Novel hangar
By designing a new type of hangar with an arc-shaped structure, the problem of exceeding the approved building area in hangar projects was solved, achieving control of building area and standardization of hangars, and reducing the impact of engineering design.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CHINA AVIATION INT CONSTR & INVESTMENT CO LTD
- Filing Date
- 2025-04-21
- Publication Date
- 2026-06-09
Smart Images

Figure CN224338709U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the field of hangar construction, and more specifically, to a new type of hangar. Background Technology
[0002] Hangars are essential supporting facilities for civil aviation and general aviation airports. In recent years, the construction, renovation and expansion of airports in my country have developed rapidly. Against this backdrop, a large number of hangar projects have been reported for construction in batches.
[0003] During the batch reporting process of new hangar construction projects, some users submitted usable areas instead of building areas. As a result, the areas reported and approved in the early stages were all smaller than the building areas, which caused the building areas and costs in the later engineering design to exceed the approved areas and costs, greatly affecting the engineering design.
[0004] Therefore, how to reduce the impact on engineering design has become a technical problem that needs to be solved in this field. Utility Model Content
[0005] In view of this, this application proposes a new type of hangar to reduce the impact on engineering design.
[0006] This application proposes a novel hangar comprising: a main structure standing on the ground, the main structure including a first substructure, a second substructure, a third substructure, and a fourth substructure, the first substructure, the second substructure, the third substructure, and the fourth substructure being sequentially connected to define an internal space for placing an aircraft; wherein the first substructure and the third substructure are positioned opposite each other and their orthographic projections on the ground are both straight, and the second substructure and the fourth substructure are positioned opposite each other and their orthographic projections on the ground are both arc-shaped; wherein the area of the first shape is a preset approved area, and the first shape is the shape enclosed by the orthographic projections of the main structure on the ground.
[0007] Optionally, the novel hangar further includes: a hangar cover structure, the main structure supporting the hangar cover structure, the second shape being the same as the first shape, wherein the second shape is the shape of the orthographic projection of the hangar cover structure on the ground.
[0008] Optionally, the second substructure and / or the fourth substructure are equipped with a door.
[0009] Optionally, the warehouse door is an arc-shaped side-turn door.
[0010] Optionally, the warehouse door is a double-sided arc-shaped revolving door.
[0011] Optionally, the first substructure and / or the third substructure are provided with windows.
[0012] According to the technical solution of this application, the orthographic projections of the second and fourth substructures on the ground are arc-shaped, that is, the second and fourth substructures are designed as arc-shaped structures, so that the area of the shape enclosed by the orthographic projections of the main structure on the ground is the pre-approved area, thereby ensuring that the building area and cost in the engineering design will not exceed the approved area and cost, thus reducing the impact on the engineering design.
[0013] Other features and advantages of this application will be described in detail in the following detailed description section. Attached Figure Description
[0014] The accompanying drawings, which form part of this application, are used to provide a further understanding of this application, and the illustrative embodiments and descriptions thereof are used to explain this application. In the drawings:
[0015] Figure 1 This is a top view of a novel hangar according to a preferred embodiment of this application;
[0016] Figure 2 A rendering of a novel hangar according to a preferred embodiment of this application; and
[0017] Figure 3 This is a rendering of a novel hangar according to a preferred embodiment of this application. Detailed Implementation
[0018] The technical solution of this application will now be described in detail with reference to the accompanying drawings and embodiments.
[0019] This application provides a novel hangar.
[0020] like Figure 1 As shown, the new hangar includes a main structure. The main structure is the wall structure of the new hangar. The main structure stands on the ground. The main structure includes a first substructure 10, a second substructure 20, a third substructure 30, and a fourth substructure 40. The first substructure 10, the second substructure 20, the third substructure 30, and the fourth substructure 40 are connected sequentially to define an internal space 50 for placing aircraft.
[0021] like Figure 1 As shown, the first substructure 10 and the third substructure 30 are positioned opposite each other, and their orthographic projections on the ground are both straight. In other words, the first substructure 10 and the third substructure 30 are straight structures.
[0022] like Figure 1 As shown, the second substructure 20 and the fourth substructure 40 are positioned opposite each other, and their orthographic projections on the ground are both arc-shaped. In other words, the second substructure 20 and the fourth substructure 40 are arc-shaped structures.
[0023] The area of the first shape is the pre-approved area, and the first shape is the shape formed by the orthographic projection of the main structure on the ground.
[0024] It should be noted that, Figure 1 Two new types of hangars are shown. In practical applications, the number of new hangars can be determined according to specific circumstances, and there is no limit to this.
[0025] In this embodiment, the net usable dimensions of the aircraft to the first substructure 10, second substructure 20, third substructure 30, and fourth substructure 40 can be determined based on the aircraft type to be parked in the new hangar. The net usable dimension is the safe distance from the aircraft. In this embodiment, the aircraft type to be parked in the new hangar construction project can be determined first. Based on the aircraft size, the safe distances to surrounding obstacles such as the aircraft wings, nose, and tail can be determined, thereby determining the rectangular net usable dimensions of the new hangar, i.e., the net usable dimensions of the aircraft to the first substructure 10, second substructure 20, third substructure 30, and fourth substructure 40.
[0026] The second substructure 20 and / or the fourth substructure 40 are equipped with storage doors 60. For example... Figure 2 As shown, the fourth substructure 40 is equipped with a double-sided arc-shaped revolving door 601. When open, the double-sided arc-shaped revolving door 601 moves towards the first substructure 10 and the third substructure 30 from the middle position respectively; when closed, the double-sided arc-shaped revolving door 601 moves towards the middle from the first substructure 10 and the third substructure 30 respectively.
[0027] In this embodiment, the double-sided arc-shaped revolving door 601 can be an arc-shaped track sliding door with a steel frame structure, bearing the load at the bottom and guiding at the top. The control method combines central control and individual control, with an operating speed of 8-10 meters per minute. In addition, the double-sided arc-shaped revolving door 601 also has a manual opening function, allowing the door to be opened manually or with the assistance of a power source in case of power outages or emergencies.
[0028] Optionally, in this embodiment, the garage door 60 can be an arc-shaped revolving door. The arc-shaped revolving door can be a double-sided arc-shaped revolving door or a single-sided arc-shaped revolving door. Specifically, a single-sided arc-shaped revolving door rotates from one side to the other when opening and closing. For example, […]. Figure 2 The double-sided arc-shaped revolving door 601 shown is replaced with a single-sided arc-shaped revolving door. When it is open, it rotates from the first substructure 10 to the third substructure 30, and when it is closed, it rotates from the third substructure 30 to the first substructure 10, and vice versa.
[0029] Optionally, in embodiments of this application, the first substructure 10 and / or the third substructure 30 are provided with windows. For example... Figure 2As shown, both the first substructure 10 and the third substructure 30 are provided with windows. It should be noted that, in the embodiments of this application, when windows are provided, the appearance and number of windows can be determined according to specific circumstances, and there are no restrictions on this.
[0030] Optionally, in an embodiment of this application, the novel hangar further includes a hangar cover structure 70. For example... Figure 3 As shown, the cover structure 70 covers the main structure. The main structure supports the cover structure 70, and the second shape is the same as the first shape, wherein the second shape is the shape of the orthographic projection of the cover structure 70 on the ground.
[0031] Optionally, in this embodiment, the cover structure 70 can be a steel space frame structure.
[0032] In this embodiment, the cover structure 70 is a circular structure with an arc edge, which saves steel and reduces costs.
[0033] In this embodiment, the second and fourth substructures are designed as arc-shaped structures, making the new hangar similar to a cylinder. This effectively solves the problem of insufficient approved building area failing to meet usage requirements. It not only reduces the building area but also still meets the hangar's usage needs, thus ensuring the smooth progress of the engineering design. The technical solution provided by this embodiment satisfies the hangar's usage requirements without exceeding the approved area, and can be standardized according to different aircraft models, facilitating engineering design.
[0034] The technical solution provided in this application can be applied to projects where the approved area is insufficient to meet the hangar usage requirements. It proposes a new type of hangar similar to a cylinder, which 1) can save building area, reduce project investment, and ensure design progress while meeting hangar usage requirements and not exceeding the approved area; 2) can achieve standardization and modularization of the hangar according to different commonly used aircraft models, which is convenient for the engineering design of other similar related projects.
[0035] The preferred embodiments of this application have been described in detail above. However, this application is not limited to the specific details of the above embodiments. Within the scope of the technical concept of this application, various simple modifications can be made to the technical solution of this application, and these simple modifications all fall within the protection scope of this application.
[0036] It should also be noted that the various specific technical features described in the above embodiments can be combined in any suitable manner without contradiction. In order to avoid unnecessary repetition, this application will not describe the various possible combinations separately.
[0037] Furthermore, various different implementations of this application can be combined in any way, as long as they do not violate the spirit of this application, they should also be regarded as the content disclosed in this application.
Claims
1. A novel hangar, characterized in that, The new hangar includes: The main structure stands on the ground. The main structure includes a first substructure, a second substructure, a third substructure, and a fourth substructure. The first substructure, the second substructure, the third substructure, and the fourth substructure are connected in sequence to define an internal space for placing the aircraft. Wherein, the first substructure and the third substructure are positioned opposite each other and their orthographic projections on the ground are both straight, while the second substructure and the fourth substructure are positioned opposite each other and their orthographic projections on the ground are both arc-shaped; The area of the first shape is the preset approved area, and the first shape is the shape formed by the orthographic projection of the main structure on the ground.
2. The novel hangar according to claim 1, characterized in that, The new hangar also includes: A warehouse cover structure, wherein the main structure supports the warehouse cover structure, and the second shape is the same as the first shape, wherein the second shape is the shape of the orthographic projection of the warehouse cover structure on the ground.
3. The novel hangar according to claim 1, characterized in that, The second substructure and / or the fourth substructure are equipped with a door.
4. The novel hangar according to claim 3, characterized in that, The warehouse door is an arc-shaped side-turn door.
5. The novel hangar according to claim 4, characterized in that, The warehouse door is a double-sided curved revolving door.
6. The novel hangar according to claim 1, characterized in that, The first substructure and / or the third substructure are provided with windows.