CN217805333U - Assembly fixture of skid-type undercarriage of unmanned helicopter - Google Patents
Assembly fixture of skid-type undercarriage of unmanned helicopter Download PDFInfo
- Publication number
- CN217805333U CN217805333U CN202221142391.7U CN202221142391U CN217805333U CN 217805333 U CN217805333 U CN 217805333U CN 202221142391 U CN202221142391 U CN 202221142391U CN 217805333 U CN217805333 U CN 217805333U
- Authority
- CN
- China
- Prior art keywords
- skid
- undercarriage
- assembly
- unmanned helicopter
- fixing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Connection Of Plates (AREA)
Abstract
The utility model provides an assembly fixture of unmanned helicopter skid formula undercarriage, including the fixed subassembly that is used for the brace table of centre gripping skid formula undercarriage bow beam and is used for fixed skid, fixed subassembly sets up in the mounted position that skid and bow beam are corresponding. The utility model provides an assembly fixture of unmanned helicopter skid formula undercarriage, frock simple structure conveniently operates, and single can accomplish the undercarriage assembly, has effectively practiced thrift the manpower; the part location is accurate, and the clamping is reasonable can be high, effectively reduces the disqualification rate of undercarriage, has guaranteed the quality of product.
Description
Technical Field
The utility model relates to a helicopter assembly process field especially relates to an assembly fixture of unmanned helicopter skid formula undercarriage.
Background
With the development of the unmanned helicopter technology in China, the unmanned helicopter is widely applied to various industries at present. The skid landing gear is an important component for supporting the fuselage of the unmanned helicopter, is formed by a skid and an arched beam, bears the weight of the whole helicopter and provides supporting and buffering functions for the landing of the helicopter, so that the skid landing gear is required to have higher strength and impact resistance. Because the bow-shaped roof beam is the abnormal shape structure, consequently it is comparatively difficult and with higher costs to preprocess the installation locating hole, leads to having the problem of installation location. Currently, the undercarriage is assembled mainly by a method of fixing a skid and an arched beam through a C-shaped clamp in the industry. Although the method is low in cost, the assembly precision is poor, the flatness of the assembled undercarriage is poor, and the undercarriage needs to be reworked and adjusted for many times, so that the manpower and the time are wasted.
Therefore, in order to solve the defects of the existing assembly process method, the assembly tool of the skid type undercarriage is needed, and the assembly tool can meet the requirements of being capable of assembling and positioning the skid and the arched beam, being capable of meeting the requirements of accurately preprocessing an installation positioning hole, being simple and convenient for workers to install and operate and the like.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims at providing an assembly fixture of unmanned helicopter skid formula undercarriage solves each part of skid formula undercarriage location difficulty in the assembling process, and the size and the position requirement of bow-shaped roof beam and skid when guaranteeing the assembly are poor to the problem of assembly precision.
The utility model aims at providing an assembly fixture of unmanned helicopter sled formula undercarriage, including the fixed subassembly that is used for the brace table of centre gripping sled formula undercarriage bow beam and is used for fixed skid, fixed subassembly sets up in the mounted position that skid and bow beam are corresponding.
Furthermore, two ends of the top of the arched beam are correspondingly provided with a supporting seat for fixing the arched beam.
Further, the supporting seat is arranged on the supporting platform base through two upright supporting columns.
Furthermore, the supporting seat is correspondingly provided with clamping covers for clamping the bent pipe of the arched beam, and the clamping covers are symmetrically distributed at two ends of the top of the arched beam.
Furthermore, a sleeve piece which is matched and positioned with two ends of the top of the arched beam is arranged between the supporting seat and the clamping cover.
Further, fixed subassembly includes that skid base, skid fixing base, skid dog and skid embrace tightly the piece, skid fixing base, skid dog and skid are embraced tightly the piece and are installed on skid base, the skid dog is installed and is used for blocking the skid in skid length direction's afterbody, the skid is embraced tightly the piece and is installed and be used for blocking the skid in skid length direction both sides.
Furthermore, equal fixed mounting of brace table and mounting is on the base platform, the base platform has a plurality of T type grooves that are used for fixing at transverse distribution.
The utility model has the advantages that: the utility model provides an assembly fixture of unmanned helicopter skid formula undercarriage, frock simple structure conveniently operates, and single can accomplish the undercarriage assembly, has effectively practiced thrift the manpower; the part location is accurate, and the clamping is reasonable can be high, effectively reduces the disqualification rate of undercarriage, has guaranteed the quality of product.
Drawings
The invention will be further described with reference to the following figures and examples:
FIG. 1 is an isometric view of the tool of the present invention;
FIG. 2 is a perspective view of a support platform of the present invention;
fig. 3 is a top view of the tool of the present invention.
Detailed Description
As shown in the figure, the utility model provides an assembly fixture of unmanned helicopter sled formula undercarriage, including the supporting bench 4 that is used for centre gripping sled formula undercarriage bow beam 1 and the fixed subassembly 5 that is used for fixed skid 2, fixed subassembly sets up in skid 2 and the corresponding assembly position of bow beam 1. Wherein skid 2 and bow-shaped roof beam 1 are through connecting piece 3 fixing bolt assembly that punches on the frock, and connecting piece 3 pre-installation is on skid 2. Therefore, the skid type undercarriage is assembled in batches by fixing the undercarriage arched beam on the support table, fixing the skid on the fixing assembly, adjusting the position of the skid to the assembling position corresponding to the two ends of the arched beam and fixing the fixing assembly.
In this embodiment, two ends of the top of the arched beam 1 are correspondingly provided with a support seat 401 for fixing the arched beam. As shown in the figure, the supporting seat is of an I-shaped structure, two ends of a transverse main rod are respectively provided with a longitudinal branch rod, and the arched beam character-shaped positions are arranged on the branch rods at the two ends. The support table 4 is located at the top of the arched beam and provided with a symbol-shaped support seat 401, and the arched beam can be supported through the support seat, so that subsequent assembly work is facilitated.
In this embodiment, the supporting base 401 is disposed on the supporting base 405 through two upright supporting pillars 404. As shown in the figure, the supporting seat is fixed on the supporting base through the upright supporting column, so that a supporting platform is formed integrally, the supporting column can be supported by a whole square column, and the supporting seat can also be supported at a stress point by two square columns in the figure. The form adopted in the embodiment can reduce the material utilization and simultaneously lighten the weight of the device.
In this embodiment, the supporting seat 401 is correspondingly provided with clamping covers 402 for clamping the bent pipe of the arched beam, and the clamping covers are symmetrically distributed at two ends of the top of the arched beam 1. The clamping cover used for clamping the arched beam is installed at the position of the arched beam on the supporting seat, the clamping cover can be clamped in a whole symbol mode or a block end symbol clamping mode, and the arched beam is fixed and clamped in a mode that the symbol clamping blocks are respectively arranged at two ends of the top of the arched beam. Meanwhile, the clamping block can be fixed on the supporting seat in a bolt or hinged mode, so that the clamping block is convenient for workers to disassemble and assemble.
In this embodiment, a sleeve 403 that is positioned at two ends of the top of the arched beam in a matching manner is further disposed between the support base 401 and the clamping cover 402. The sleeve 403 is mainly a bush at two ends of the top of the arched beam in the embodiment, and is used for quickly clamping the arched beam in a locator type manner when the arched beam is placed on the supporting seat, so that the operation of workers and the positioning of workpieces are facilitated.
In this embodiment, fixed subassembly includes that skid base 501, skid fixing base 502, skid dog 504 and skid embrace tightly piece 503, skid fixing base, skid dog and skid embrace tightly the piece and all install on the skid base, the skid dog is installed and is used for blocking the skid in skid length direction's afterbody, the skid embraces tightly the piece and installs and be used for blocking the skid in skid length direction both sides. Fixed subassembly mainly used skid is spacing and fixed to increase the assembly precision, reduce the volume of doing over again. As shown in the figure, it is spacing to the skid afterbody mainly to embrace tight piece through skid dog and skid, and rethread skid fixing base is fixed the skid to make the skid stable on the base not rock.
In this embodiment, brace table 4 and fixed subassembly 5 are all fixed mounting on base platform 6, base platform 6 has a plurality of T type grooves that are used for fixing at transverse distribution. As shown in the figure, a supporting table and a fixing assembly in the device are fixed on a cast iron platform, the tool positioning device is connected with the cast iron platform through a combination bolt to fix and limit the device, and the supporting table and the fixing assembly can move transversely through a T-shaped groove in the cast iron platform to adjust the position of the supporting table and the fixing assembly to reach the optimal position required by assembly.
Finally, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the present invention can be modified or replaced by other means without departing from the spirit and scope of the present invention, which should be construed as limited only by the appended claims.
Claims (6)
1. The utility model provides an assembly fixture of unmanned helicopter skid-type undercarriage which characterized in that: the device comprises a supporting table for clamping a skid type undercarriage arch beam and a fixing assembly for fixing a skid, wherein the fixing assembly is arranged at an assembly position of the skid corresponding to the arch beam; fixed subassembly includes that skid base, skid fixing base, skid dog and skid embrace tightly the piece and install on skid base, the skid dog is installed in skid length direction's afterbody and is used for blocking the skid, the skid is embraced tightly the piece and is installed in skid length direction both sides and is used for blocking the skid.
2. The assembly fixture of the skid type undercarriage of the unmanned helicopter according to claim 1, wherein: and two ends of the top of the arched beam are correspondingly provided with a supporting seat for fixing the arched beam.
3. The assembly fixture of the skid type undercarriage of the unmanned helicopter according to claim 2, wherein: the supporting seat is arranged on the supporting platform base through two upright supporting columns.
4. The assembly fixture of the skid type undercarriage of the unmanned helicopter according to claim 2, wherein: the supporting seat is correspondingly provided with clamping covers for clamping the bent pipe of the arched beam, and the clamping covers are symmetrically distributed at two ends of the top of the arched beam.
5. The assembly fixture of unmanned helicopter skid undercarriage of claim 3 characterized in that: and a sleeve piece which is matched and positioned with the two ends of the top of the arched beam is also arranged between the supporting seat and the clamping cover.
6. The assembly fixture of the skid type undercarriage of the unmanned helicopter according to claim 1, wherein: the supporting table and the fixing assembly are fixedly mounted on the base platform, and a plurality of T-shaped grooves for fixing are transversely distributed on the base platform.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221142391.7U CN217805333U (en) | 2022-05-12 | 2022-05-12 | Assembly fixture of skid-type undercarriage of unmanned helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221142391.7U CN217805333U (en) | 2022-05-12 | 2022-05-12 | Assembly fixture of skid-type undercarriage of unmanned helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN217805333U true CN217805333U (en) | 2022-11-15 |
Family
ID=83984183
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202221142391.7U Active CN217805333U (en) | 2022-05-12 | 2022-05-12 | Assembly fixture of skid-type undercarriage of unmanned helicopter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN217805333U (en) |
-
2022
- 2022-05-12 CN CN202221142391.7U patent/CN217805333U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN108188649B (en) | Clamping device for thin-wall variable-section pipe | |
CN110000530B (en) | Automatic assembly device and automatic assembly method for railway cantilever assembly | |
CN101733608B (en) | Universal fixture and method for welding H-shaped steel stand columns | |
CN112570987B (en) | Flexible posture-adjusting and involuting tool and assembling method thereof | |
CN216781624U (en) | Assembly fixture for wall plate at rear upper part of rear fuselage of airplane | |
CN217805333U (en) | Assembly fixture of skid-type undercarriage of unmanned helicopter | |
CN209754391U (en) | Quartz boat welding position tool | |
CN211568337U (en) | Light helicopter skid undercarriage assembly positioning fixture | |
CN206047467U (en) | Group weldering integral type box soldering cramping apparatus | |
CN210649259U (en) | Frame point-fixing welding fixture with adjustable length and width | |
CN211362175U (en) | Universal experimental frame for skylight of trolley | |
CN212706625U (en) | Universal aircraft fuselage supports frock | |
CN212217602U (en) | Multifunctional welding positioning tool for scissor arm of lifter | |
CN104191216A (en) | Equipment assembling system and method | |
CN109945755B (en) | Measuring tool is used in installation of fin lift guide rail | |
CN211491313U (en) | Flexible engine valve collet mounting tool | |
CN211495668U (en) | Workpiece positioning stepping conveying mechanism | |
CN209867656U (en) | Resistance band spot welding auxiliary device | |
CN108857974B (en) | Positioning jig for front face support of automobile | |
CN107671473B (en) | It is a kind of to build the column maintained equipment and be oriented to wheel group to tooling | |
CN202388161U (en) | Flip-over type cab front-low edge welding fixture | |
CN110497372A (en) | A kind of scribing tooling of manifold Al-alloy casing | |
CN111038733A (en) | Unmanned helicopter frame assembly fixture | |
CN219192565U (en) | Aircraft component assembly type frame | |
CN219189944U (en) | Frock structure of holding ring |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |