CN212056646U - Bracket for aerial measuring instrument, aerial measuring device and airplane - Google Patents
Bracket for aerial measuring instrument, aerial measuring device and airplane Download PDFInfo
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- CN212056646U CN212056646U CN202020555306.4U CN202020555306U CN212056646U CN 212056646 U CN212056646 U CN 212056646U CN 202020555306 U CN202020555306 U CN 202020555306U CN 212056646 U CN212056646 U CN 212056646U
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Abstract
The utility model relates to a bracket, aerial survey device and aircraft for the aerial survey appearance, bracket includes support piece, transition piece and hasp subassembly for the aerial survey appearance. The transition piece is mounted on the support piece and used for mounting an aeronautical measuring instrument. The lock catch component is provided with a lock catch piece and a connecting piece, the lock catch piece is used for connecting an undercarriage of the airplane, and the connecting piece is connected with the supporting piece. During aerial survey, lock the lock catch piece in the undercarriage of aircraft to install aerial survey instrument in the transition piece, the bottom of external aircraft when making aerial survey instrument operation, alright carry out the aviation through aerial survey instrument like this and shoot ground. Can arrange the bottom of aircraft in the aviation measuring instrument is external through support piece, transition piece and hasp subassembly's mating reaction, simple structure, the dismouting is simple and easy, is favorable to improving the installation effectiveness. By changing the length of the supporting piece and the size of the transition piece, the bracket for the aerial measuring instrument can be suitable for airplanes and aerial measuring instruments of different types, and is wide in application range.
Description
Technical Field
The utility model relates to an aeronautical survey technical field especially relates to a bracket, aeronautical survey device and aircraft for aeronautical survey appearance.
Background
The aerial photogrammetry is that an aerial measuring device is loaded on an airplane, aerial photography is carried out on the ground by using the aerial measuring device, and the topographic map surveying and mapping operation is completed by combining the steps of ground control point measurement, transferring and drawing, three-dimensional surveying and mapping and the like. The aerial shooting measurement of the airplane has the characteristics of quick response capability, outstanding timeliness, flexibility, safety and the like, and is widely applied to the fields of urban planning, desertification monitoring, accurate agriculture and the like. Traditional aerial survey device loads in the fixed wing aircraft inside and holds in the palm with loaded down with trivial details device and hangs in the helicopter outside, and mounting structure is complicated, and the dismouting is loaded down with trivial details, and the installation effectiveness is low.
SUMMERY OF THE UTILITY MODEL
Therefore, it is necessary to provide a bracket for an aerial surveying instrument, and an aircraft, which have simple structures and easy assembly and disassembly, and are beneficial to improving the installation efficiency.
A cradle for an aerial gauge, comprising:
a support member;
a transition piece for mounting an aeronautical measuring instrument, the transition piece being mounted to the support piece;
the locking assembly is provided with a locking piece and a connecting piece, the locking piece is used for connecting an undercarriage of an airplane, and the connecting piece is connected with the supporting piece.
In one embodiment, the locking part comprises a first arc-shaped plate and a second arc-shaped plate, one end of the first arc-shaped plate is detachably connected with one end of the second arc-shaped plate, and the other end of the first arc-shaped plate is detachably connected with the other end of the second arc-shaped plate.
In one embodiment, the locking member comprises a first arc-shaped plate and a second arc-shaped plate, one end of the first arc-shaped plate is detachably connected with one end of the second arc-shaped plate, and the other end of the first arc-shaped plate is detachably connected with the other end of the second arc-shaped plate.
In one embodiment, the connecting member is a connecting sleeve, and the connecting sleeve is arranged on the locking member.
In one embodiment, the bracket for the aerial measuring instrument further comprises a shock absorbing member, and the shock absorbing member is arranged on the transition member.
In one embodiment, the bracket for the aerial measuring instrument further comprises a mounting member, wherein the top of the mounting member is connected with the shock absorbing member, and the side of the mounting member is used for connecting the aerial measuring instrument.
In one embodiment, the bracket for the aerial surveying instrument further comprises a safety buckle, the safety buckle comprises a first buckle and a second buckle, the first buckle is arranged at one end of the supporting part, the second buckle is arranged at the other end of the supporting part, and the first buckle and the second buckle are respectively arranged at the outer side of the connecting part of the buckle component.
In one embodiment, the transition piece is a transition plate provided with a through hole for adapting to a lens of the aerial surveying instrument.
In one embodiment, the supporting members include a first supporting member and a second supporting member which are arranged at intervals, the number of the locking assemblies is four, two of the locking assemblies are respectively arranged at two ends of the first supporting member, and the other two of the locking assemblies are respectively arranged at two ends of the second supporting member.
The utility model provides an aerial measuring device, aerial measuring device includes aerial measuring instrument and foretell bracket for the aerial measuring instrument, aerial measuring instrument locates the transition piece of bracket for the aerial measuring instrument.
An aircraft comprises an aircraft body and the aerial measurement device, wherein the aerial measurement device is mounted on an undercarriage of the aircraft body.
The bracket for the aerial measuring instrument, the aerial measuring device and the airplane at least have the following advantages:
foretell aerial survey is bracket, aerial measuring device and aircraft for the appearance, the transition piece is installed in support piece, and the connecting piece of hasp subassembly is connected in support piece. When needing to carry out the aerial survey, lock the hasp piece of hasp subassembly in the undercarriage of aircraft to install the aerial survey instrument in the transition piece, make the bottom of external aircraft during the operation of aerial survey instrument, like this alright carry out the aviation through the aerial survey instrument and shoot ground. Can arrange the bottom of aircraft in the aviation measuring instrument is external through support piece, transition piece and hasp subassembly's mating reaction, simple structure, the dismouting is simple and easy, is favorable to improving the installation effectiveness. And, the hasp subassembly is connected support piece and transition piece to the undercarriage for the bracket for the aeronautical measuring apparatu can install in the undercarriage of aircraft steadily. In addition, the length of the supporting piece and the size of the transition piece are changed, so that the bracket for the aerial measuring instrument can be suitable for airplanes and aerial measuring instruments of different types, and the application range is wide.
Drawings
Fig. 1 is a schematic structural view of a bracket for an aerial surveying instrument according to an embodiment of the present invention;
FIG. 2 is a schematic structural view of a latch assembly of the bracket for an aerial measurement instrument shown in FIG. 1;
FIG. 3 is a schematic view of the shock absorber of the bracket for an aerial survey instrument shown in FIG. 1;
FIG. 4 is a schematic view of the shock absorber of the bracket for an aerial survey instrument shown in FIG. 1 mounted to a transition piece;
FIG. 5 is a schematic view of the mounting member of the bracket for an aerial survey instrument shown in FIG. 1;
FIG. 6 is a schematic view of the safety catch of the bracket for an aerial survey instrument shown in FIG. 1;
fig. 7 is a schematic structural diagram of an aerial survey device according to an embodiment of the present invention.
10. The support piece, 11, the first support piece, 12, the second support piece, 20, the transition piece, 21, the through-hole, 30, the latch assembly, 31, the latch piece, 311, the first arc-shaped plate, 3111, the first latch portion, 3112, the second latch portion, 312, the second arc-shaped plate, 3121, the third latch portion, 3122, the fourth latch portion, 32, the connecting piece, 40, the shock absorbing member, 50, the mounting piece, 51, the first mounting plate, 52, the second mounting plate, 53, the first baffle, 54, the second baffle, 60, the safety latch, 61, the first latch, 62, the second latch, 70, the aeronautical measuring instrument.
Detailed Description
In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. The present invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein, as those skilled in the art will be able to make similar modifications without departing from the spirit and scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", 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 simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present application, unless expressly stated or limited otherwise, the first feature may be directly on or directly under the second feature or indirectly via intermediate members. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.
Referring to fig. 1, 2 and 7, an exemplary embodiment of a bracket for an aerial measuring instrument includes a support member 10, a transition member 20 and a locking assembly 30. A transition piece 20 is mounted to the support 10, the transition piece 20 being used to mount an aeronautical measuring instrument 70. The latch assembly 30 is provided with a latch member 31 and a connecting member 32, the latch member 31 is used for connecting the landing gear of the aircraft, and the connecting member 32 is connected with the supporting member 10.
In the above-described bracket for an aircraft measuring instrument, the transition member 20 is mounted to the support member 10, and the connecting member 32 of the locking assembly 30 is connected to the support member 10. When the aerial survey needs to be carried out, the lock catch piece 31 of the lock catch assembly 30 is locked on the landing gear of the airplane, and the aerial survey instrument 70 is installed on the transition piece 20, so that the aerial survey instrument 70 is externally arranged at the bottom of the airplane during operation, and thus the aerial photograph can be carried out on the ground through the aerial survey instrument 70. The aviation measuring instrument 70 can be externally arranged at the bottom of the airplane through the matching action of the supporting piece 10, the transition piece 20 and the locking assembly 30, the structure is simple, the assembly and disassembly are simple, and the improvement of the installation efficiency is facilitated. Also, the latch assembly 30 connects the support 10 and the transition piece 20 to the landing gear, so that the bracket for an aircraft measuring instrument can be smoothly mounted to the landing gear of the aircraft. In addition, the length of the supporting piece 10 and the size of the transition piece 20 are changed, so that the bracket for the aerial measuring instrument can be suitable for different types of airplanes and the aerial measuring instrument 70, and the application range is wide.
Specifically, referring to fig. 1, the supporting member 10 is provided with a threaded hole, the transition piece 20 is correspondingly provided with a threaded hole, and a screw is inserted into the threaded hole of the supporting member 10 and the threaded hole of the transition piece 20 to detachably connect the supporting member 10 and the transition piece 20, so that the assembly and disassembly are easy, the supporting member 10 and the transition piece 20 can be conveniently replaced, and the assembly efficiency can be improved. Of course, in other embodiments, the transition piece 20 may also be welded to the support piece 10, but not limited thereto.
In one embodiment, referring to fig. 1 and 2, the locking member 31 includes a first arc plate 311 and a second arc plate 312, one end of the first arc plate 311 is detachably connected to one end of the second arc plate 312, and the other end of the first arc plate 311 is detachably connected to the other end of the second arc plate 312. During the use, dismantle first arc 311 and second arc 312, locate the outside of undercarriage with first arc 311 and second arc 312 respectively, then connect the both ends of first arc 311 and second arc 312, just so lock catch piece 31 in the whippletree of undercarriage. This hasp piece 31's simple structure, the dismouting is simple and easy, is favorable to improving the installation effectiveness.
Specifically, referring to fig. 2, a first locking portion 3111 is formed at one end of the first arc-shaped plate 311, and a second locking portion 3112 is formed at the other end of the first arc-shaped plate 311; the first locking portion 3111 is provided with a first threaded hole, and the second locking portion 3112 is provided with a second threaded hole. Correspondingly, a third latch portion 3121 is formed at one end of the second arc-shaped plate 312, and a fourth latch portion 3122 is formed at the other end of the second arc-shaped plate 312; the third locking portion 3121 is provided with a third threaded hole, and the fourth locking portion 3122 is provided with a fourth threaded hole. Catch piece 31 further comprises two fasteners. The first threaded hole of the first arc-shaped plate 311 and the third threaded hole of the second arc-shaped plate 312 are correspondingly arranged, and one fastener sequentially penetrates through the first threaded hole and the third threaded hole to detachably connect the first latch portion 3111 and the third latch portion 3121. The second threaded hole of the first arc-shaped plate 311 and the fourth threaded hole of the second arc-shaped plate 312 are correspondingly arranged, and the other fastener sequentially penetrates through the second threaded hole and the fourth threaded hole to detachably connect the second latch portion 3112 and the fourth latch portion 3122. Of course, in other embodiments, the locking member 31 may further include a locking block provided with a locking slot; the locking block is equipped with two, and first hasp portion 3111 and third hasp portion 3121 joint are in the draw-in groove of one of them locking block, and second hasp portion 3112 and fourth hasp portion 3122 joint are in the draw-in groove of another locking block.
Specifically, in the present embodiment, the first arc plate 311 and the second arc plate 312 are made of aircraft aluminum. The aviation aluminum material has good mechanical property and processing property, good plasticity after solution treatment, good heat treatment strengthening effect, high strength below 150 ℃ and good toughness.
Further, the inner surface of the locking part 31 of the locking assembly 30 is provided with a rubber pad, so that the friction force between the locking part 31 and the landing gear can be increased, the locking part 31 is tightly attached to the landing gear, and the bracket for the aviation measuring instrument is favorably and firmly locked to the landing gear. The thickness of the rubber pad may be set according to the thickness of the landing gear, and is not particularly limited herein.
In one embodiment, referring to fig. 1 and 2, the connecting member 32 is a connecting sleeve, and the connecting sleeve is disposed on the locking member 31. Specifically, the connecting sleeve is disposed on the top of the locking member 31, and the axis of the connecting sleeve intersects with the axis of the locking member 31. It should be noted that the size of the connecting sleeve is adapted to the size of the supporting member 10, so as to facilitate the connecting sleeve to be sleeved on the supporting member 10. During installation, the supporting piece 10 can be quickly connected to the undercarriage through the connecting sleeve, so that the bracket for the aerial measuring instrument is easy to disassemble and assemble, and the improvement of the installation efficiency is facilitated. In the present embodiment, the axis of the connecting sleeve is perpendicular to the axis of the locking member 31. In other embodiments, the connecting member 32 may also be a catch member.
In the present embodiment, the supporting member 10 is a long rod, and the connecting member 32 is a sleeve. Of course, in other embodiments, the support member 10 may be a square rod, and the connecting member 32 may be a square sleeve. The shapes of the supporting member 10 and the connecting member 32 are not particularly limited, and the supporting member 10 may be fittingly connected to the connecting member 32.
Further, referring to fig. 1 and 6, the bracket for an aerial measuring instrument further includes a safety catch 60. The safety latch 60 includes a first latch 61 and a second latch 62, the first latch 61 is disposed at one end of the support 10, and the second latch 62 is disposed at the other end of the support 10. Specifically, the first latch 61 and the second latch 62 are screwed to the support 10, and the first latch 61 and the second latch 62 are respectively disposed on the outer side of the locking assembly 30. During the takeoff or landing of the aircraft, the landing gear has inward or outward tension, and the first latch 61 and the second latch 62 are respectively arranged at the two ends of the support 10, so that the latch assembly 30 can be prevented from being separated from the support 10. It should be noted that, during installation, a certain distance is reserved between the safety catch 60 and the connecting piece 32 of the locking assembly 30, so that the landing gear can be effectively protected and prevented from being damaged.
In one embodiment, referring to fig. 1, 3 and 4, the bracket for an aerial measuring instrument further comprises a shock absorbing member 40, the shock absorbing member 40 being disposed on the transition piece 20. When installed, the damping member 40 is attached to an aerial measuring instrument 70. By arranging the damping piece 40 on the transition piece 20, the damping piece 40 can play a damping role, so that the aerial measuring instrument 70 is more stable, safe and efficient in the process of flying of the airplane, and the aerial shooting measurement precision of the aerial measuring instrument 70 is improved.
Specifically, please refer to fig. 3 and 4, the base of the damping member 40 is provided with a threaded hole, the transition member 20 is correspondingly provided with a threaded hole, and the screw penetrates through the threaded holes of the transition member 20 and the damping member 40 to detachably connect the transition member 20 and the damping member 40, so that the assembly and disassembly are simple and easy, and the assembly efficiency is improved.
Specifically, in the present embodiment, please refer to fig. 4, the damping member 40 is a damping pad. Four shock pads are provided, two of which are disposed on one side of the surface of the transition piece 20 at intervals, and the other two shock pads are disposed on the other side of the surface of the transition piece 20 correspondingly. By arranging the four shock-absorbing pads on the transition piece 20, the aerial measuring instrument 70 is more stable, safe and efficient in the process of flying of the airplane, and the aerial shooting and measuring precision of the aerial measuring instrument 70 is improved. Of course, in other embodiments, two, three or more than five shock absorbing members 40 may be provided, and the number of shock absorbing members 40 is not particularly limited herein.
Further, referring to fig. 1, 5 and 7, the bracket for an aerial surveying instrument further includes a mounting member 50, a top portion of the mounting member 50 is connected to the shock absorbing member 40, and a side portion of the mounting member 50 is used to connect the aerial surveying instrument 70. It will be appreciated that the mount 50 is a triangular mount. Specifically, the mounting member 50 includes a first mounting plate 51, a second mounting plate 52, a first baffle 53 and a second baffle 54, wherein one side of the first mounting plate 51 is connected with one side of the second mounting plate 52 to form an L-shaped structure; the first baffle 53 and the second baffle 54 are disposed on two sides of the L-shaped structure opposite to each other. The first mounting plate 51 is provided with a threaded hole, the aeronautical measuring instrument 70 is correspondingly provided with a threaded hole, and screws are sequentially arranged through the threaded holes of the first mounting plate 51 and the aeronautical measuring instrument 70 so as to detachably connect the mounting piece 50 to the aeronautical measuring instrument 70. The second mounting plate 52 is provided with a threaded hole, the shock absorbing member 40 is correspondingly provided with a threaded hole, and a screw is inserted into the threaded holes of the second mounting plate 52 and the shock absorbing member 40 so as to detachably mount the mounting member 50 on the shock absorbing member 40, so that the aeronautical measuring instrument 70 is mounted on the shock absorbing member 40 through the mounting member 50.
In one embodiment, referring to fig. 4 and 7, the transition piece 20 is a transition plate provided with a through hole 21 for fitting a lens of an aerial surveying instrument 70. Because the transition piece 20 is a transition plate, the contact area between the aerial measuring instrument 70 and the transition plate is large, so that the aerial measuring instrument 70 can be conveniently and stably installed, aerial measuring equipment is more stable in the process of flying of an airplane, and the aerial shooting and measuring precision of the aerial measuring instrument 70 is improved. When the aerial surveying instrument 70 is installed, the lens of the aerial surveying instrument 70 is correspondingly arranged at the through hole 21 of the transition plate, so that the aerial surveying instrument 70 can emit laser to the ground or carry out aerial shooting through the lens.
In one embodiment, referring to fig. 1 and 7, the supporting member 10 includes a first supporting member 11 and a second supporting member 12 which are spaced apart from each other. Four lock catch assemblies 30 are arranged, wherein two lock catch assemblies 30 are respectively arranged at two ends of the first support piece 11, and the first support piece 11 is connected with the landing gear of the airplane through the lock catch assemblies 30; two other lock catch assemblies 30 are respectively arranged at two ends of the second support 12, and the second support 12 is connected with the landing gear of the airplane through the lock catch assemblies 30. By providing the first support member 11 and the second support member 12, stable mounting of the aerial measurement instrument 70 to the bracket for an aerial measurement instrument is facilitated. In addition, the first support member 11 and the second support member 12 are respectively connected to the landing gear of the aircraft through the four locking assemblies 30, so that the installation stability is improved conveniently, and the use safety is high.
Further, referring to fig. 1 and 7, there are two first latches 61, and there are two second latches 62; the two first latches 61 are respectively disposed at one ends of the first support 11 and the second support 12, and the two second latches 62 are respectively disposed at the other ends of the first support 11 and the second support 12. During the takeoff or landing of the aircraft, the landing gear has inward or outward tension, and the first latch 61 and the second latch 62 are respectively arranged at the two ends of the support 10, so that the latch assembly 30 can be prevented from being separated from the support 10. It should be noted that, during installation, a certain distance is reserved between the safety catch 60 and the connecting piece 32 of the locking assembly 30, so that the landing gear can be effectively protected and prevented from being damaged.
Referring to fig. 1 and 7, an embodiment of an aerial surveying device includes an aerial surveying instrument 70 and a bracket for an aerial surveying instrument according to any of the embodiments described above. The aerial survey instrument 70 is provided to the transition piece 20 of the cradle for an aerial survey instrument.
In the above-described aerial surveying device, the transition piece 20 is mounted to the support 10, and the connecting piece 32 of the locking assembly 30 is connected to the support 10. When the aerial survey needs to be carried out, the lock catch piece 31 of the lock catch assembly 30 is locked on the landing gear of the airplane, and the aerial survey instrument 70 is installed on the transition piece 20, so that the aerial survey instrument 70 is externally arranged at the bottom of the airplane during operation, and thus the aerial photograph can be carried out on the ground through the aerial survey instrument 70. The aviation measuring instrument 70 can be externally arranged at the bottom of the airplane through the matching action of the supporting piece 10, the transition piece 20 and the locking assembly 30, the structure is simple, the assembly and disassembly are simple, and the improvement of the installation efficiency is facilitated. Also, the latch assembly 30 connects the support 10 and the transition piece 20 to the landing gear, so that the bracket for an aircraft measuring instrument can be smoothly mounted to the landing gear of the aircraft. In addition, the length of the supporting piece 10 and the size of the transition piece 20 are changed, so that the bracket for the aerial measuring instrument can be suitable for different types of airplanes and the aerial measuring instrument 70, and the application range is wide.
The aircraft of an embodiment includes the aircraft body and the aerial measurement device of any preceding embodiment, and the aerial measurement device is installed in the undercarriage of aircraft body.
In the aircraft described above, the transition piece 20 is mounted to the support member 10 and the attachment piece 32 of the latch assembly 30 is attached to the support member 10. When the aerial survey needs to be carried out, the lock catch piece 31 of the lock catch assembly 30 is locked on the landing gear of the airplane, and the aerial survey instrument 70 is installed on the transition piece 20, so that the aerial survey instrument 70 is externally arranged at the bottom of the airplane during operation, and thus the aerial photograph can be carried out on the ground through the aerial survey instrument 70. The aviation measuring instrument 70 can be externally arranged at the bottom of the airplane through the matching action of the supporting piece 10, the transition piece 20 and the locking assembly 30, the structure is simple, the assembly and disassembly are simple, and the improvement of the installation efficiency is facilitated. Also, the latch assembly 30 connects the support 10 and the transition piece 20 to the landing gear, so that the bracket for an aircraft measuring instrument can be smoothly mounted to the landing gear of the aircraft. In addition, the length of the supporting piece 10 and the size of the transition piece 20 are changed, so that the bracket for the aerial measuring instrument can be suitable for different types of airplanes and the aerial measuring instrument 70, and the application range is wide.
Specifically, in this embodiment, the aircraft may be a helicopter, and the aerial measurement device is externally disposed on a landing gear of the helicopter.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.
Claims (10)
1. A cradle for an aerial measuring instrument, comprising:
a support member;
a transition piece for mounting an aeronautical measuring instrument, the transition piece being mounted to the support piece;
the locking assembly is provided with a locking piece and a connecting piece, the locking piece is used for connecting an undercarriage of an airplane, and the connecting piece is connected with the supporting piece.
2. The bracket for an aerial measuring instrument according to claim 1, wherein the locking member includes a first arc-shaped plate and a second arc-shaped plate, one end of the first arc-shaped plate is detachably connected to one end of the second arc-shaped plate, and the other end of the first arc-shaped plate is detachably connected to the other end of the second arc-shaped plate.
3. The bracket for an aerial measuring instrument as defined in claim 1, wherein the connecting member is a connecting sleeve, and the connecting sleeve is disposed on the locking member.
4. The aircraft measurement instrument bracket of claim 1, further comprising a shock absorber disposed on the transition piece.
5. The bracket for an aerial measuring instrument according to claim 4, further comprising a mounting member, a top portion of the mounting member being connected to the shock absorbing member, and a side portion of the mounting member being used for connecting the aerial measuring instrument.
6. The bracket for an aerial measuring instrument according to claim 1, further comprising a safety catch, wherein the safety catch comprises a first catch and a second catch, the first catch is disposed at one end of the supporting member, the second catch is disposed at the other end of the supporting member, and the first catch and the second catch are respectively disposed at outer sides of the connecting member of the catch assembly.
7. The bracket for an aerial measuring instrument as defined in claim 1, wherein the transition piece is a transition plate provided with a through hole for fitting a lens of the aerial measuring instrument.
8. The bracket for an aerial measuring instrument according to claim 1, wherein the supporting member includes a first supporting member and a second supporting member which are arranged at intervals, and the number of the locking assemblies is four, two of the locking assemblies are respectively arranged at two ends of the first supporting member, and the other two of the locking assemblies are respectively arranged at two ends of the second supporting member.
9. An aerial surveying device, comprising an aerial surveying instrument and a carriage for an aerial surveying instrument according to any one of claims 1 to 8, the aerial surveying instrument being provided at a transition of the carriage for an aerial surveying instrument.
10. An aircraft, characterized in that it comprises an aircraft body and an aerial measurement device according to claim 9, mounted to a landing gear of the aircraft body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020555306.4U CN212056646U (en) | 2020-04-15 | 2020-04-15 | Bracket for aerial measuring instrument, aerial measuring device and airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020555306.4U CN212056646U (en) | 2020-04-15 | 2020-04-15 | Bracket for aerial measuring instrument, aerial measuring device and airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212056646U true CN212056646U (en) | 2020-12-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020555306.4U Active CN212056646U (en) | 2020-04-15 | 2020-04-15 | Bracket for aerial measuring instrument, aerial measuring device and airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212056646U (en) |
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2020
- 2020-04-15 CN CN202020555306.4U patent/CN212056646U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |