阅读说明：本技术 一种试验试飞一体化保障方舱 (Integrated guarantee shelter for test flight ) 是由 戴磊 刘潇 林鹏 左林玄 曾宏刚 于 2019-09-11 设计创作，主要内容包括：本申请属于飞机试飞保障技术领域,特别涉及一种试验试飞一体化保障方舱。方舱包括：沿长度方向依次设置的可扩展工作舱和设备舱,所述可扩展工作舱沿宽度方向的一侧依次设置有6个工作席位,所述可扩展工作舱可沿宽度方向向另一侧扩展,所述可扩展工作舱的扩展部分可设置可折叠收纳的桌子和座椅,且对应的舱壁上安装有投影幕布及白板；在扩展前,工作人员能够经过所述设备舱进入所述可扩展工作舱,在扩展后,工作人员能够经过所述设备舱或者直接从外部进入所述可扩展工作舱；所述设备舱沿宽度方向的两侧均布置有3个减震机柜和1个储物柜,所述设备舱沿长度方向的两端均设置有舱门；所述方舱的顶部设置有天线、视频监控设备以及室外照明设备。(The application belongs to the technical field of airplane test flight guarantee, and particularly relates to an integrated guarantee shelter for test flight. The shelter includes: the extensible working cabin and the equipment cabin are sequentially arranged along the length direction, one side of the extensible working cabin along the width direction is sequentially provided with 6 working seats, the extensible working cabin can be extended to the other side along the width direction, an extension part of the extensible working cabin can be provided with a foldable table and a foldable seat, and a projection curtain and a white board are arranged on the corresponding cabin wall; before the expansion, workers can enter the expandable working cabin through the equipment cabin, and after the expansion, the workers can enter the expandable working cabin through the equipment cabin or directly from the outside; the two sides of the equipment cabin in the width direction are uniformly provided with 3 damping cabinets and 1 storage cabinet, and the two ends of the equipment cabin in the length direction are provided with cabin doors; and the top of the shelter is provided with an antenna, video monitoring equipment and outdoor lighting equipment.)

1. the utility model provides an experimental integrated guarantee shelter that tries to fly, its characterized in that, the shelter includes: an expandable working cabin and an equipment cabin which are arranged along the length direction in sequence, wherein,

One side of the expandable working cabin along the width direction is sequentially provided with 6 working seats, the expandable working cabin can be expanded to the other side along the width direction, after the expandable working cabin is expanded, the expansion part of the expandable working cabin is provided with a foldable table and a foldable seat, and a projection curtain and a white board are arranged on the corresponding cabin wall; the expandable working cabin is provided with a cabin door, before expansion, workers can enter the expandable working cabin through the equipment cabin, and after expansion, the workers can enter the expandable working cabin through the equipment cabin or directly from the outside;

the two sides of the equipment cabin in the width direction are uniformly provided with 3 damping cabinets and 1 storage cabinet, and the two ends of the equipment cabin in the length direction are provided with cabin doors;

and the top of the shelter is provided with an antenna, video monitoring equipment and outdoor lighting equipment.

2. The integrated guarantee shelter for test flight according to claim 1,

Under the test flight test scene, 6 work seats include: a flight control seat, a flight planning and data monitoring seat, an airborne test data monitoring seat, a task command seat, a ground data chain and equipment monitoring seat and a monitoring scheduling seat;

in a ground test scenario, the 6 work seats include: the system comprises a visual display seat, an interface simulation control seat, a flight simulation control seat, a main control seat, a data monitoring seat and a monitoring and dispatching seat.

3. The integrated guarantee shelter for test flight according to claim 2, wherein each work seat is provided with a table and a seat, the table is provided with a first display, and a window and a second display are arranged on the wall of the shelter on the same side as the work seat.

4. The integrated guarantee shelter for test flight according to claim 3, wherein the first display is a 24-inch display provided with a shock absorber, and the second display is a 60-inch display and is mounted on the shelter wall through a shock absorption bracket.

5. The integrated guarantee shelter for test flight according to claim 1, wherein 5 antennas are arranged at the top of the shelter, and comprise an image chain antenna, a telemetry data chain antenna, a differential data chain antenna, a GNSS base station antenna and a talkback radio antenna.

6. The integrated guarantee shelter for test flight according to claim 5, wherein 3 video monitoring devices are arranged at the top of the shelter, and comprise 1 pan-tilt monitoring camera and 2 fixed monitoring cameras.

7. the integrated guarantee shelter for test flight according to claim 6, wherein 4 outdoor lighting devices are arranged at the top of the shelter, 1 outdoor lighting device is arranged on a tripod head, and 3 outdoor lighting devices are arranged at the top edge of the shelter.

8. The integrated guarantee shelter for test flight according to claim 1, wherein the shelter is provided with an air conditioner and an oil tank.

9. The integrated guarantee shelter for test flight according to claim 1, wherein the shelter is provided with a lifting mechanism.

10. The integrated guarantee shelter for test flight according to claim 1, wherein a partition door is arranged between the expandable working shelter and the equipment shelter.

Technical Field

The application belongs to the technical field of airplane test flight guarantee, and particularly relates to an integrated guarantee shelter for test flight.

Background

With the vigorous development of the unmanned aerial vehicle industry at home and abroad, a large number of outfield debugging, testing and test flying requirements of unmanned aerial vehicle systems are derived. For the test flight of unmanned planes and carrier rockets, station environment support is needed. The airport that is fit for unmanned aerial vehicle to test to fly is usually far away, and the guarantee condition is limited, can't provide sufficient test and the official working place that flies of test and test for unmanned aerial vehicle. In addition, the transportation and debugging of the test equipment greatly occupy the effective working time of scientific research personnel; the micro and small unmanned aerial vehicle usually uses a notebook, a storage battery, a portable table and chair and a tent to carry out test flight work, a fixed working environment is not provided, a large amount of time is consumed for test preparation and recovery, and equipment is easy to omit or damage; the ground station vehicle modified from the light bus is convenient for road maneuvering, test preparation and withdrawing, but has small space and limited bearing capacity. The unmanned aerial vehicle can not carry a large number of test cabinets and various antennas, is not suitable for medium and large unmanned aerial vehicles with complex systems, and is used for long-time and full-factor test, debugging and preparation before test flight.

Accordingly, a technical solution is desired to overcome or at least alleviate at least one of the above-mentioned drawbacks of the prior art.

Disclosure of Invention

The application aims at providing an integrated guarantee shelter for test flight test, and solving at least one problem existing in the prior art.

The technical scheme of the application is as follows:

an integrated guarantee shelter for test flight, the shelter comprising: an expandable working cabin and an equipment cabin which are arranged along the length direction in sequence, wherein,

one side of the expandable working cabin along the width direction is sequentially provided with 6 working seats, the expandable working cabin can be expanded to the other side along the width direction, after the expandable working cabin is expanded, the expansion part of the expandable working cabin is provided with a foldable table and a foldable seat, and a projection curtain and a white board are arranged on the corresponding cabin wall; the expandable working cabin is provided with a cabin door, before expansion, workers can enter the expandable working cabin through the equipment cabin, and after expansion, the workers can enter the expandable working cabin through the equipment cabin or directly from the outside;

the two sides of the equipment cabin in the width direction are uniformly provided with 3 damping cabinets and 1 storage cabinet, and the two ends of the equipment cabin in the length direction are provided with cabin doors;

and the top of the shelter is provided with an antenna, video monitoring equipment and outdoor lighting equipment.

Alternatively,

under the test flight test scene, 6 work seats include: a flight control seat, a flight planning and data monitoring seat, an airborne test data monitoring seat, a task command seat, a ground data chain and equipment monitoring seat and a monitoring scheduling seat;

In a ground test scenario, the 6 work seats include: the system comprises a visual display seat, an interface simulation control seat, a flight simulation control seat, a main control seat, a data monitoring seat and a monitoring and dispatching seat.

Optionally, each work seat is provided with a table and a seat, the table is provided with a first display, and a bulkhead on the same side as the work seat is provided with a window and a second display.

Optionally, the first display is a 24-inch display equipped with a shock absorber, and the second display is a 60-inch display mounted on the bulkhead through a shock-absorbing bracket.

Optionally, the top of the shelter is provided with 5 antennas, including an image chain antenna, a telemetry data chain antenna, a differential data chain antenna, a GNSS base station antenna, and a walkie-talkie antenna.

optionally, the top of the shelter is provided with 3 video monitoring devices, including 1 pan-tilt monitoring camera and 2 fixed monitoring cameras.

Optionally, 4 outdoor lighting devices are arranged on the top of the shelter, wherein 1 outdoor lighting device is installed on the tripod head, and 3 outdoor lighting devices are installed on the top edge of the shelter.

Optionally, the shelter is configured with an air and fuel tank.

Optionally, the shelter is provided with a lifting mechanism.

Optionally, a partition door is configured between the expandable working cabin and the equipment cabin.

The invention has at least the following beneficial technical effects:

The test flight integrated guarantee shelter is a multifunctional test flight guarantee shelter integrating tests, test flights, meetings and outfield rest, and can be loaded and unloaded without the aid of large tools such as cranes, forklifts and the like; the shelter integrates three functions of ground test, test flight test and guarantee, and the integration level is high; the assembling and debugging time of the test equipment is saved for scientific research personnel, and the working efficiency is improved; providing a relatively comfortable working environment, and relieving the fatigue of long-time outfield tests; the long-time on-site test and the test flight of the medium-large unmanned aerial vehicle are suitable, and the test flight device is also suitable for the test flight related to the small unmanned aerial vehicle.

Drawings

FIG. 1 is a top view of the interior of an integrated assurance shelter of an embodiment of the present application prior to expansion of a test flight;

FIG. 2 is an internal side view of a test flight integrated assurance shelter of one embodiment of the present application;

FIG. 3 is a top view of the interior of an expanded integrated assurance shelter of a test flight test according to one embodiment of the present application;

Fig. 4 is a layout diagram of a top of a test flight integrated guarantee shelter according to an embodiment of the present application.

Detailed Description

In order to make the implementation objects, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are a subset of the embodiments in the present application and not all embodiments in the present application. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present application and should not be construed as limiting the present application. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application. Embodiments of the present application will be described in detail below with reference to the accompanying drawings.

In the description of the present application, it is to be understood that the terms "center", "longitudinal", "lateral", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience in describing the present application and for simplifying the description, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed in a particular orientation, and be operated, and therefore should not be construed as limiting the scope of the present application.

The present application is described in further detail below with reference to fig. 1 to 4.

the application provides an experimental integrated guarantee shelter that tries to fly, the shelter includes: the extensible working cabin and the equipment cabin are sequentially arranged along the length direction.

The utility model provides an experimental integrated guarantee shelter that tries to fly to design on the basis of 12 meters standard collection dress, does not join in marriage the chassis, adopts the transportation of standard container tractor, and for loading and unloading, the shelter can take elevating system certainly for loading and unloading and adjustment level, reduction maintenance and cost of transportation. The shelter comprises an expandable working cabin and an equipment cabin which are sequentially arranged along the length direction, and noise isolation is carried out through a partition door.

Specifically, one side of expanded work cabin edge width direction has set gradually 6 fixed work seats, and under the experimental scene of trying to fly away, the work seat includes: the system comprises a flight control seat, a flight planning and data monitoring seat, an airborne test data monitoring seat, a task command seat, a ground data chain and equipment monitoring seat and a monitoring and dispatching seat. Under the ground test scene, the work seat includes: the system comprises a visual display seat, an interface simulation control seat, a flight simulation control seat, a main control seat, a data monitoring seat and a monitoring and dispatching seat. Each work seat is provided with a table and a seat, the table of the work seat is an integrated table, 10 24-inch first displays with shock absorbers are arranged on the table, 2 windows are arranged on the bulkhead on the same side of the work seat, and 2 60-inch second displays with shock-absorbing brackets are arranged on the bulkhead.

in order to meet the requirement of a working space, the extensible working cabin adopts a unilateral extension mode, and during the test period, the cabin of the extensible working cabin is used as a working area, a meeting area and a rest area. The expandable working cabin can be expanded to the other side along the width direction, after the expandable working cabin is expanded, the expansion part of the expandable working cabin is provided with a foldable table and a foldable seat, and a projection curtain and a white board for a conference are installed on the corresponding cabin wall. The area of the working cabin is increased by about 15m after being expanded²Meeting conditions of not less than 10 persons and providing rest space for the staff.

Furthermore, 3 damping cabinets and 1 storage cabinet are uniformly arranged on two sides of the equipment cabin in the width direction, the length, the width and the height of each damping cabinet are not less than 600, 800 and 200mm, and the cabinets can be rapidly and integrally detached. The length multiplied by the width multiplied by the height of the storage cabinet is not less than 2000 multiplied by 600 multiplied by 2000mm, and the storage cabinet is used for storing experimental equipment.

the both ends of equipment cabin edge length direction all are provided with the hatch door, the hatch door of its afterbody is two divisions of doors, supply personnel and equipment to get into the equipment cabin, set up double-deck hatch door between equipment cabin and the expanded work cabin, expanded work cabin is before the extension, personnel get into the work cabin through the equipment cabin, the shelter extension back, personnel can get into the work cabin through the equipment cabin or directly from the outside, the staff can get into expanded work cabin through the equipment cabin, after the extension, the staff can get into expanded work cabin through the equipment cabin or directly from the outside.

the top of the shelter is provided with an antenna, video monitoring equipment and outdoor lighting equipment. In one embodiment of the present application, the shelter roof is equipped with 5 antennas including an image chain antenna, a telemetry data chain antenna, a differential data chain antenna, a GNSS base station antenna, and a walkie-talkie antenna, via a support. The 3 video monitoring equipment comprises 1 pan-tilt monitoring camera and 2 monitoring cameras. 4 outdoor lighting, 1 of which is arranged at the pan-tilt and 3 at the top edge of the shelter. The shelter of the present application is also configured with an air conditioner and an oil tank.

The utility model provides an experimental integrated guarantee shelter that tries to fly is experimental, tries to fly, meeting and outfield rest multi-functional experimental guarantee shelter as an organic whole, and this shelter mainly used has man-machine, unmanned aerial vehicle etc. to prepare before the experimental debugging, maintenance, test, the trying to fly of fixed outfield, the control of trying to fly, meeting discussion and rest.

The test flight integrated guarantee shelter simplifies the processes of loading, unloading and environment debugging of the outfield test equipment, and reduces the preparation time and the withdrawing time before the test; after the shelter is unfolded, the shelter does not need to be folded, so that the effective working time of the outfield test can be prolonged, and the test preparation before dawn and the test collection after night are convenient; safe storage environments are provided for internal and confidential equipment related to the test, the safety and the efficiency are improved, and omission is avoided; the comfortable outfield condition is provided, the test working efficiency is improved, the labor intensity of workers is reduced, the fatigue is relieved, and the delay of the test progress caused by waiting for weather and the like is avoided; provides a good environment for the external field test discussion and decision.

The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present application should be covered within the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.