Electrical equipment for connection to a tachometer for measuring a speed of rotation of a wheel of an aircraft landing gear
10890601 ยท 2021-01-12
Assignee
Inventors
Cpc classification
G01P21/00
PHYSICS
G01R31/52
PHYSICS
G01P3/60
PHYSICS
G01R31/008
PHYSICS
International classification
B60T8/88
PERFORMING OPERATIONS; TRANSPORTING
G01R31/50
PHYSICS
Abstract
An electrical equipment includes a calculator or a data concentrator for connecting to a tachometer via a cable that includes a measurement wire and a test wire. The electrical equipment has a measurement input to which the measurement wire can be connected and a test input to which the test wire can be connected, measurement acquisition components connected to the measurement input and arranged to acquire an electrical measurement signal present on the measurement wire and produced by the tachometer, test acquisition components connected to the test input and arranged to detect whether the test wire is or is not open-circuit, and processor components arranged to detect a break of the measurement wire if the test wire is open-circuit.
Claims
1. An electrical equipment comprising: a measurement input arranged to be connected to a measurement wire of a cable for connecting to a tachometer; a test input arranged to be connected to a test wire of the cable; measurement acquisition components connected to the measurement input and arranged to acquire an electrical measurement signal present on the measurement wire and produced by the tachometer; test acquisition components connected to the test input and arranged to detect whether the test wire is or is not open-circuit; and processor components arranged to detect a break of the measurement wire if the test wire is open-circuit.
2. The electrical equipment according to claim 1, wherein the test input is a discrete input, and wherein the test acquisition components are arranged to detect a discrete open-circuit signal or a discrete ground signal.
3. The electrical equipment according to claim 2, the electrical equipment including a first test input and a second test input, the first test input being for connecting to the test wire and the second test input being connected to an electrical ground of the electrical equipment.
4. The electrical equipment according to claim 1, wherein the test acquisition components are arranged to measure a test resistance.
5. The electrical equipment according to claim 4, wherein the test resistance is a resistance between the test input and an electrical ground of the electrical equipment.
6. The electrical equipment according to claim 4, wherein the electrical equipment includes a first test input and a second test input, the test resistance being a resistance between the first test input and the second test input.
7. A system comprising: a tachometer; a cable including a measurement wire and a test wire; and an electrical equipment comprising: a measurement input connected to the measurement wire of the cable; a test input connected to a test wire of the cable; measurement acquisition components connected to the measurement input and arranged to acquire an electrical measurement signal present on the measurement wire and produced by the tachometer; test acquisition components connected to the test input and arranged to detect whether the test wire is or is not open-circuit; and processor components arranged to detect a break of the measurement wire if the test wire is open-circuit, wherein the cable has a first end connected to the tachometer and a second end connected to the electrical equipment.
8. The system according to claim 7, wherein the measurement wire and the test wire are twisted together.
9. The system according to claim 7, wherein the test wire is connected to tachometer ground at the first end of the cable.
10. The system according to claim 7, wherein the tachometer includes an electric circuit having a resistor connected therein, and wherein the test wire is connected to tachometer ground via the resistor.
11. The system according to claim 7, wherein the cable has two test wires, wherein the tachometer has an electrical circuit having a resistor connected therein, and wherein each test wire is connected to a distinct terminal of the resistor.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Reference is made to the accompanying drawings, in which:
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION OF THE INVENTION
(7) With reference to
(8) The calculation means 1 are situated in a hold of an aircraft.
(9) The calculation means 1 comprise a casing 4 containing measurement acquisition components 7, test acquisition components 8, and processor components 9.
(10) The calculation means 1 comprises a first measurement input 11 and a second measurement input 12. The first measurement input 11 and the second measurement input 12 are connected to the measurement acquisition components 7.
(11) The calculation means 1 also include a test input 14. The test input 14 is a discrete input. The test input 14 is connected to the test acquisition components 8.
(12) The test acquisition components 8 can be seen in
(13) The test acquisition components 8 comprise resistors 17 and 18 connected to the test input 14, a reference voltage source 19 connected via a resistor 21 to a point P situated between the resistors 17 and 18, and a resistor 22 connected between the resistor 18 and electrical ground 23 of the calculation means 1. The test acquisition component 8 also includes a lowpass filter 25 and a hysteresis comparator 26. An input of the lowpass filter 25 is connected to the resistor 18 and to the resistor 22. An output of the lowpass filter 25 is connected to an input of the hysteresis comparator 26.
(14) The electrical ground 23 is connected to the casing 4 of the calculation means 1.
(15) The tachometer 2 is for measuring the speed of rotation of an aircraft landing-gear wheel. The tachometer 2 comprises a casing 30 incorporating a speed-of-rotation sensor. The speed-of-rotation sensor comprises a rotor and a stator that includes a winding 31.
(16) In this example, part of the length of the cable 3 is located in a harness that groups together a plurality of similar cables connected to tachometers. The harness runs from the landing gear to the hold of the aircraft.
(17) The cable 3 has a first end 33 and a second end 34. The first end 33 is connected to the tachometer 2. The second end 34 is connected to the calculation means 1.
(18) The cable 3 has a first measurement wire 36, a second measurement wire 37, and a test wire 38. The first measurement wire 36, the second measurement wire 37, and the test wire 38 are twisted together, i.e. they are wound helically about one another.
(19) At the first end 33 of the cable 3, the first measurement wire 36 is connected to a first terminal of the stator winding 31. The second measurement wire 37 is connected to a second terminal of the stator winding 31. The test wire 38 is connected to ground 39 of the tachometer 2 via shielding of the harness or of the cable 3, or indeed via a mechanical body of the tachometer 2 if the casing 30 of the tachometer 2 is referenced to ground.
(20) At the second end 34 of the cable 3, the first measurement wire 36 is connected to the first measurement input 11 of the calculation means 1, the second measurement wire 37 is connected to the second measurement input 12, and the test wire 38 is connected to the test input 14.
(21) The measurement acquisition components 7 of the calculation means 1 acquire an electrical measurement signal of voltage and/or frequency representative of the speed of rotation of the wheel.
(22) The test acquisition components 8 compare a test voltage Vt at the input to the hysteresis comparator 26 with a detection threshold, specifically a predetermined voltage threshold. The test voltage Vt is representative of the impedance connected to the test input 14.
(23) If the test voltage Vt is below the predetermined voltage threshold, the test acquisition components 8 detect that a discrete ground signal is being applied of the test input 14. The ground signal corresponds to the test wire 38 being connected to the ground 39 of the tachometer 2 at the first end 33 of the cable 3.
(24) The processor components 9 then detect continuity of the test wire 38, and thus that the test wire 38 has not been broken. The processor components 9 therefore do not detect a break in the first measurement wire 36 or in the second measurement wire 38. Specifically, because of the proximity between the test wire 38 and the first and second measurement wires 36 and 37, a break in the test wire 38, e.g. due to a tire bursting, will very probably be accompanied by a break in the first measurement wire 36 or in the second measurement wire 37.
(25) If the test voltage Vt is greater than or equal to the predetermined voltage threshold, the test acquisition components 8 detect that a discrete open-circuit signal is being applied to the test input 14. The open circuit corresponds to the test wire 38 being open-circuit.
(26) The processor components 9 then detect a break in the test wire 38, and thus a break in the first measurement wire 36 and/or in the second measurement wire 37. The processor components 9 then invalidate speed-of-rotation measurement from the electrical measurement signal, deactivating the tachometer 2, and generating a fault message.
(27) With reference to
(28) The calculation means in this example have a first test input 101 and a second test input 102. The first test input 101 and the second test input 102 are both discrete inputs. The calculation means has test acquisition components 103. Once more, the test acquisition components 103 are components for acquiring a discrete signal.
(29) The test acquisition components 103 comprise an operational amplifier 104, a lowpass filter 105, and a hysteresis comparator 106.
(30) A non-inverting input of the operational amplifier 104 is connected to the first test input 101 via a resistor 107. An inverting input of the operational amplifier 104 is connected to the second test input 102 via a resistor 108.
(31) The test wire is connected to the first test input 101.
(32) The second test input 102 is connected to electrical ground 110 of the calculation means, e.g. via the casing of the calculation means or via the shielding of the harness or of the cable.
(33) A first reference current source 111 is connected to the non-inverting input via a resistor 112. A second reference current source 113 is connected to the inverting input via a resistor 114.
(34) An output from the operational amplifier 104 is connected to an input of the lowpass filter 105. An output of the lowpass filter 105 is connected to an input of the hysteresis comparator 106.
(35) Once more, the test acquisition components 103 compare a test voltage Vt input to the hysteresis comparator 106 with a predetermined voltage threshold. The test voltage Vt is representative of the impedance applied between the first test input 101 and the second test input 102.
(36) If the test voltage Vt is less than the predetermined voltage threshold, the test acquisition components 103 detect that a discrete ground signal is being applied to the first test input 101.
(37) The processor components then detect continuity of the test wire, and thus that the test wire has not been broken. The processor components therefore do not detect a break in the first measurement wire or in the second measurement wire.
(38) If the test voltage Vt is greater than the predetermined voltage threshold, the test acquisition components 103 detect that an open-circuit discrete signal is being applied to the first test input 101.
(39) The processor components then detect a break in the test wire, and thus a break in the first measurement wire and/or in the second measurement wire. The processor components invalidate speed-of-rotation measurements from the electrical measurement signal, deactivating the tachometer and generating a fault message.
(40) With reference to
(41) The tachometer 202 includes an electric circuit having a resistor 204 connected therein. The test wire 205 is connected to ground 206 of the tachometer 202 via the resistor 204.
(42) The calculation means 201 include a test input 207 connected to the test wire 205. In this example, the test acquisition components 208 are components for measuring resistance.
(43) The test acquisition components 208 include a first input 210 connected to the test input 207 of the calculation means 201, and a second input 211 connected to electrical ground of the calculation means 201.
(44) The test acquisition components 208 measure a test resistance between the first input 210 and the second input 211, and thus between the test input 207 and electrical ground of the calculation means 201.
(45) If the test resistance is less than a predetermined resistance threshold, the test acquisition components 208 do not detect that the test wire 205 is open-circuit. The processor components 212 detect that the test wire 205 is not broken.
(46) If the test resistance is greater than or equal to a predetermined resistance threshold, then the test acquisition components 208 detect that the test wire 205 is open-circuit.
(47) The processor components 212 thus detect that the test wire 205 is broken and thus that the first measurement wire and/or the second measurement wire is broken. The processor components 212 invalidate speed-of-rotation measurements from the electrical measurement signal, deactivating the tachometer and generating a fault message.
(48) With reference to
(49) In the fourth embodiment of the invention, the cable 303 has a first test wire 305 and a second test wire 306.
(50) At a first end 307 of the cable 303, the first test wire 305 is connected to a first terminal of a resistor 308 in the tachometer 302. At the first end 307 of the cable 303, the second test wire 306 is connected to a second terminal of the resistor 308.
(51) At a second end 309 of the cable 303, the first test wire 305 is connected to a first test input 311 of the calculation means 301. At the end second end 309 of the cable 303, the second test wire 306 is connected to a second test input 312 of the calculation means 301.
(52) The test acquisition components 314 include a first input 315 connected to the first test input 311 of the calculation means 301, and a second input 316 connected to the second test input 312 of the calculation means 301.
(53) Once more, the test acquisition components 314 are components for measuring resistance.
(54) The test acquisition components 314 measure a test resistance between the first input 315 and the second input 316, and thus between the first test input 311 and the second test input 312 of the calculation means 301.
(55) If the test resistance lies within a valid range of resistance values, then the processor components 317 detect that the first test wire 305 and the second test wire 306 are not broken.
(56) If the test resistance does not lie in the valid range of resistance values, then the processor components 317 detect that the first test wire 305 and/or the second test wire 306 is/are broken.
(57) The processor components 317 then detect a break in the first measurement wire 318 and/or the second measurement wire 319. The processor components 317 invalidate speed-of-rotation measurements from the electrical measurement signal, deactivating the tachometer and generating a fault message.
(58) Naturally, the present invention is not limited to the embodiments described but covers any variant coming within the field of the invention as defined by the claims.
(59) Although the electrical equipment described above comprises calculation means, the electrical equipment could be different, e.g. a data concentrator.