CN213705814U - Airborne photoelectric pod installation device - Google Patents
Airborne photoelectric pod installation device Download PDFInfo
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- CN213705814U CN213705814U CN202022420488.7U CN202022420488U CN213705814U CN 213705814 U CN213705814 U CN 213705814U CN 202022420488 U CN202022420488 U CN 202022420488U CN 213705814 U CN213705814 U CN 213705814U
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- shock absorber
- nacelle
- adapter
- mounting screw
- mounting
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Abstract
The utility model discloses an airborne photoelectricity nacelle installation device is applicable to the quick installation of almost all capstan head type photoelectricity nacelles, including being used for installing to the aircraft mounting base on external switching support and through nacelle switching support mounting screw with external switching leg joint's nacelle switching support, nacelle switching support has a plurality of bumper shock absorber adapter through lock nut and bumper shock absorber adapter mounting screw installation, all installs three-dimensional equal rigidity bumper shock absorbers through bumper shock absorber mounting screw on every bumper shock absorber adapter, three-dimensional equal rigidity bumper shock absorber on be provided with nacelle mounting screw, external switching support on install external switching support mounting screw. The utility model has the characteristics of simple structure, low cost, high strength, installation labour saving and time saving can satisfy different external interface platforms etc. and show, can be used to the installation of various unmanned aerial vehicle, unmanned aerial vehicle photoelectric load.
Description
Technical Field
The utility model belongs to the ray apparatus field, concretely relates to quick installation device of external photoelectricity nacelle of aircraft.
Background
The installation of traditional photoelectricity nacelle designs according to the aircraft platform of difference, especially to the photoelectricity nacelle that weight exceedes 30kg, if installation device design is unreasonable, installs comparatively labouriously, very big waste manpower and time.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to solve the above-mentioned problem that prior art exists, provide a quick machine carries photoelectricity nacelle installation device, adaptable most aircraft platform, it is quick laborsaving to install.
The utility model provides a technical scheme that technical problem adopted is: the airborne photoelectric pod mounting device comprises an external transfer support and a pod transfer support, wherein the pod transfer support is used for being mounted on an airplane mounting base, the pod transfer support is connected with the external transfer support through pod transfer support mounting screws, the pod transfer support is provided with a plurality of shock absorber transfer seats through locknuts and shock absorber transfer seat mounting screws, a three-dimensional equal-rigidity shock absorber is mounted on each shock absorber transfer seat through shock absorber mounting screws, pod mounting screws are arranged on the three-dimensional equal-rigidity shock absorbers, and external transfer support mounting screws are mounted on the external transfer support.
According to the airborne photoelectric pod installation device, a notch is formed in the center of a pod transfer support, and the outward transfer support is located in the notch.
The number of the shock absorber adapter bases of the airborne photoelectric pod mounting device is four.
Furthermore, the pod mounting screw is in a national standard GB32.2 specification. The shock absorber adapter mounting screws, the pod adapter bracket mounting screws and the external adapter bracket mounting screws are in the national standard GB5783 specification.
The utility model discloses can labour saving and time saving, realize the quick installation of photoelectricity nacelle, external switching support can satisfy different mounting platform's requirement through suitably changing the appearance and to the external interface for various have man-machine, unmanned aerial vehicle photoelectric load's installation.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is an installation schematic diagram of the shock absorber adapter and the three-dimensional iso-stiffness shock absorber of the present invention;
fig. 3 is a schematic view of the present invention after installation of the photovoltaic pod.
The figures are numbered: 1-locknut, 2-nacelle mounting screw, 3-nacelle adapter bracket, 4-shock absorber adapter mounting screw, 5-nacelle adapter bracket mounting screw, 6-external adapter bracket, 7-external adapter bracket mounting screw, 8-shock absorber adapter, 9-shock absorber mounting screw, and 10-three-dimensional equal-rigidity shock absorber.
Detailed Description
The present invention will be further explained with reference to the drawings and examples.
As shown in fig. 1, 2 and 3, the utility model discloses an airborne optoelectronic pod installation device, including locknut 1, optoelectronic pod mounting screw 2, optoelectronic pod switching support 3, bumper shock absorber adapter mounting screw 4, optoelectronic pod switching support mounting screw 5, to external switching support 6, to external switching support mounting screw 7, bumper shock absorber adapter 8, bumper shock absorber mounting screw 9 and rigidity bumper shock absorber 10 such as three-dimensional.
Firstly, an external transfer bracket 6 is installed on a corresponding airplane installation base, is fixed by an external transfer bracket installation screw 7 (generally selected by specification GB 5783), and is provided with a locknut 1; sequentially mounting four three-dimensional equal-stiffness shock absorbers 10 on a shock absorber adapter 8, and fixing the four three-dimensional equal-stiffness shock absorbers by using shock absorber mounting screws 9 (generally selecting the specification GB 70.1); sequentially mounting a shock absorber adapter 8 provided with a three-dimensional equal-rigidity shock absorber 10 on a photoelectric turret and fixing the shock absorber adapter by using a photoelectric pod mounting screw 2 (generally selecting the specification GB 32.2), wherein the pod mounting screw 2 is characterized in that the head part of the pod mounting screw is provided with a small hole, so that the anti-loosening requirement of the photoelectric pod on an airplane vibration platform can be met by threading a steel wire for locking, and after the screw is fastened, threading a steel wire with the diameter of 1.5mm on the head part of the screw for locking, so that the photoelectric pod is prevented from loosening caused by being in a vibration environment for; the pod adapter bracket 3 is arranged on a shock absorber adapter 8 and is fixed by a locknut 1 and a shock absorber adapter mounting screw 4 (generally selected by specification GB 5783); after the completion, the photoelectric turret is integrally supported, bypasses a gap between the external transfer support 6 and the pod transfer support 3 from bottom to top and falls on the external transfer support 6; the outer adapting bracket 6 is provided with a spigot, and when the photoelectric pod adapting bracket 3 meets the spigot, the alignment of the mounting hole positions of the outer adapting bracket 6 and the photoelectric pod adapting bracket 3 is quickly realized;
by rotating the photoelectric pod, when the bayonet of the external transfer support 6 collides with the pod transfer support 3 to cause the rotation incapability, the pod transfer support is fixed by penetrating the pod transfer support mounting screws 5 (generally selecting the specification GB 5783), and finally, the four pod mounting screws 2 are penetrated into phi 1.5 steel wires to prevent looseness, so that the mounting is finished.
The utility model discloses a mainly used adaptation photoelectricity nacelle makes the adaptability improvement according to photoelectricity nacelle installation interface, and nacelle switching support 3 center is seted up jaggedly, and external switching support 6 is located the breach, and place on external switching support 6 after the photoelectricity nacelle passes through the breach during installation, rotates the photoelectricity nacelle again and finds the mounting hole to external switching support 6 and photoelectricity nacelle switching support 3, can use manpower sparingly.
The external transfer support 6 of the utility model is mainly used for adapting to the mounting platform, the adaptability improvement is made according to different mounting platforms, most of the external transfer support can be adapted only by changing the external mounting interface, the spigot is arranged on the external transfer support 6, and the rapid alignment of the mounting hole sites of the external transfer support 6 and the photoelectric pod transfer support 3 can be realized; the installation can be realized by changing an external adapter bracket according to different external interface platforms. The vibration damping device can be realized by selecting different three-dimensional equal-rigidity shock absorbers 10 and changing the installation interface according to the vibration characteristics of the external platform and the performance of the photoelectric pod. After the photoelectric pod is fastened with the three-dimensional equal-rigidity shock absorber 10 through connecting screws, the anti-loosening of an airborne vibration environment can be realized through steel wire penetration, and the flight safety is ensured.
The above embodiments are merely illustrative of the principles and effects of the present invention, and some embodiments may be applied, and it will be apparent to those skilled in the art that a plurality of modifications and improvements may be made without departing from the inventive concept of the present invention, and all of these modifications and improvements fall within the protection scope of the present invention.
Claims (6)
1. An airborne optoelectronic pod mounting apparatus, comprising: the nacelle adapter bracket comprises an external adapter bracket (6) and a nacelle adapter bracket (3) connected with the external adapter bracket (6) through nacelle adapter bracket mounting screws (5), wherein the nacelle adapter bracket (3) is provided with a plurality of shock absorber adapter seats (8) through locknuts (1) and shock absorber adapter seat mounting screws (4), each shock absorber adapter seat (8) is provided with a three-dimensional equal-rigidity shock absorber (10) through a shock absorber mounting screw (9), the three-dimensional equal-rigidity shock absorber (10) is provided with a nacelle mounting screw (2), and the external adapter bracket (6) is provided with an external adapter bracket mounting screw (7).
2. The airborne optoelectronic pod mounting apparatus of claim 1 wherein the pod adaptor bracket (3) is centrally notched and the outward adaptor bracket (6) is located within the notch.
3. An airborne optoelectronic pod mounting apparatus as claimed in claim 1 or claim 2 wherein there are four shock absorber adapters (8).
4. An airborne optoelectronic pod mounting apparatus as claimed in claim 3 wherein the pod mounting screw (2) is of the national standard GB32.2 specification.
5. An airborne optoelectronic pod mounting apparatus as claimed in claim 3 wherein the shock absorber adapter mounting screws (4), pod adapter bracket mounting screws (5) and external adapter bracket mounting screws (7) are of the national standard GB5783 specification.
6. An airborne optoelectronic pod mounting apparatus as claimed in claim 3 wherein the shock absorber mounting screw (9) is of the national standard GB 70.1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022420488.7U CN213705814U (en) | 2020-10-27 | 2020-10-27 | Airborne photoelectric pod installation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022420488.7U CN213705814U (en) | 2020-10-27 | 2020-10-27 | Airborne photoelectric pod installation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213705814U true CN213705814U (en) | 2021-07-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022420488.7U Active CN213705814U (en) | 2020-10-27 | 2020-10-27 | Airborne photoelectric pod installation device |
Country Status (1)
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| CN (1) | CN213705814U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117446199A (en) * | 2023-12-11 | 2024-01-26 | 中国科学院长春光学精密机械与物理研究所 | Quick loading and unloading device for airborne photoelectric nacelle |
-
2020
- 2020-10-27 CN CN202022420488.7U patent/CN213705814U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117446199A (en) * | 2023-12-11 | 2024-01-26 | 中国科学院长春光学精密机械与物理研究所 | Quick loading and unloading device for airborne photoelectric nacelle |
| CN117446199B (en) * | 2023-12-11 | 2024-05-17 | 中国科学院长春光学精密机械与物理研究所 | Quick loading and unloading device for airborne photoelectric nacelle |
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