CN210391591U - Multifunctional assembling and adjusting equipment for aircraft landing system interception piece - Google Patents
Multifunctional assembling and adjusting equipment for aircraft landing system interception piece Download PDFInfo
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- CN210391591U CN210391591U CN201921268174.0U CN201921268174U CN210391591U CN 210391591 U CN210391591 U CN 210391591U CN 201921268174 U CN201921268174 U CN 201921268174U CN 210391591 U CN210391591 U CN 210391591U
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Abstract
The utility model provides a multifunctional assembling and debugging device for an interception piece of an aircraft landing system, wherein a universal traction device is used for transporting the multifunctional assembling and debugging device for the interception piece of the aircraft landing system for loading the interception piece; the stability augmentation device is used for stably loading multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system of the interception piece; the lifting device adjusts the height of the lifting device through a hydraulic power device, so that the height and the angle of the intercepting piece are adjusted; the transverse adjusting device is used for adjusting the transverse position of the intercepting piece; the supporting follow-up device is arranged on the transverse adjusting device and used for connecting and supporting the intercepting piece. The utility model provides a multi-functional installation and debugging equipment of aircraft landing system interception piece novel structure, degree of automation is high, and work efficiency, safety index are high.
Description
Technical Field
The utility model belongs to the technical field of aircraft assembly, debugging, concretely relates to multi-functional debugging equipment of aircraft landing system interception piece.
Background
In an aircraft landing control system, three major parts of assembly, control and debugging of parts are involved. The most important part of the system is the adjustment of the interception piece, and as the aircraft landing system needs the interception piece to hook the steel cable on the ground after the aircraft lands on a runway, the speed of the aircraft is reduced to zero. Therefore, the intercepting part has larger self weight and appearance structure size when being designed, is limited by narrow working space, is extremely inconvenient to assemble and debug, can finish the assembling and debugging work of the aircraft landing system basically by the simultaneous coordinated operation of 10 persons, and has low working efficiency and low safety factor. Secondly, the interception piece in the landing system is in a folding state in the normal takeoff and flight process of the airplane, when the airplane is in various flight states in the air, a certain gap value between the interception piece and the airplane is ensured, otherwise the airplane structure is damaged, and the function of the landing system of the airplane is seriously affected, so that the gap measurement is required to be carried out on each position of the interception piece in the folding state, the adjustment is carried out, and the limitation is caused by the narrow operation space and the structural specificity of the interception piece.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a multi-functional debugging equipment of aircraft landing system interception piece and application method to solve the above-mentioned problem among the prior art.
The technical scheme of the utility model is that:
a multifunctional assembling and adjusting device for an aircraft landing system interception piece comprises a trolley lifting chassis 17, and a universal traction device, a stability augmentation device 1, a lifting device, a hydraulic power device, a transverse adjusting device and a supporting follow-up device which are arranged on the trolley lifting chassis 17.
The universal traction device is used for transporting multifunctional assembling and adjusting equipment for the interceptor of the aircraft landing system for loading the interceptor; the stability augmentation device 1 is arranged at the four corners of the vehicle erecting chassis 17 and is used for stabilizing the multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system loading the interception piece; the front end and the rear end above the car lifting chassis 17 are respectively provided with a lifting device, and the lifting device adjusts the height of the lifting device through a hydraulic power device, so that the height and the angle of the intercepting piece are adjusted; the transverse adjusting device is arranged on the lifting device and used for adjusting the transverse position of the intercepting piece; the supporting follow-up device is arranged on the transverse adjusting device and used for connecting and supporting the intercepting piece.
The universal traction device comprises a universal connector 13, a brake device 14, a power driving handle 15, a universal guide wheel 18 and a pulley 21; wherein, the universal guide wheel 18 is arranged at the front end below the vehicle erecting chassis 17, the pulley 21 is arranged at the rear end below the vehicle erecting chassis 17, and the braking device 14 and the power driving handle 15 are connected through the universal connector 13 on the side wall of the front end of the vehicle erecting chassis 17. The power-driven handle 15 is used for starting the electric consignment system and moving the multifunctional assembly and adjustment equipment of the interception piece of the aircraft landing system by driving the universal guide wheel 18 and the pulley 21.
The stability augmentation device 1 is arranged at the four corners of the vehicle erecting chassis 17, the stability augmentation device 1 comprises a connecting arm and a stability augmentation jack, one end of the connecting arm is connected with the vehicle erecting chassis 17, and the other end of the connecting arm is connected with the stability augmentation jack. After the multifunctional installing and adjusting equipment for the aircraft landing system interceptor loaded with the interceptor is transported to the installing position of the interceptor, the connecting arm of each stability augmentation device 1 is opened, and the stability augmentation jack of each stability augmentation device 1 is adjusted to be in close contact with the ground, so that the stability of the multifunctional installing and adjusting equipment for the aircraft landing system interceptor loaded with the interceptor is ensured.
The lifting device comprises a lifting hinge mechanism slide rail bracket 11 and a lifting hinge mechanism 12, one end of the lifting hinge mechanism 12 is connected with the lifting hinge mechanism slide rail bracket 11, and the other end is connected to the vehicle erecting chassis 17.
The hydraulic power device comprises a hand-operated hydraulic pump 2 and a hydraulic actuating cylinder 3, the hand-operated hydraulic pump 2 is arranged on the side wall of the rear end of the chassis 17 of the trolley, and the hydraulic actuating cylinder 3 is connected with the lifting hinge mechanism 12 and used for providing power for lifting of the lifting hinge mechanism 12.
Horizontal adjusting device including setting up horizontal step motor 4 on lifting hinge mechanism slide rail bracket 11, forked tail slide rail 9 and forked tail slide rail groove 10, horizontal step motor 4 fixes the one end at forked tail slide rail 9 through the mounting hole of its base, its output shaft passes through the lead screw and constitutes slider with forked tail slide rail groove 10, make forked tail slide rail groove 10 turn into the horizontal displacement of forked tail slide rail groove 10 on forked tail slide rail 9 through the axial displacement volume of horizontal step motor 4, be used for when the horizontal assembly angle of interception piece is improper, transversely adjust the mounted position.
Support servo device include multi-angle bracket 6 and support frame 7, support frame 7 sets up on forked tail slide rail groove 10, multi-angle bracket 6 connects on support frame 7, when interception piece slope installation and debugging in-process, provides the bracket device that a multi-angle closely supported.
In a specific embodiment, the multifunctional assembling and adjusting equipment for the intercepting part of the aircraft landing system is further provided with an electric control lifting and shifting operation panel 16 and an electric control system 19, wherein the electric control lifting and shifting operation panel 16 is connected with the electric control system 19, and the electric control system 19 is connected with a lifting device, a transverse adjusting device and a universal traction device and is used for adjusting the lifting and moving of the lifting device and the transverse adjusting device and the moving of the multifunctional assembling and adjusting equipment for the intercepting part of the aircraft landing system.
In a particular embodiment, the aircraft landing system interceptor multi-functional rigging equipment is further provided with an anti-skid support 5 attached to the side wall of the slide bracket 11 of the aft end of the lifting hinge mechanism for preventing the interceptor from sliding down when installed at an oblique angle.
In a specific embodiment, the multifunctional debugging device for the aircraft landing system interceptor is further provided with a nitrogen cylinder 20, and the nitrogen cylinder 20 is arranged between the two lifting devices and used for providing compressed nitrogen required by debugging for the interceptor.
The utility model discloses an effect and benefit are:
(1) the utility model provides a multi-functional debugging equipment of aircraft landing system interception piece novel structure collects assembly, debugging, measurement, manipulates in the comprehensive machinery debugging equipment of an organic whole, and this equipment degree of automation is not only high, and work efficiency is high moreover, and four nimble steady devices that increase have not only reduced the volume of whole equipment, but also can strictly guarantee the stability of whole equipment.
(2) The multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system adopts the hand-operated hydraulic pump as a power device of a front hinge lifting system and a rear hinge lifting system of the whole equipment and the flexible hydraulic system, so that the whole interception piece is always in a stable lifting state in the lifting process, the whole assembling process can be completed by only 1-2 people, the working strength is reduced by 3-4 times, and the safety and the reliability of the whole assembling process are greatly improved.
(3) The transverse adjusting device of the multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system adopts the adjusting device consisting of the transverse stepping motor 4, the dovetail slide rail 9 and the dovetail slide rail groove 10, so that after the interception piece reaches the specified installation height, micro-installation and adjustment can be carried out transversely through the electric control lifting and shifting operation panel 16, the adjusting mode is simplified, and the installation precision is ensured.
(4) The whole installation and debugging process of the multifunctional installation and debugging equipment for the aircraft landing system interception piece adopts the hydraulic system, the electric control system and the air pressure system, so that the special flexibility is embodied in the aspect of consigning heavy interception parts, and the multifunctional installation and debugging equipment is also applicable in the aspect of debugging.
(5) The multifunctional installing and debugging equipment for the interception piece of the landing system of the aircraft adopts the multi-angle bracket 6 and the support frame 7 to form a bracket device, can adapt to the installation and debugging work of various angles of the interception piece, changes the working mode that a plurality of functional trolley frames need to be prepared for assembling and debugging the interception piece in the prior art, and greatly improves the whole working efficiency and reliability.
Drawings
Fig. 1 is a schematic structural view of a multifunctional debugging device for an aircraft landing system intercepting part provided in an embodiment of the present invention.
In the figure: the device comprises a stability augmentation device 1, a manual hydraulic pump 2, a hydraulic actuator cylinder 3, a transverse stepping motor 4, an anti-skid support 5, a multi-angle bracket 6, a support frame 7, a dovetail slide rail 9, a dovetail slide rail groove 10, a slide rail bracket of a lifting hinge mechanism 11, a lifting hinge mechanism 12, a universal connector 13, a brake device 14, a power driving handle 15, an electric control lifting and shifting operation panel 16, a vehicle chassis 17, a universal guide wheel 18, an electric control system 19, a nitrogen cylinder 20 and a pulley 21.
Detailed Description
The following further describes a specific embodiment of the present invention with reference to the drawings and technical solutions.
It is to be understood that the appended drawings are not to scale, but are merely drawn with appropriate simplifications to illustrate various features of the basic principles of the invention. Specific design features of the invention disclosed herein, including, for example, specific dimensions, orientations, locations, and configurations, will be determined in part by the particular intended application and environment of use.
In the several figures of the drawings, identical or equivalent components (elements) are referenced with the same reference numerals.
In the description of the present invention, it should be noted that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
Fig. 1 is a schematic structural view of a multifunctional debugging device for an aircraft landing system intercepting part provided in an embodiment of the present invention. Referring to fig. 1, in this embodiment, the multifunctional assembling and adjusting device for the interception member of the aircraft landing system comprises a vehicle erecting chassis 17, and a universal traction device, a stability augmentation device 1, a lifting device, a hydraulic power device, a transverse adjusting device and a support follow-up device which are arranged on the vehicle erecting chassis 17.
The universal traction device is used for transporting multifunctional assembling and adjusting equipment for the interceptor of the aircraft landing system for loading the interceptor; the stability augmentation device 1 is arranged at the four corners of the vehicle erecting chassis 17 and is used for stabilizing the multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system loading the interception piece; the front end and the rear end above the car lifting chassis 17 are respectively provided with a lifting device, and the lifting device adjusts the height of the lifting device through a hydraulic power device, so that the height and the angle of the intercepting piece are adjusted; the transverse adjusting device is arranged on the lifting device and used for adjusting the transverse position of the intercepting piece; the supporting follow-up device is arranged on the transverse adjusting device and used for connecting and supporting the intercepting piece.
Specifically, in the present embodiment, the universal traction device includes a universal connector 13, a brake device 14, a power driving handle 15, a universal guide wheel 18 and a pulley 21; wherein, the universal guide wheel 18 is arranged at the front end below the vehicle erecting chassis 17, the pulley 21 is arranged at the rear end below the vehicle erecting chassis 17, and the braking device 14 and the power driving handle 15 are connected through the universal connector 13 on the side wall of the front end of the vehicle erecting chassis 17. The power driving handle 15 is used for starting the electric consignment system, the multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system is moved by driving the universal guide wheel 18 and the pulley 21, and the interception piece can be transported to each position by adopting electric power after being transported to the equipment, so that the labor amount is reduced.
The stability augmentation device 1 is arranged at the four corners of the vehicle erecting chassis 17, the stability augmentation device 1 comprises a connecting arm and a stability augmentation jack, one end of the connecting arm is connected with the vehicle erecting chassis 17, and the other end of the connecting arm is connected with the stability augmentation jack. After the multifunctional installing and adjusting equipment for the aircraft landing system interceptor loaded with the interceptor is transported to the installing position of the interceptor, the connecting arm of each stability augmentation device 1 is opened, and the stability augmentation jack of each stability augmentation device 1 is adjusted to be in close contact with the ground, so that the stability of the multifunctional installing and adjusting equipment for the aircraft landing system interceptor loaded with the interceptor is ensured.
The lifting device comprises a lifting hinge mechanism slide rail bracket 11 and a lifting hinge mechanism 12, one end of the lifting hinge mechanism 12 is connected with the lifting hinge mechanism slide rail bracket 11, and the other end is connected to the vehicle erecting chassis 17.
The hydraulic power device comprises a hand-operated hydraulic pump 2 and a hydraulic actuator cylinder 3, wherein the hand-operated hydraulic pump 2 is arranged on the side wall of the rear end of the chassis 17 of the trolley, and the hydraulic actuator cylinder 3 is connected with the lifting hinge mechanism 12 and used for providing power for lifting of the lifting hinge mechanism 12.
The transverse adjusting device comprises a transverse stepping motor 4, a dovetail slide rail 9 and a dovetail slide rail groove 10 which are arranged on a slide rail bracket 11 of a lifting hinge mechanism, wherein: horizontal step motor 4 is fixed in the one end of forked tail slide rail 9 through the mounting hole of its base, and its output shaft passes through the lead screw and constitutes slider with forked tail slide rail groove 10 for forked tail slide rail groove 10 turns into the lateral displacement of forked tail slide rail groove 10 on forked tail slide rail 9 through the axial displacement volume of horizontal step motor 4, and when the horizontal assembly angle of interception piece is improper, can transversely adjust the mounted position as required.
Support follow-up device and include multi-angle bracket 6 and support frame 7, support frame 7 sets up on forked tail slide rail groove 10, and multi-angle bracket 6 connects on support frame 7, when interception piece slope installation and debugging in-process, provides the bracket device that a multi-angle closely supported.
In a specific embodiment, the multifunctional assembling and adjusting equipment for the intercepting part of the aircraft landing system is further provided with an electric control lifting and shifting operation panel 16 and an electric control system 19, wherein the electric control lifting and shifting operation panel 16 is connected with the electric control system 19, and the electric control system 19 is connected with a lifting device, a transverse adjusting device and a universal traction device and is used for adjusting the lifting and moving of the lifting device and the transverse adjusting device and the moving of the multifunctional assembling and adjusting equipment for the intercepting part of the aircraft landing system.
In a specific embodiment, the multifunctional assembling and adjusting device for the interception piece of the aircraft landing system is also provided with an anti-skid support 5 which is connected with the side wall of a slide rail bracket 11 of a lifting hinge mechanism at the rear end, and when the interception piece is installed at a certain inclined angle, the interception piece is prevented from sliding downwards to play a role of blocking.
In a specific embodiment, the multifunctional installation and adjustment equipment for the interceptor of the aircraft landing system is further provided with a nitrogen cylinder 20, and the nitrogen cylinder 20 is arranged between the two lifting devices and used for providing compressed nitrogen required by debugging for the interceptor, so that the flexibility and the versatility of the equipment are improved.
The use of the multifunctional debugging equipment for the aircraft landing system interception piece comprises the following steps:
(1) the interceptor is carried to the multi-angle bracket 6 on the multifunctional interceptor installation and adjustment equipment of the aircraft landing system, and then the electric consignment system is started through the power-driven handle 15 to consign the interceptor to the installation position on the aircraft.
(2) Adjusting the installation position of the interception piece, opening the four stability augmentation devices 1, shaking the handle of the hand-operated hydraulic pump 2, observing the level gauge, and adjusting the level of the multifunctional installation and adjustment equipment of the interception piece of the aircraft landing system.
(3) The front hinge change-over switch and the rear hinge change-over switch of the hand-operated hydraulic pump 2 are adjusted to the position of 'the front hinge and the rear hinge are lifted simultaneously', the handle of the hand-operated hydraulic pump 2 is shaken to lift the interception piece to a certain height, then the change-over switch of the hand-operated hydraulic pump 2 is changed to the position of 'the front hinge is lifted', the handle of the hand-operated hydraulic pump 2 is shaken to enable the interception piece to incline at a certain angle until the mounting hole of the interception piece is completely coincided with the mounting hole on the machine.
(4) If the transverse deviation occurs in the centering process of the mounting holes of the intercepting parts, at the moment, the transverse stepping motors 4 at the front end and the rear end drive the dovetail slide rail grooves 10 to transversely finely adjust the intercepting parts through the transverse adjusting knobs on the electric control lifting and shifting operation panel 16 until the mounting holes of the intercepting parts are concentric with the mounting holes of the airplane, and the intercepting parts and the mounting holes are connected through the positioning large shaft, namely the assembly work is finished.
(5) One end of the inflatable belt is connected to the nitrogen gas bottle 20, the other end of the inflatable belt is connected to the air pressure buffer strut of the interception piece, the inflation switch is turned on, the interception piece is inflated with compressed nitrogen with the specified pressure of P1, the buffer strut is completely ejected, and then the compressed nitrogen in the interception piece is discharged by the deflation switch of the inflatable belt.
(6) Adjusting the support adjusting baffle, clamping the measuring device at the measuring point of the intercepting piece, and screwing the support adjusting baffle tightly.
(7) The front hinge change-over switch of the hand-operated hydraulic pump 2 is adjusted to the position of 'front hinge descending', the handle of the hand-operated hydraulic pump 2 is shaken, the front hinge bracket is descended to the initial position, the rear hinge change-over switch of the hand-operated hydraulic pump 2 is converted to the 'ascending' position, the handle of the hand-operated hydraulic pump 2 is shaken, and the rear end of the interception piece is gradually ascended until the air pressure buffering support column is contacted with the aircraft skin.
(8) The measuring tool is clamped on the structure of the intercepting part, the handle of the hand-operated hydraulic pump 2 is shaken, so that the intercepting part is gradually lifted, and the related gap data of the intercepting part is monitored and measured in real time in different rows.
(9) After the work is finished, a rear hinge change-over switch of the hand-operated hydraulic pump 2 is switched to a descending position, a handle of the hand-operated hydraulic pump 2 is shaken to enable the rear end of the intercepting piece to gradually descend to an initial position, the intercepting piece is charged with specified compressed nitrogen again through an inflatable belt, then a jack of the stability augmentation device 1 is separated from the ground, and the trolley is taken out of a retraction working area of the intercepting piece.
(10) The aircraft cockpit is connected with a full-aircraft power supply, a ground pump station system establishes a specified working pressure P2 for the aircraft, the cockpit dials the retraction switch of the intercepting part to the 'retraction' position, the intercepting part is observed until the locking hook of the intercepting part is locked in the retraction process, the compression amount of the stroke of the strut is buffered, and the clearance values of structures at each position corresponding to different compression amounts are recorded. If the gap is not good, the corresponding pull rod needs to be further adjusted and then rechecked.
(11) And if the adjustment work is finished, the measuring device is detached from the measuring point of the intercepting piece, the work is finished, and the trolley is moved to the tool area.
It can be seen that, the utility model provides a multi-functional debugging equipment of aircraft landing system interception piece collects installation, debugging, manipulates in an organic whole, and it can be accomplished the debugging measurement work of heavy weight, nonstandard overall dimension part by 2 people in narrow and small space, and diversified assurance should take off landing system's the stability and measured data's accurate nature. The device has novel structure and high automation degree, integrates installation, debugging and measurement operation into a whole, and has high working efficiency, safety index and measurement precision.
The above description of exemplary embodiments has been presented only to illustrate the technical solutions of the present invention, and is not intended to be exhaustive or to limit the present invention to the precise forms described. Obviously, many modifications and variations are possible in light of the above teaching to those skilled in the art. The exemplary embodiments were chosen and described in order to explain certain principles of the invention and its practical application to thereby enable others skilled in the art to understand, implement and utilize the invention in various exemplary embodiments and with various alternatives and modifications. It is intended that the scope of the invention be defined by the following claims and their equivalents.
Claims (5)
1. The multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system is characterized by comprising a trolley erecting chassis (17), a universal traction device, a stability augmentation device (1), a lifting device, a hydraulic power device, a transverse adjusting device and a supporting follow-up device, wherein the universal traction device, the stability augmentation device (1), the lifting device, the hydraulic power device, the transverse adjusting device and the supporting follow-up device are arranged on the trolley erecting chassis (17); wherein the content of the first and second substances,
the universal traction device is used for transporting multifunctional assembling and adjusting equipment for the interceptor of the aircraft landing system for loading the interceptor; the stability augmentation device (1) is arranged at the four corners of the trolley chassis (17) and is used for stably loading multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system of the interception piece; the front end and the rear end above the car lifting chassis (17) are respectively provided with a lifting device, and the lifting device adjusts the height of the lifting device through a hydraulic power device, so that the height and the angle of the intercepting piece are adjusted; the transverse adjusting device is arranged on the lifting device and used for adjusting the transverse position of the intercepting piece; the supporting follow-up device is arranged on the transverse adjusting device and used for connecting and supporting the intercepting piece;
the universal traction device comprises a universal connector (13), a brake device (14), a power driving handle (15), a universal guide wheel (18) and a pulley (21); wherein, the universal guide wheel (18) is arranged at the front end below the car erecting chassis (17), the pulley (21) is arranged at the rear end below the car erecting chassis (17), and the side wall of the front end of the car erecting chassis (17) is connected with the brake device (14) and the power driving handle (15) through the universal connector (13); the power driving handle (15) is used for starting the electric consignment system, and moving the multifunctional assembling and adjusting equipment for the interception piece of the aircraft landing system by driving the universal guide wheel (18) and the pulley (21);
the stability augmentation device (1) is arranged at the four corners of the vehicle erecting chassis (17), the stability augmentation device (1) comprises a connecting arm and a stability augmentation jack, one end of the connecting arm is connected with the vehicle erecting chassis (17), and the other end of the connecting arm is connected with the stability augmentation jack; after the multifunctional installation and adjustment equipment for the interception piece of the aircraft landing system loading the interception piece is transported to the installation position of the interception piece, the connecting arm of each stability augmentation device (1) is opened, and the stability augmentation jack of each stability augmentation device (1) is adjusted to be in close contact with the ground so as to ensure the stability of the multifunctional installation and adjustment equipment for the interception piece of the aircraft landing system loading the interception piece;
the lifting device comprises a lifting hinge mechanism slide rail bracket (11) and a lifting hinge mechanism (12), one end of the lifting hinge mechanism (12) is connected with the lifting hinge mechanism slide rail bracket (11), and the other end is connected to the vehicle erecting chassis (17);
the hydraulic power device comprises a hand-operated hydraulic pump (2) and a hydraulic actuator cylinder (3), the hand-operated hydraulic pump (2) is arranged on the side wall of the rear end of the chassis (17) of the trolley, and the hydraulic actuator cylinder (3) is connected with the lifting hinge mechanism (12) and used for providing power for lifting of the lifting hinge mechanism (12);
the transverse adjusting device comprises a transverse stepping motor (4), a dovetail slide rail (9) and a dovetail slide rail groove (10), wherein the transverse stepping motor (4) is arranged on a slide rail bracket (11) of the lifting hinge mechanism, the transverse stepping motor (4) is fixed at one end of the dovetail slide rail (9) through a mounting hole of a base of the transverse stepping motor, and an output shaft of the transverse stepping motor and the dovetail slide rail groove (10) form a sliding device through a lead screw, so that the dovetail slide rail groove (10) is converted into transverse displacement of the dovetail slide rail groove (10) on the dovetail slide rail (9) through the axial displacement of the transverse stepping motor (4) and is used for transversely adjusting the mounting position when the transverse assembly angle of the interception piece is not appropriate;
support servo device include multi-angle bracket (6) and support frame (7), support frame (7) set up on forked tail slide rail groove (10), multi-angle bracket (6) are connected on support frame (7), when interception piece slope installation and debugging in-process, provide the bracket device that a multi-angle closely supported.
2. The aircraft landing system interceptor multifunctional assembly and adjustment device of claim 1, further comprising an electrically controlled elevation and displacement operating panel (16) and an electrically controlled system (19), wherein the electrically controlled elevation and displacement operating panel (16) is connected to the electrically controlled system (19), and the electrically controlled system (19) is connected to the elevating device, the lateral adjustment device and the universal towing device, and is configured to adjust the elevation and movement of the elevating device and the lateral adjustment device, and the movement of the aircraft landing system interceptor multifunctional assembly and adjustment device.
3. An aircraft landing system interceptor multifunctional assembly device according to claim 1 or 2, further comprising an anti-slip bracket (5) attached to the side wall of the rail bracket (11) of the rear lifting hinge mechanism for preventing the interceptor from slipping down when installed at an oblique angle.
4. The aircraft landing system interceptor multifunctional servicing equipment of claim 1 or 2, wherein the aircraft landing system interceptor multifunctional servicing equipment is further provided with a nitrogen cylinder (20), and the nitrogen cylinder (20) is arranged between the two lifting devices and is used for providing compressed nitrogen required for debugging the interceptor.
5. The aircraft landing system interceptor multifunctional servicing equipment of claim 3, wherein the aircraft landing system interceptor multifunctional servicing equipment is further provided with a nitrogen cylinder (20), and the nitrogen cylinder (20) is arranged between the two lifting devices and is used for providing compressed nitrogen required for commissioning for the interceptor.
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| CN201921268174.0U CN210391591U (en) | 2019-08-07 | 2019-08-07 | Multifunctional assembling and adjusting equipment for aircraft landing system interception piece |
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| CN201921268174.0U CN210391591U (en) | 2019-08-07 | 2019-08-07 | Multifunctional assembling and adjusting equipment for aircraft landing system interception piece |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
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2019
- 2019-08-07 CN CN201921268174.0U patent/CN210391591U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
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