一种使用空气模块组成的临时飞机库
The main body of the aircraft hangar, composed of air modules, combined with inflatable components, wind-resistant components, and anchoring components, solves the problem of slippage and overturning of traditional air module temporary aircraft hangars in strong wind environments, achieving higher structural stability and safety.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CHENGDU HANGYU INTELLIGENT INNOVATION TECHNOLOGY SERVICE CO LTD
- Filing Date
- 2025-08-05
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional air-modular temporary hangars are prone to sliding or overturning in strong winds and cannot effectively resist wind torque and tension, leading to damage to structural integrity and limiting their application range and reliability.
The main body of the aircraft hangar is composed of multiple air blocks, combined with inflatable components, wind-resistant components, strength support components, and anchoring components. The ground contact area is increased by the support pad, the counterweight components improve the overturning resistance, and the tensioned integral structure is formed by cables and anchoring components to enhance wind resistance stability.
It effectively prevents the aircraft hangar from sliding or lifting, improves its anti-overturning strength, ensures the safety of equipment and personnel inside the hangar, and enhances its reliability under different climatic conditions.
Smart Images

Figure CN224514869U_ABST
Abstract
Claims
1. A temporary hangar using air modules, comprising a hangar body (1), the hangar body (1) being composed of multiple sets of air blocks (11), and multiple sets of inflation components (2) provided on both sides of the hangar body (1), the inflation components (2) providing gas to the interior of the multiple sets of air blocks (11), characterized in that: The air block (11) is arc-shaped, and the top of the main body of the aircraft hangar (1) is provided with a wind-resistant component (3), which improves the wind resistance of the main body of the aircraft hangar (1). The main body (1) of the aircraft hangar is provided with strength support components (4) on both sides. The strength support components (4) include a support pad (41), a counterweight component (42) and an anchoring component (43). The support pad (41) is fixedly installed at the bottom of the main body (1) of the aircraft hangar to increase the contact area between the main body (1) of the aircraft hangar and the ground. The counterweight component (42) and the anchoring component (43) have the function of improving the overturning resistance of the main body (1) of the aircraft hangar. A connecting component (5) is provided on the top of the counterweight component (42). The connecting component (5) connects the counterweight component (42) and the wind-resistant component (3). The anchoring component (43) can be stored inside the counterweight component (42).
2. A temporary hangar consisting of air modules according to claim 1, characterized in that: The inflation assembly (2) includes an inflation pump body (21), a connecting pipe (22), an inflation pipe (23), and a fastening ring (24). The connecting pipe (22) is fixedly installed at the air outlet of the inflation pump body (21). Multiple sets of the inflation pipes (23) are fixedly installed on the outer wall of the connecting pipe (22). Inflation sleeves (111) are fixedly connected to the bottom of both sides of the air block (11). The inflation sleeves (111) are sleeved on the outer peripheral wall of the inflation pipe (23). The fastening ring (24) fixes the inflation sleeves (111) and the inflation pipe (23).
3. A temporary hangar composed of air modules according to claim 2, characterized in that: The wind-resistant component (3) includes a first cable (31) and two sets of second cables (32), with multiple sets of the first cable (31) and two sets of second cables (32) evenly distributed along the top of the main body (1) of the aircraft hangar.
4. A temporary hangar composed of air modules according to claim 3, characterized in that: The counterweight assembly (42) consists of a first counterweight block (421) and a second counterweight block (422). The first counterweight block (421) and the second counterweight block (422) are composed of the same components. The first counterweight block (421) and the second counterweight block (422) are located on both sides of the main body of the aircraft hangar (1) and are arranged symmetrically.
5. A temporary hangar comprised of air modules according to claim 1, characterized in that: The connecting component (5) includes a first connecting ring (51) and a second connecting ring (52), which are respectively fixedly installed on the top sides of the first counterweight (421) and the second counterweight (422).
6. A temporary hangar comprised of air modules according to claim 3, characterized in that: The two ends of the first cable (31) are connected to the first connecting rings (51) on both sides by buckles, and the two ends of the two sets of second cables (32) are connected to the first connecting rings (51) and the second connecting rings (52) on both sides by buckles.
7. A temporary hangar comprised of air modules according to claim 1, characterized in that: The anchoring assembly (43) includes a ground anchor fixing tip (431), an extension plate (432), a first limiting plate (433), a second limiting plate (434), and a sliding groove (435). The ground anchor fixing tip (431) is disposed on both sides of the top of the extension plate (432), and the bottom of the ground anchor fixing tip (431) passes through the extension plate (432) and is inserted into the ground surface layer.
8. A temporary hangar composed of air modules according to claim 7, characterized in that: The groove (435) is opened on the inner walls of both sides of the counterweight. The two sides of the extension plate (432) are slidably connected inside the groove (435). The first limiting plate (433) is fixedly installed on the outer wall of the extension plate (432). The second limiting plate (434) is fixedly installed on the top of the two sets of ground anchor fixing tips (431). The first limiting plate (433) and the second limiting plate (434) are respectively attached to the outer walls of both sides of the counterweight.