CN210286348U - Cable installation auxiliary assembly for general aircraft - Google Patents
Cable installation auxiliary assembly for general aircraft Download PDFInfo
- Publication number
- CN210286348U CN210286348U CN201920922007.7U CN201920922007U CN210286348U CN 210286348 U CN210286348 U CN 210286348U CN 201920922007 U CN201920922007 U CN 201920922007U CN 210286348 U CN210286348 U CN 210286348U
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- mounting
- mounting panel
- transmission case
- rotation
- cable installation
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Abstract
The utility model discloses a cable erection auxiliary assembly for general aircraft, including the mounting panel, there is a removal bottom plate front end bottom both sides difference fixed mounting of mounting panel, the front end surface central point of mounting panel puts movable mounting and has an installation rotation post, the rear end fixed surface of mounting panel installs a transmission case. A general cable erection auxiliary assembly for aircraft, constitute the frame through mounting panel and removal bottom plate, and four universal wheels of taking the brake block are installed to bottom at the frame, make things convenient for the removal and the fixing of frame, rotate the post in the front end installation of mounting panel simultaneously, transmission case is installed at the rear end of mounting panel, and carousel is installed to the rear end at the transmission case, link up carousel and rotation post through the gear in transmission incasement portion, the realization can control the rotation post through the carousel and rotate, the realization is rolled up the cable of covering on the rotation post and is carried out the rolling.
Description
Technical Field
The utility model relates to a cable installation field, in particular to cable installation auxiliary assembly for general aircraft.
Background
The cable is used for transmitting electric energy, information and realizing the wire rod product of electromagnetic energy conversion, usually by several or several groups of wire composition, itself has good corrosion-resistant, stand wear and tear and insulating properties, undertake important role in the power industry, and various control system need realize its function through laying the cable on the aircraft, however, the cable that uses on the aircraft mostly is thin small-size, when installation is laid, the cable is rolled up oneself and is heavier, the manpower can't be lifted and laid, and the restriction of equipment hand aircraft organism environment such as large-scale fork truck can't normally operate, to this kind of condition, need design an auxiliary assembly for aircraft cable installation.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides a cable installation auxiliary assembly for general aircraft can effectively solve the problem among the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a cable installation auxiliary assembly for general aircraft, includes the mounting panel, the front end bottom both sides of mounting panel fixed mounting respectively have a removal bottom plate, the front end surface central point of mounting panel puts movable mounting and has an installation rotation post, the rear end fixed surface of mounting panel installs a transmission case, the rear end surface of transmission case movable mounting has a carousel in addition.
Preferably, the movable bottom plate is vertically welded at the bottom of the front end of the mounting plate in a welding mode, two universal wheels are respectively mounted at the bottoms of the mounting plate and the movable bottom plate, and brake pads are arranged on the universal wheels.
Preferably, the transmission case passes through mode fixed mounting of screw connection on the rear end face of mounting panel, the carousel be the disc structure of a fretwork, the perpendicular movable mounting in edge of carousel has a turning handle to its centre of a circle position department fixed mounting has a transmission shaft, the transmission shaft inwards stretches into the inside of transmission case to with the coaxial fixed connection of a rotation axis of transmission incasement portion, fixed mounting has a driving gear in the axis of rotation.
Preferably, a second rotating shaft is fixedly installed on one side of the first rotating shaft in the transmission case, a driven gear is fixedly installed on the second rotating shaft, the driven gear is meshed with the driving gear, the number of teeth of the driving gear is 34, and the number of teeth of the driven gear is 17.
Preferably, the front end of No. two axis of rotation passes the transmission case and at a connecting rod of terminal coaxial fixed connection, anti-tooth external screw thread has been seted up on the terminal surface of connecting rod, the installation is rotated the post afterbody and is seted up a mounting groove correspondingly, it is equipped with anti-tooth internal thread to correspond carving on the inner wall of mounting groove.
Preferably, the surface of the mounting rotating column is wrapped with a layer of anti-abrasion soft rubber mat.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses in, constitute a portable frame through mounting panel and removal bottom plate, rotate the post through movable mounting one on the mounting panel of frame and entangle the cable book with the cover, simultaneously at transmission case of rear end installation of mounting panel, utilize the gear engagement of incasement to carry out the transmission, the carousel that realizes utilizing the transmission case rear end drives and rotates the post and rotates, and manual limit removes the limit and rolls when making things convenient for the manual work to lay the cable, uses manpower sparingly, improves the efficiency that the cable was laid on the aircraft.
Drawings
Fig. 1 is a schematic overall structure diagram of a cable installation auxiliary device for a general aircraft according to the present invention;
fig. 2 is a side view of a cable installation aid for a general-purpose aircraft according to the present invention;
fig. 3 is a rear view of the cable installation aid for a general-purpose aircraft according to the present invention;
fig. 4 is a schematic view of the internal structure of the transmission case of the cable installation auxiliary device for a general aircraft according to the present invention;
fig. 5 is the utility model relates to a column connection installation schematic diagram is rotated in installation of cable installation auxiliary assembly for general aircraft.
In the figure: 1. mounting a plate; 2. moving the base plate; 3. a universal wheel; 4. mounting a rotating column; 5. a transmission case; 6. a turntable; 7. a drive shaft; 8. rotating the handle; 9. a first rotating shaft; 10. a driving gear; 11. a driven gear; 12. a second rotating shaft; 13. mounting grooves; 14. a reverse internal thread; 15. a connecting rod; 16. and (4) reverse thread external threads.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-5, a cable installation auxiliary device for a general airplane includes a mounting plate 1, a movable bottom plate 2 is respectively and fixedly mounted on two sides of the bottom of the front end of the mounting plate 1, an installation rotating column 4 is movably mounted on the center of the surface of the front end of the mounting plate 1, a transmission case 5 is fixedly mounted on the surface of the rear end of the mounting plate 1, and a rotary table 6 is movably mounted on the surface of the rear end of the transmission case 5.
The movable bottom plate 2 is vertically welded at the bottom of the front end of the mounting plate 1 in a welding mode, two universal wheels 3 are respectively mounted at the bottoms of the mounting plate 1 and the movable bottom plate 2, and the universal wheels 3 are respectively provided with a brake pad; the transmission case 5 is fixedly arranged on the rear end face of the mounting plate 1 in a screw connection mode, the rotary table 6 is of a hollow disc structure, a rotating handle 8 is vertically and movably arranged at the edge of the rotary table 6, a transmission shaft 7 is fixedly arranged at the position of the circle center of the rotary table, the transmission shaft 7 extends inwards into the transmission case 5 and is coaxially and fixedly connected with a first rotating shaft 9 in the transmission case 5, and a driving gear 10 is fixedly arranged on the first rotating shaft 9; a second rotating shaft 12 is fixedly arranged on one side of the first rotating shaft 9 in the transmission case 5, a driven gear 11 is fixedly arranged on the second rotating shaft 12, the driven gear 11 is meshed with the driving gear 10, the number of teeth of the driving gear 10 is 34, and the number of teeth of the driven gear 11 is 17; the front end of the second rotating shaft 12 penetrates through the transmission case 5 and is coaxially and fixedly connected with a connecting rod 15 at the tail end, the surface of the tail end of the connecting rod 15 is provided with a reverse thread external thread 16, the tail part of the installation rotating column 4 is correspondingly provided with an installation groove 13, and a reverse thread internal thread 14 is correspondingly carved on the inner wall of the installation groove 13; the surface of the mounting rotating column 4 is wrapped with a layer of anti-abrasion soft rubber cushion.
It should be noted that the utility model relates to a cable installation auxiliary device for general aircraft, through designing a mounting plate 1, two moving bottom plates 2 are vertically installed on two sides of the front end bottom of the mounting plate 1, and four universal wheels 3 with brake pads are installed on the bottom of the mounting plate 1 and the two moving bottom plates 2, to realize the moving and fixing of the whole auxiliary device, through installing a mounting rotating column 4 at the front end center of the mounting plate 1, the surface of the mounting rotating column 4 is wrapped with a layer of abrasion-proof soft rubber pad, to prevent the cable roll sleeve from generating unnecessary abrasion when rotating on the mounting plate, at the same time, a transmission case 5 is installed on the rear end face of the mounting plate 1, a pair of mutually meshed driving gear 10 and driven gear 11 are arranged in the transmission case 5, a connecting rod 15 is connected to the end of a second rotating shaft 12 on the driven gear 11, and the connecting rod 15 extends out of the mounting plate 1 to be fixedly connected with the mounting rotating column 4 through a reverse thread connection mode, and a rotation axis 9 on the driving gear 10 then stretches out the transmission case 5 and is connected with transmission shaft 7 of 6 centre of a circle departments of carousel to when realizing through the rotation of rotating handle 8 control carousel 6, through the transmission of driving gear 10 with driven gear 11, finally drive the rotation of installation rotation post 4, realize the semi-automatic rolling to the cable, conveniently lay the operation, the drive ratio of driving gear 10 and driven gear 11 is 2 simultaneously, make installation rotation post 4 can slowly rotate, make things convenient for personnel to control.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides a cable installation auxiliary assembly for general aircraft which characterized in that: including mounting panel (1), there is a removal bottom plate (2) front end bottom both sides difference fixed mounting of mounting panel (1), the front end surface central point of mounting panel (1) puts movable mounting and has an installation rotation post (4), the rear end fixed surface of mounting panel (1) installs a transmission case (5), the rear end surface of transmission case (5) movable mounting has a carousel (6) in addition.
2. The universal aircraft cable installation aid of claim 1, wherein: remove bottom plate (2) and pass through the welding mode vertical welding in the front end bottom of mounting panel (1), two universal wheels (3) are installed respectively to mounting panel (1) and the bottom of removing bottom plate (2), all have the brake block on universal wheel (3).
3. The universal aircraft cable installation aid of claim 1, wherein: transmission case (5) are on the rear end face of mounting panel (1) through mode fixed mounting of screw connection, carousel (6) be the disc structure of a fretwork, the perpendicular movable mounting in edge of carousel (6) has a turning handle (8) to its centre of a circle position department fixed mounting has a transmission shaft (7), transmission shaft (7) inwards stretch into the inside of transmission case (5) to with a rotation axis (9) coaxial fixed connection of transmission case (5) inside, fixed mounting has a driving gear (10) on rotation axis (9).
4. The universal aircraft cable installation aid of claim 3, wherein: the inside of transmission case (5) is located one side of axis of rotation (9) and another fixed mounting has a No. two axis of rotation (12), No. two axis of rotation (12) another fixed mounting has a driven gear (11) to driven gear (11) and driving gear (10) intermeshing, the number of teeth of driving gear (10) is 34, and the number of teeth of driven gear (11) is 17.
5. The universal aircraft cable installation aid of claim 4, wherein: the front end of No. two axis of rotation (12) passes transmission case (5) and at a terminal coaxial fixed connection connecting rod (15), anti-tooth external screw thread (16) have been seted up on the terminal surface of connecting rod (15), installation rotation post (4) afterbody correspondence has been seted up one mounting groove (13), corresponding carving on the inner wall of mounting groove (13) is equipped with anti-tooth internal thread (14).
6. The universal aircraft cable installation aid of claim 1, wherein: the surface of the mounting rotating column (4) is wrapped with a layer of anti-abrasion soft rubber cushion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920922007.7U CN210286348U (en) | 2019-06-19 | 2019-06-19 | Cable installation auxiliary assembly for general aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920922007.7U CN210286348U (en) | 2019-06-19 | 2019-06-19 | Cable installation auxiliary assembly for general aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210286348U true CN210286348U (en) | 2020-04-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920922007.7U Active CN210286348U (en) | 2019-06-19 | 2019-06-19 | Cable installation auxiliary assembly for general aircraft |
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| CN (1) | CN210286348U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111994741A (en) * | 2020-09-04 | 2020-11-27 | 王芳 | Optical fiber line winding and unwinding devices for communication engineering |
-
2019
- 2019-06-19 CN CN201920922007.7U patent/CN210286348U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111994741A (en) * | 2020-09-04 | 2020-11-27 | 王芳 | Optical fiber line winding and unwinding devices for communication engineering |
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