1. Field
The disclosure relates generally to a method and apparatus for installing fluid fittings and fasteners. More particularly, the present disclosure relates to a self-contained, combined wrench and marking system for installing and marking fluid fittings and fasteners, and to a method for installing and marking fluid fittings and fasteners.
2. Background
An aircraft includes many movable structures, for example and without limitation, wing flaps, vertical fins and ailerons, that are operated hydraulically. Accordingly, a typical aircraft may include many hydraulic lines that extend throughout the aircraft and that are comprised of numerous line sections joined together by fluid fittings.
The fittings are assembled to the line sections using nuts, and it is important that the assembled structures be fluid-tight. In a typical procedure for installing a hydraulic line in an aircraft, a mechanic first loosely attaches one end of a fitting to a line section by hand-tightening the nut at the one end of the fitting, then stretches or compresses the line section so that the opposite end of the fitting can be attached to another line section, again by hand-tightening the nut at the opposite end of the fitting. The mechanic then further tightens the nuts, first at one end and then at the opposite end of the fitting. This process of alternately tightening the nuts at the ends of the fitting may be repeated two or three times until the nuts at both ends of the fitting are fully tightened.
A mechanic may install several hundred hydraulic fittings in a day, and to help ensure that all nuts and fittings have been properly tightened, it is often the practice to mark a nut and/or fitting after it has been fully tightened.
As a result of the process of alternately and repeatedly tightening the nuts at the opposite ends of a fitting, however, it is not uncommon that the mechanic might inadvertently fail to fully tighten the nut at one or both ends of a fitting, yet still mark the nuts as being fully tightened.
All fittings in a hydraulic line of an aircraft are subjected to leak-testing such that any nuts that may have been only hand-tightened or that were otherwise improperly installed will be identified and properly fastened. When a fitting fails leak-testing, however, it is necessary to clean the leaked aviation hydraulic fluid (e.g., Skydrol) from surrounding surfaces, and to then fully tighten any loose nuts prior to retesting of the fitting. In addition to being time consuming, the preferred cleaning agent used to clean the leaked aviation hydraulic fluid is Freon which is a hazardous material and may also cause damage to the surrounding surfaces that requires repair.
Thus, it would be desirable to minimize the number of fittings that fail during leak-testing.
The typical procedure for marking an assembled hydraulic joint requires the mechanic to apply a colored compound, (e.g., Inspection seal lacquer F925) by squeezing a small tube so that a stripe of the compound, sometimes referred to as a “torque stripe”, covers both the fitting and the nut. This procedure for marking an installed hydraulic joint may be unsatisfactory.
One problem, as indicated above, is that the mechanic may inadvertently mark a fitting that has not been fully tightened. Also, these manual marking procedures are time consuming and reduce productivity. Recognizing the inadequacies of manual marking procedures, a marking wrench was developed. The prior art marking wrench both tightens a fastener and then marks the tightened nut with ink to indicate that the nut has been tightened.
The prior art marking wrench, however, is still not fully satisfactory. For one thing, the marking wrench only marks the nut and not its mating fitting. It is desirable to have the mark cover both nut and fitting so that it would be known if someone loosened, or tampered with the nut. A misaligned mark on the nut and fitting surfaces flags this condition. The prior art marking wrench is also non-ratcheting which makes operation of the wrench rather slow. Furthermore, the prior art marking wrench contacts the nut with ink impregnated felt, but trials of this wrench found that the felt dried up, rendering its marking capability useless.
There is, accordingly, a need for a mechanism for installing fittings and fasteners in hydraulic lines in an aircraft and in other applications that will minimize fluid leaks during leak-testing, and that will also automatically mark installed fittings and fasteners after they have been properly installed.
An embodiment of the disclosure provides a self-contained combined wrench and marking system. The self-contained combined wrench and marking system has a wrench that may include a wrench head for rotating a fastener during a fastener tightening operation, a torque measuring mechanism for measuring a torque applied to the fastener during the fastener tightening operation, and an angle measuring mechanism for rotating the fastener to a preset angle during the fastener tightening operation. The self-contained combined wrench and marking system also has a marking system for automatically marking the fastener after the torque is applied to the fastener and after rotating the fastener to the preset angle.
A further embodiment of the disclosure provides a self-contained combined wrench and marking system. The self-contained combined wrench and marking system has a wrench that may include a wrench head for tightening a fastener during a fastener tightening operation. The self-contained combined wrench and marking system also has a marking system for automatically marking the fastener after tightening the fastener. The marking system may include a marking fluid reservoir containing a marking fluid, a spray nozzle line connected to the marking fluid reservoir for receiving the marking fluid from the marking fluid reservoir, a replaceable gas cartridge containing a gas propellant, and a control valve for delivering the gas propellant from the replaceable gas cartridge to the spray nozzle line for spraying the marking fluid for marking the fastener.
A further embodiment of the disclosure provides a method for installing a fitting and for marking automatically an installed fitting. The method may include rotating a fastener to attach the fitting during a fastener tightening operation, measuring a torque applied to the fastener during the fastener tightening operation, and rotating the fastener to a preset angle during the fastener tightening operation. The method may also include marking automatically the installed fitting and the fastener after applying the torque to the fastener and after rotating the fastener to the preset angle.
A further embodiment of the disclosure provides a A self-contained combined wrench and marking system. The self-contained combined wrench and marking system has a wrench. The wrench may include a ratcheting wrench head for rotating a fastener during a fastener tightening operation, and a torque measuring mechanism for measuring a torque applied to the fastener during the fastener tightening operation. The torque measuring mechanism may include a strain-beam that is stressed during the fastener tightening operation, and a stress measuring mechanism for measuring an amount of stress on the strain-beam, wherein the amount of stress is related to torque. The wrench may also include an angle measuring mechanism for rotating the fastener to a preset angle during the fastener tightening operation, and the angle measuring mechanism may include a gyroscope. The self-contained combined wrench and marking system also has a marking system for automatically marking the fastener after the torque measuring mechanism determines that the torque applied to the fastener is equal to a preset torque value and after the angle measuring mechanism determines that the fastener is rotated to the preset angle. The marking system may include a marking fluid reservoir containing a marking fluid, a spray nozzle line connected to the marking fluid reservoir for receiving the marking fluid from the marking fluid reservoir, and a replaceable gas cartridge containing a gas propellant. A first control valve may deliver the gas propellant from the replaceable gas cartridge to the marking fluid reservoir for delivering the marking fluid from the marking fluid reservoir to the spray nozzle line, and a second control valve may deliver the gas propellant from the replaceable gas cartridge to the spray nozzle line for spraying the marking fluid for marking the fastener.
A further embodiment of the disclosure provides a method for installing a fitting and for marking automatically an installed fitting. The method includes a fastener tightening operation. The fastener tightening operation may include rotating a fastener to attach the fitting, measuring a torque applied to the fastener while rotating the fastener to apply a preset torque to the fastener, and measuring a rotation angle of the fastener while rotating the fastener for rotating the fastener to a preset angle to install the fitting. The method also includes a marking operation for marking automatically the installed fitting and the fastener. The marking operation may include delivering a gas propellant from a replaceable gas cartridge to a marking fluid reservoir for delivering a marking fluid from the marking fluid reservoir to a spray nozzle line, and delivering the gas propellant from the replaceable gas cartridge to the spray nozzle line for spraying the marking fluid from the spray nozzle line.
The features, functions, and advantages can be achieved independently in various embodiments or may be combined in yet other embodiments.
The novel features believed characteristic of the embodiments are set forth in the appended claims. The embodiments themselves, however, as well as a preferred mode of use, further objectives and advantages thereof, will best be understood by reference to the following detailed description of advantageous embodiments when read in conjunction with the accompanying drawings.
Referring more particularly to the drawings, embodiments of the disclosure may be described in the context of an aircraft manufacturing and service method 100 as shown in
Each of the processes of method 100 may be performed or carried out by a system integrator, a third party, and/or an operator (e.g., a customer). For the purposes of this description, a system integrator may include without limitation any number of aircraft manufacturers and major-system subcontractors; a third party may include without limitation any number of venders, subcontractors, and suppliers; and an operator may be an airline, leasing company, military entity, service organization, and so on.
As shown in
Apparatus and methods embodied herein may be employed during any one or more of the stages of the production and service method 100. For example, components or subassemblies corresponding to production process 106 may be fabricated or manufactured in a manner similar to components or subassemblies produced while the aircraft 200 is in service. Also, one or more apparatus embodiments, method embodiments, or a combination thereof may be utilized during the production stages 106 and 108, for example, by substantially expediting assembly of or reducing the cost of an aircraft 200. Similarly, one or more of apparatus embodiments, method embodiments, or a combination thereof may be utilized while the aircraft 200 is in service, for example and without limitation, to maintenance and service 114.
With reference now to
Returning to
Housing portion 304 may include housing body 312 covered by housing body cover 314. A display and control panel 316 may be mounted on housing body cover 314. Display and control panel 316, which is also illustrated in
Housing body 312 may also include ink refill port 332 for refilling an ink reservoir included in the marking system of marking wrench 300.
Nosepiece portion 306 includes a nosepiece body 534, which is illustrated in
Head portion 308 includes ratcheting head 340 of the marking wrench. Ratcheting head 340 is adapted to grip and rotate a nut, such as hydraulic nut 350 in
In an advantageous embodiment of the disclosure, marking wrench 300 may be used to install and mark hydraulic nuts and fittings to assemble hydraulic lines of an aircraft. It should be understood, however, that the marking wrench may also be used in other fastening applications and it is not intended to limit advantageous embodiments to any particular application.
According to an advantageous embodiment, marking wrench 300 may be about 17 inches long and weigh about two pounds. Marking wrench 300 may also be less than one inch thick, and thus provides a narrow profile in the plane of rotation of the marking wrench such that the marking wrench may be used in confined areas.
Gyroscope 506 may be used to measure the angle of rotation of a nut being rotated (displaced angle) by marking wrench 300, for example, hydraulic nut 350 in
Also illustrated in
Strain-beam 508 senses an amount by which it is bent. Specifically, when marking wrench 300 rotates a nut in a clockwise direction, nosepiece body 534 bends and pushes against strain-pin 510 which, in turn, applies a load onto strain-beam 508 causing it to bend. Through calibration, the amount of stress on the strain-beam as a result of being bent is related to torque, enabling torque to be measured.
More particularly, as a result of the bending of strain-beam 508, a voltage sent to the strain-beam changes, due to the strain-beam's change in resistance, then an instrumentation amplifier on main circuit board 502 amplifies this signal. The amplified voltage signal, or analog signal, is sent to a suitable microcontroller, such as a Microchip PIC microcontroller, on the main circuit board 502. The microcontroller has analog-to-digital converter capability so that the analog voltage can be converted to digital format. In digital format, the microcontroller can apply various measured and stored correction factors, such as the calibration factor, to compute torque.
The fluid system is generally designated by reference number 700. CO2 may be delivered by a disposable 16 gram, or other size, CO2 cylinder 702 which contains CO2 at approximately 900 psig. As shown in
The control program checks for over pressure as well as for under pressure because when the pressure in CO2 cylinder 702 drops from use, the low pressure left in the cylinder may cause regulator 704 to increase the outlet pressure to considerably above 25 psig.
Two lines of the four lines split from line 706 may supply flow to solenoid-actuated valves 710 and 712. Valve 710 may be used to operate pilot actuated valve 714 which, in turn, may inject ink into nozzle line 716 via ink line 718. Solenoid-actuated valve 712 may be used to flood nozzle line 716 with CO2 so as to propel the ink out spray nozzle 338 during a marking operation.
The fourth line split from line 706 may go directly into ink reservoir 720 which may comprise a low volume pump. A piston, schematically shown at 722, may separate the CO2 from the ink in reservoir 720 which is always pressurized. The ink should be pressurized so that it will function properly in all orientations of the marking wrench, especially when spraying in an overhead direction.
The following sequence of events may occur to actuate an ink spray shot:
Display 318 may be an LCD (liquid crystal display), and may display three seven-segment digits without decimal points which may be used to represent letters or numbers. For example,
On/Set button 320 has two functions. The On feature turns marking wrench 300 on and off. The Set feature may be used to set (store) a value into memory. Mode button 322 may be used for selecting a desired function among several available functions as will be described hereinafter.
Status lights 324, 326 and 328 may comprise LEDs (light emitting diodes) of three different colors. For example light 324 may be green, light 326 may be yellow, and light 328 may be red. According to an advantageous embodiment, green LED 324 may be on during torque measurement, yellow LED 326 may be on during angle measurement, and red LED 328 may go on when angle measurement is complete. In addition, red LED 328 may go on in conjunction with messages being displayed on display 318 to indicate a fault, such as that the battery needs changing, the CO2 cylinder needs replacing or that the gyroscope needs replacing.
As shown in
During the diagnostic sub-program (Step 1104) the gyroscope baseline may also be determined. The gyroscope baseline may be used to determine the nut angle, and should be determined while the marking wrench is not moving.
Returning to Step 1106, if an action is not required as a result of the diagnostic tests (No output of Step 1106), an options mode may be entered into to select options for operating the marking wrench (Step 1112). Entry into the options mode may be accomplished by pressing mode button 322 on display and control panel 316.
As shown in
A similar procedure is used when the other options shown in
Returning to
The torque measuring process is generally designated by dashed box 1116, and begins by display 318 displaying current torque (Step 1118). Display 318 may initially display 0 inch-pounds indicating that there is no load on the handle of the marking wrench. Green LED 324 may also turn on indicating that torque is being measured (Step 1120). The user then begins tightening a nut, ratcheting if necessary (Step 1122).
As the nut is tightened, a determination is made whether the measured torque is within a selected percentage of the preset torque value, for example, within 5 inch-pounds of the preset value (Step 1124). If the measured torque is not within 5 inch-pounds of the preset torque value (No output of Step 1124, the method returns to Step 1124 as the nut continues to be tightened. If the torque gets within 5 inch-pounds of the preset torque value (Yes output of Step 1124), buzzer 616 on main printed circuit board 502 may beep five times (Step 1126) as an indicator.
A determination is then made whether the measured torque is equal to the preset torque value (Step 1128). If the measured torque does not equal the preset torque value (No output of Step 1128), the method returns to Step 1128 as the nut continues to be tightened. If the measured torque equals the preset torque value (Yes output of Step 1128), the green LED may turn off and the yellow LED 326 may turn on ending the torque measuring process (Step 1130). The method then switches to an angle measuring mode.
The angle measuring process is generally designated by dashed box 1132, see
A determination is then made whether the measured angle is equal to the preset angle (Step 1142). If it is determined that the measured angle is not equal to the measured angle (No output of Step 1142), the method returns to Step 1142 and the user continues to tighten the nut. If it is determined that the measured angle is equal to the preset angle (Yes output of Step 1142), the red LED may go on to indicate that angle measurement is complete (Step 1144).
When the preset angle is reached, the wrench may also begin to vibrate (Step 1146). This indicates to the user that the wrench is ready to spray. After a time delay of one second, the marking wrench then sprays both the nut and the fitting (Step 1148). After the spraying, the marking wrench may automatically turn off (Step 1150).
Returning to
Nosepiece body 1402 of the combined wrench and marking system may include a stepper motor 1404 with gearbox which is controlled by the microcontroller 602 on the main circuit board of the combined wrench and marking system. The output shaft on the gearbox may be attached to blade coupling 1406 (shaped similar to a blade screwdriver) which is inserted into a blade receptacle (shaped similar to a slotted screw head) on valve stem 1408. Valve stem 1408 has exterior threads 1430 which mate with interior threads on nosepiece body 1402. Since connected together, by blade coupling 1406 and blade receptacle, rotation of the output shaft causes the valve stem 1408 to rotate in nosepiece body 1402. As this rotation occurs, the valve stem 1408 will either extend or retract into the nosepiece body 1402, depending on the rotation direction of the output shaft. This will cause the blade coupling 1406 to be withdrawn or be further inserted into the blade receptacle. The advantage of this coupling arrangement, is that the thrust force is applied on the threads 1430 and not onto the shaft of the stepper motor 1404.
In operation, ink pressurized to about 5 psig is directed into ink port 1410. No ink flows, however, until valve stem 1408 is retracted. When the stepper motor 1404 is signaled by the control program to rotate a certain number of steps, valve stem 1408 will rotate in nosepiece body 1402 causing the valve to retract from the front ink seal 1412. Retraction is dependent on the valve stem screw threads 1430.
At this point, ink is injected into mixing chamber 1414. The valve stem is then extended forward to seal front ink seal 1412. Then an electronic valve (not shown in
A combined wrench and marking system according to advantageous embodiments is completely self-contained and does not require connection to an external air line or to any other external source. As a result it is easy to handle and manipulate. Use of a combined wrench and marking system according to advantageous embodiments may reduce the number of hydraulic leaks that occur during leak-testing of a fitting that has been attached to a hydraulic line section because both the nut and the fitting are automatically marked only after the nut has been properly tightened. This will help ensure that joints that have not been properly assembled will not be inadvertently marked.
The combined wrench and marking systems according to advantageous embodiments is light in weight and compact in size. In addition, the combined wrench and marking systems according to advantageous embodiments is less than one inch thick and has no protruding components, and thus provides a narrow profile in the plane of rotation of the marking wrench such that the marking wrench may be used in confined areas.
The description of the different advantageous embodiments has been presented for purposes of illustration and description, and is not intended to be exhaustive or limited to the embodiments in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. Further, different advantageous embodiments may provide different advantages as compared to other advantageous embodiments. The embodiment or embodiments selected are chosen and described in order to best explain the principles of the embodiments, the practical application, and to enable others of ordinary skill in the art to understand the disclosure for various embodiments with various modifications as are suited to the particular use contemplated.
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Number | Date | Country | |
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20090114067 A1 | May 2009 | US |