Aircraft environment test loading and unloading integrated device

Abstract

The utility model discloses an aircraft environment test loading and unloading integrated device, which comprises an object carrying support, an object lifting belt and a flexible embracing ring, the object carrying support is connected with the object lifting belt, and the flexible embracing ring is arranged on the object lifting belt. And a stable plane is arranged at the bottom of the carrying support. The loading support comprises a left half ring and a right half ring, connecting flanges are arranged on the left half ring and the right half ring, and the connecting flanges are connected through bolts. And a cushion layer is arranged between the connecting flanges. A buffer protection layer is arranged on the inner contact surface of the carrying support. The flexible embracing ring is of a connecting structure selected from a belt buckle, a nylon buckle and a hook-and-loop fastener. And a tensile piece is arranged in the object lifting belt. A lifting ring is arranged on the object carrying support, a lifting hook is arranged on one side of the object lifting belt, and the object lifting belt and the object carrying support are connected through cooperation of the lifting hook and the lifting ring. The problems of safety, operation and the like existing in an aircraft environment test are solved, and convenience is provided for test arrangement, test preparation completion and product disassembly of a product environment test.

Description

Technical Field

[0001] The utility model belongs to the field of handling tooling, and in particular relates to an integrated loading and unloading device for an aircraft environmental test. Background Art

[0002] Aircraft include aerial vehicles and underwater vehicles, and their appearance is mainly columnar. Due to the large differences in the appearance of aircraft, the corresponding environmental test loading and unloading structures are different. The structures are configured according to the complexity of the products. Borrowing may lead to unsafe factors in the test process. In order to meet the requirements of environmental test loading and unloading, solve the problems of environmental test characteristics, performance testing and other aspects of aircraft products, a multi-adaptable environmental test loading and unloading device is provided. Utility Model Content

[0003] The purpose of the utility model is to provide an integrated assembly and disassembly device for an aircraft environmental test, so as to meet the requirements of the spacecraft environmental test and improve its adaptability.

[0004] In order to solve the above problems, the utility model discloses an integrated device for loading and unloading an aircraft environmental test, including a load tray, a lifting belt and a flexible holding ring, wherein the load tray is connected to the lifting belt, and the flexible holding ring is arranged on the lifting belt.

[0005] As a further improvement of the above technical solution:

[0006] The bottom of the object carrier is provided with a stable plane.

[0007] The object carrier includes a left half ring and a right half ring, and the left half ring and the right half ring are provided with connecting flanges, and the connecting flanges are connected by bolts.

[0008] A cushion layer is provided between the connecting flanges.

[0009] The inner contact surface of the object carrier is provided with a buffer protection layer.

[0010] The flexible holding ring is a connecting structure such as a belt buckle, a nylon buckle or a Velcro.

[0011] A tensile member is provided in the lifting belt.

[0012] The object carrier is provided with a lifting ring, and one side of the object lifting belt is provided with a lifting hook, and the object lifting belt and the object carrier are connected by the cooperation of the lifting hook and the lifting ring.

[0013] A handle is provided on the upper portion of the lifting belt.

[0014] The inner diameter of the object carrier decreases from top to bottom.

[0015] Compared with the prior art, the beneficial effects of the present invention are:

[0016] This utility model's integrated loading and unloading device for aircraft environmental testing includes a lifting strap, a flexible holding ring, and a loading tray. The lifting strap and the loading tray are connected through positioning holes, and the flexible holding ring and the lifting strap are sewn together to form a single unit. The product is placed on the loading tray, and the entire device is lifted by the lifting strap for environmental testing, achieving integrated loading and unloading. The structure is safe and reliable, and the design ensures that the product will not tip over during loading and unloading. The structure is compact, and the length of the lifting strap can be adjusted as needed. Operation is simple and convenient, requiring two people to work together, with each person completing the loading and unloading of the product using only one hand. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the overall structure of the utility model;

[0018] Figure 2 This is a schematic diagram of the internal structure of the utility model;

[0019] Figure 3 This is a side view of the structure of the utility model;

[0020] Figure 4 This is a schematic diagram of the structure of the object carrier of the present invention from a top view.

[0021] Figure numerals: 1. lifting strap; 2. flexible holding ring; 3. load carrier; 31. stabilizing plane; 32. left half ring; 33. right half ring; 11. handle; 34. connecting flange; 35. bolt; 4. aircraft. DETAILED DESCRIPTION

[0022] In order to make the technical means, creative features, objectives and effects achieved by the present invention easier to understand, the present invention is further described below in conjunction with specific implementation methods.

[0023] In the description of this utility model, 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, indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings and are intended solely to facilitate the description of this utility model and simplify the description. They are not intended to indicate or imply that the devices or components referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0024] In the description of this utility model, it should be noted that, unless otherwise expressly specified or limited, the terms "installed," "provided with," "connected," etc. should be understood in a broad sense. For example, "connected" can mean a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, or it can be internal communication between two components. Those skilled in the art will be able to understand the specific meanings of the above terms in this utility model based on the specific circumstances.

[0025] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0026] like Figures 1 to 4 As shown, this embodiment of the integrated loading and unloading device for aircraft environmental testing includes a carrier 3, a lifting belt 1, and a flexible ring 2. The carrier 3 is connected to the lifting belt 1, and the flexible ring 2 is mounted on the lifting belt 1. A stabilizing surface 31 is provided at the bottom of the carrier 3. This device improves the integrated loading and unloading device for product environmental testing, solves safety and operational issues associated with aircraft product environmental testing, and facilitates test setup, test preparation, and product disassembly. It features a safe and reliable structure, a compact size, adjustable design, and easy operation.

[0027] The cargo tray 3 comprises a left half-ring 32 and a right half-ring 33, each provided with a connecting flange 34 connected by bolts 35. A cushion is provided between the connecting flanges 34. Using a split cargo tray 3 enhances its adaptability and accommodates a wider range of aircraft sizes.

[0028] A buffering protective layer is provided on the inner contact surface of the carrier 3. The buffering protective layer is made of silicone material to prevent the carrier 3 from rigidly contacting the aircraft 4 and causing damage to the surface of the aircraft 4.

[0029] The flexible holding ring 2 is a connecting structure such as a belt buckle, a nylon buckle or a Velcro. The flexible holding ring 2 fixes the upper part of the aircraft 4. The belt body with an adjustable diameter is used as the holding ring, and the adjustment mode of the holding ring can be freely selected.

[0030] A tensile member is provided in the lifting belt 1. The lifting belt 1 is prone to breakage after long-term use, so a lifting belt 1 with a tensile member is selected. The tensile member can be made of metal wire or other tensile materials.

[0031] A lifting ring is provided on the load tray 3, and a hook is provided on one side of the lifting belt 1. The connection between the lifting belt 1 and the load tray 3 is achieved by the cooperation of the hook and the lifting ring.

[0032] The top of the lifting belt 1 is provided with a handle 11. The setting of the handle 11 is convenient for the user to grasp, and the handle 11 is a soft material.

[0033] The inner diameter of the carrier 3 decreases from top to bottom. Since the outer diameter of the entry section of the aircraft 4 is in a gradually increasing form, the arrangement of the carrier 3 is conducive to the restriction of the aircraft 4.

[0034] During use, the carrier 3 is placed next to the aircraft 4. Using specialized equipment, the aircraft 4 is inserted into the carrier 3, completing the installation. The flexible holding loops 2 are then placed around the aircraft 4. Multiple flexible holding loops 2 can be provided depending on the stability requirements. It is best to manually lift the lifting strap 1 using the handle 11 to carry the aircraft 4 to the environmental test site for temperature testing. Once the test is complete, the lifting strap 1 is lifted to remove the aircraft 4.

[0035] The aircraft environmental test assembly and disassembly integrated device of the utility model has a compact and reliable structure and is safe, simple, quick and convenient to operate.

[0036] The above is only an embodiment of the present invention, and common knowledge such as the specific structure and characteristics of the scheme are not described in detail here. For those skilled in the art, it is obvious that the present invention is not limited to the details of the above exemplary embodiments, and the present invention can be implemented in other specific forms without departing from the spirit or basic characteristics of the present invention. Therefore, no matter from which point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the present invention is limited by the appended claims rather than the above description, and it is intended that all changes that fall within the meaning and scope of the equivalent elements of the claims are included in the present invention. Any figure mark in the claims should not be regarded as limiting the claim involved.

Claims

1. An integrated device for loading and unloading an aircraft environmental test, characterized in that: The utility model comprises a carrier (3), a lifting belt (1) and a flexible holding ring (2); the carrier (3) is connected to the lifting belt (1), and the flexible holding ring (2) is arranged on the lifting belt (1).

2. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The bottom of the object carrier (3) is provided with a stabilizing plane (31).

3. The integrated assembly and disassembly device for aircraft environmental testing according to claim 2, characterized in that: The object carrier (3) comprises a left half ring (32) and a right half ring (33), and the left half ring (32) and the right half ring (33) are provided with connecting flanges (34), and the connecting flanges (34) are connected by bolts (35).

4. The integrated assembly and disassembly device for aircraft environmental testing according to claim 3, characterized in that: A cushion layer is provided between the connecting flanges (34).

5. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The inner contact surface of the object carrier (3) is provided with a buffer protection layer.

6. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The flexible holding ring (2) is a connection structure such as a belt buckle, a nylon buckle, or a Velcro.

7. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The lifting belt (1) is provided with a tensile member.

8. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The object carrier (3) is provided with a lifting ring, and one side of the object lifting belt (1) is provided with a lifting hook, and the connection between the object lifting belt (1) and the object carrier (3) is achieved through the cooperation of the lifting hook and the lifting ring.

9. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: A handle (11) is provided on the upper portion of the lifting belt (1).

10. The integrated assembly and disassembly device for aircraft environmental testing according to claim 1, characterized in that: The inner diameter of the object carrier (3) decreases from top to bottom.

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