to not less than twice the height at which it is stowed above the waterline in the lightest seagoing condition or 30 metres, whichever is the greater.Two lifebuoys shall be equipped with a self-activating smoke signal and a self-activating light; they shall be capable of quick release from the navigation bridge.
7. At least one lifebuoy on each side shall be equipped with a buoyant lifeline equal in length to not less than twice the height at which it is stowed above the waterline in the lightest seagoing condition or 30 metres, whichever is the greater.Two lifebuoys shall be equipped with a self-activating smoke signal and a self-activating light; they shall be capable of quick release from the navigation bridge. The remainder of the lifebuoys shall be equipped with self-igniting lights, in compliance with the provisions of paragraph 2.1.2 of the LSA Code.
8. "DBRN" systems designed to navigate underwater using sonar or gravity databases that provide a positioning accuracy equal to or less (better) than 0,4 nautical miles; b. "development""technology", as follows, for "active flight control systems" (including fly-by-wire or fly-by-light): 1. configuration design for interconnecting multiple microelectronic processing elements (on-board computers) to achieve "real time processing" for control law implementation; 2. control law compensation for sensor location or dynamic airframe loads, i.e., compensation for sensor vibration environment or for variation of sensor location from the centre of gravity; 3. electronic management of data redundancy or systems redundancy for fault detection, fault tolerance, fault isolation or reconfiguration; Note:7E004.b.3. does not control "technology" for the design of physical redundancy. 4. flight controls which permit inflight reconfiguration of force and moment controls for real time autonomous air vehicle control; 5. integration of digital flight control, navigation and propulsion control data into a digital flight management system for "total control of flight"; Note:7E004.b.5. does not control: a. "development""technology" for integration of digital flight control, navigation and propulsion control data into a digital flight management system for "flight path optimisation"; b. "development""technology" for "aircraft" flight instrument systems integrated solely for VOR, DME, ILS or MLS navigation or approaches. 6. full authority digital flight control or multisensor mission management systems employing "expert systems"; N.B.:for "technology" for Full Authority Digital Engine Control ("FADEC"), see 9E003.a.9. c. "technology" for the "development" of helicopter systems, as follows: 1. multi-axis fly-by-wire or fly-by-light controllers which combine the functions of at least two of the following into one controlling element: a. collective controls;
9. "Tilting spindle" (2) means a tool-holding spindle which alters, during the machining process, the angular position of its centre line with respect to any other axis. "Time constant" (6) is the time taken from the application of a light stimulus for the current increment to reach a value of 1-1/e times the final value (i.e. 63 % of the final value). "Total control of flight" (7) means an automated control of "aircraft" state variables and flight path to meet mission objectives responding to real time changes in data regarding objectives, hazards or other "aircraft". "Total digital transfer rate" (5) means the number of bits, including line coding, overhead and so forth per unit time passing between corresponding equipment in a digital transmission system. N.B.:See also "digital transfer rate". "Tow" (1) is a bundle of "monofilaments", usually approximately parallel. "Toxins" (1 2) means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of "microorganisms". "Transfer laser" (6) means a "laser" in which the lasing species is excited through the transfer of energy by collision of a non-lasing atom or molecule with a lasing atom or molecule species. "Tunable" (6) means the ability of a "laser" to produce a continuous output at all wavelengths over a range of several "laser" transitions. A line selectable "laser" produces discrete wavelengths within one "laser" transition and is not considered "tunable". "Unmanned Aerial Vehicle" ("UAV") (9) means any aircraft capable of initiating flight and sustaining controlled flight and navigation without any human presence on board.