CN115848080A - Manned airborne vehicle - Google Patents
Manned airborne vehicle Download PDFInfo
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- CN115848080A CN115848080A CN202310187059.5A CN202310187059A CN115848080A CN 115848080 A CN115848080 A CN 115848080A CN 202310187059 A CN202310187059 A CN 202310187059A CN 115848080 A CN115848080 A CN 115848080A
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- vehicle body
- control device
- flight control
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 63
- 230000007246 mechanism Effects 0.000 claims description 16
- 230000035939 shock Effects 0.000 claims description 2
- 230000004083 survival effect Effects 0.000 abstract description 3
- 230000001681 protective effect Effects 0.000 description 4
- 230000002776 aggregation Effects 0.000 description 2
- 238000004220 aggregation Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- 229920005372 Plexiglas® Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000012780 transparent material Substances 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The application belongs to the field of aircraft design, and particularly relates to a manned airborne vehicle. The airborne vehicle comprises a passenger riding vehicle body (1), a flight power and flight control device (2) and a ground moving device (3); the personnel riding vehicle body (1) is a frame type carriage and is used for bearing personnel to be airborne, the top of the personnel riding vehicle body (1) is connected to the bottom of the flight power and flight control device (2), and the bottom of the personnel riding vehicle body (1) is provided with a ground moving device (3) for driving the personnel riding vehicle body (1) to move; the manned airborne assault task is executed through the flight power and flight control device (2), and after the personnel take the vehicle body (1) to land in an airborne manner, the connection between the personnel take the vehicle body (1) and the flight power and flight control device (2) is released, and the personnel take the vehicle body (1) to move on the ground through the ground moving device (3). The system can be used for high-altitude and long-distance air drop, and the survival rate and attendance efficiency of personnel are improved.
Description
Technical Field
The application belongs to the field of aircraft design, and particularly relates to a manned airborne vehicle.
Background
In the existing air-drop outburst, air-drop is generally carried out in an umbrella-drop mode, and air-drop personnel and equipment are respectively air-dropped or air-dropped from a conveyor.
At present, the flying height of a transporter is limited to be at middle and low altitude in an parachute landing mode, the flying range is limited to be close to a landing point, airborne personnel and equipment are slow in descending speed, the landing points are scattered, and the transporter is easy to damage and attack from the ground. The problems of scattered falling points, slow aggregation speed and the like are also easily caused by the separation of air-drop personnel and equipment and the air-drop or the air-drop.
Disclosure of Invention
In order to solve at least one of the technical problems, the application designs a manned air-borne vehicle which mainly comprises a passenger riding vehicle body, a flight power and flight control device and a ground moving device;
the personnel riding vehicle body is a frame type carriage and is used for bearing personnel to be airborne, the top of the personnel riding vehicle body is connected to the bottom of the flight power and flight control device, and the bottom of the personnel riding vehicle body is provided with a ground moving device for driving the personnel riding vehicle body to move;
tandem wings are respectively arranged on two sides of the flight power and flight control device, and ducted fans for providing flight power and attitude control are arranged at wing tips of the end parts of the tandem wings;
the manned airborne vehicle executes the manned airborne shock task through the flight power and flight control device connected with the top of the personnel riding vehicle body, and after the personnel riding vehicle body is airborne and landed, the connection between the personnel riding vehicle body and the flight power and flight control device is released, and the personnel riding vehicle body is driven by the ground moving device to move on the ground.
Preferably, the front part and the side part of the frame type carriage of the personnel riding vehicle body are provided with personnel protection armors for protecting the safe landing of airborne personnel.
Preferably, the passenger vehicle body is provided with a task load compartment for loading corresponding articles according to different task types.
Preferably, the top that personnel took the automobile body is provided with spacing locking mechanical system, flight power and flight control device bottom are provided with the slide rail, spacing locking mechanical system through embedding or roll-off slide rail realize personnel take the automobile body with flight power is connected with flight control device's dismantlement.
Preferably, the ground moving means comprises a chassis at the bottom of the vehicle body on which the person rides and four wheels.
Preferably, the tandem wings are foldable wings, the roots of the tandem wings are connected with an actuating mechanism, the actuating mechanism is driven by a driving motor to move and is used for switching the tandem wings between a folded state and an extended state, when the tandem wings are in the folded state, the axes of the tandem wings are parallel to the side edge lines of the flight power and flight control device, and when the tandem wings are in the extended state, the axes of the tandem wings are perpendicular to the side edge lines of the flight power and flight control device.
Preferably, the tandem wing is a retractable wing, the flight power and flight control device has an inner cavity for accommodating the tandem wing, the inner cavity is open at the flight power and flight control device, and the tandem wing can extend out from the open position of the inner cavity of the flight power and flight control device or retract into the inner cavity of the flight power and flight control device.
Preferably, at least two tandem wings are respectively arranged on two sides of the flight power and flight control device.
The application solves the problems that the existing parachute landing type assault suit has large limitation on the flying height of the conveyor, the descending speed is low, the falling points are dispersed, the conveyor is easy to be damaged and attacked on the ground, the falling points are dispersed, the aggregation speed is low and the like.
The system can be used for high-altitude and long-distance air drop, and the survival rate and attendance efficiency of personnel are improved.
Drawings
FIG. 1 is a schematic overall configuration of a preferred embodiment of the passenger aerial vehicle of the present application.
Figure 2 is a side view of another preferred embodiment of the people-carrying airborne vehicle of the present application.
FIG. 3 is a schematic illustration of the tandem wing deployment of an airborne vehicle in accordance with a preferred embodiment of the present application.
The system comprises a vehicle body for passengers to ride 1, a flight power and flight control device 2, a ground moving device 3, a protective armor for passengers 4, a task load cabin 5, a limit locking mechanism 6, a sliding rail 7, an actuating mechanism 8, a driving motor 9, tandem wings 10 and a ducted fan 11.
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 accompanying 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 implementations that are part of this application and not all implementations. 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 obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application. Embodiments of the present application will be described in detail below with reference to the drawings.
The application provides a manned airborne vehicle, which mainly comprises a passenger riding vehicle body 1, a flight power and flight control device 2 and a ground moving device 3 as shown in figures 1 to 3;
the personnel riding vehicle body 1 is a frame type carriage and is used for bearing personnel to be airborne, the top of the personnel riding vehicle body 1 is connected to the bottom of the flight power and flight control device 2, and the bottom of the personnel riding vehicle body 1 is provided with a ground moving device 3 for driving the personnel riding vehicle body 1 to move;
the manned airborne vehicle executes the manned airborne assault task through the flight power and the flight control device 2 connected with the top of the personnel riding vehicle body 1, and releases the connection between the personnel riding vehicle body 1 and the flight power and the flight control device 2 after the personnel riding vehicle body 1 is airborne and landed, and drives the personnel riding vehicle body 1 to move on the ground through the ground moving device 3.
The application provides a manned airborne vehicle is a modular, can manned from the cargo airplane airborne, and carry out the equipment of controllable flight and ground removal, through taking personnel automobile body 1 and flight power and flight control device 2 to open and dismantle and be connected, realize the modularized design, carry people airborne assault task through flight power and flight control device 2 with personnel take automobile body 1 top connection, and after personnel take automobile body 1 airborne landing, remove personnel and take automobile body 1 and flight power and flight control device 2 to be connected, and drive personnel through ground mobile device 3 and take automobile body 1 and move on the ground. This application can be at the high altitude, keep away from the conveyer that the placement position left, possesses aerial controllable flight and ground removal ability, possesses module dismantlement and nimble load capacity, can realize personnel and the integrative airborne of equipment, has advantages such as quick, accurate, light removal.
The flight power and flight control device 2 provides flight power and attitude control through the ducted fan 11 on the flight power and flight control device, and is controlled by a conventional flight control system, and the flight control system can be further connected with a cockpit control console of a vehicle body 1 through modes such as wireless transmission and Bluetooth transmission, so that a driver can lift and control the flight power and flight control device 2.
In some alternative embodiments, the front and sides of the framed compartment of the personnel ride vehicle 1 are provided with personnel protective armor 4 for protecting airborne personnel from safe landing. The protective armor 4 may be made of a transparent material such as plexiglass.
In some alternative embodiments, the personnel ride the vehicle body 1 and are provided with task load compartments 5 for loading corresponding articles according to different task types. Referring to fig. 1, a mission load chamber 5 is generally provided at the rear of the vehicle body 1 on which a person who faces away from the cockpit rides, and the mission load chamber 5 is a box structure for loading respective load items, such as one or more of weapons, ammunition, medical equipment, information relay equipment, etc., according to different mission types.
This application personnel take automobile body 1 with flight power and flight control device 2 are modular detachable connecting device, for this reason, can realize connecting through devices such as hasp to convenient to install or dismantle, in some optional embodiments, the top that personnel took automobile body 1 is provided with spacing locking mechanical system 6, flight power is provided with slide rail 7 with flight control device 2 bottoms, spacing locking mechanical system 6 through embedding or roll-off slide rail 7 realize personnel take automobile body 1 with flight power is connected with the dismantlement of flight control device 2. In this embodiment, the limit locking mechanism 6 is embedded in the slide rail 7 of the flight power and flight control device 2, so that the flight power and flight control device 2 can be locked, when the limit locking mechanism 6 is pulled out of the slide rail 7, the freedom of movement of the slide rail 7 is released, and the flight power and flight control device 2 can drive the slide rail 7 to be separated from the passenger vehicle body 1, for example, the flight power and flight control device 2 flies back into the transport vehicle again to drive other passengers to land on the passenger vehicle body 1.
In some alternative embodiments, the ground moving device 3 comprises a chassis and four wheels located at the bottom of the passenger car body 1. In this embodiment, the ground moving device 3 is a conventional moving mechanism, such as a moving mechanism represented by an engine, a chassis and wheels, and a chain moving mechanism may be used in an alternative embodiment.
In some optional embodiments, the tandem wing 10 is a foldable wing, the root of the tandem wing 10 is connected with an actuating mechanism 8, the actuating mechanism 8 is driven by a driving motor 9 to move, so as to switch the tandem wing 10 between a folded state and an extended state, when the tandem wing 10 is in the folded state, the axis of the tandem wing 10 is parallel to the side edge line of the flight power and flight control device 2, and when the tandem wing 10 is in the extended state, the axis of the tandem wing 10 is perpendicular to the side edge line of the flight power and flight control device 2.
Fig. 2 and 3 show the tandem wing 10 in this embodiment in a folded state and an extended state, respectively. In this application, moving mechanism 8 can be the gear train carousel, drives the gear train carousel through driving motor 9 and rotates, and then drive tandem wing 10 rotates, realizes the folding and the extension of tandem wing 10. In an alternative embodiment, the actuator 8 may be a ram, which is fixed on the side of the flight power and flight control device 2, and then its output shaft is hinged to the tandem wing 10 near the end, and the root of the tandem wing 10 is hinged to the side of the flight power and flight control device 2, that is, the folding and extending of the tandem wing 10 can be realized by the retraction of the ram.
In some alternative embodiments, the tandem wing 10 may also be a retractable wing, and the flight power and flight control device 2 has an inner cavity for accommodating the tandem wing 10, the inner cavity is open at the flight power and flight control device 2, and the tandem wing 10 can be extended from the open of the inner cavity of the flight power and flight control device 2 or retracted into the inner cavity of the flight power and flight control device 2.
In some alternative embodiments, at least two tandem wings 10 are provided on each side of the flight power and flight control device 2. In the embodiment shown in fig. 2 and 3, two tandem wings 10 are respectively disposed on two sides of the flight power and flight control device 2, and as shown in fig. 2, when the two tandem wings 10 need to be disposed long enough, the two tandem wings can be designed to be stacked up and down in a folded state.
The drawback of current parachuting drop point dispersion has been solved in this application. The modular structure of the equipment can improve the assembly and disassembly efficiency of the manned airborne vehicle, and the power module can be disassembled after landing so as to be light and fast put into combat; the device can carry different types of task loads, select different types of protective armors and enhance the flexibility of equipment load. The manned airborne vehicle has the advantages that the flight power and the flight attitude can be independently controlled, the vehicle can be airborne from a higher altitude, the vehicle can be airborne from a region far away from a battlefield, the vehicle can rapidly descend, the landing point precision can be improved, the safety of people and equipment is guaranteed, the damage probability of the people and the equipment is effectively reduced, and the assaulting performance and the concealing performance of airborne assaulting are improved. In the equipment, the tandem type wings have high pneumatic efficiency, and the posture of the ducted fan is accurately controlled; in addition, the conveyer carries out high-altitude and long-distance air drop, which is beneficial to improving the survival rate and the attendance efficiency.
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.
Claims (8)
1. A manned airborne vehicle is characterized by comprising a vehicle body (1) for riding personnel, a flight power and flight control device (2) and a ground moving device (3);
the personnel riding vehicle body (1) is a frame type carriage and is used for bearing personnel to be airborne, the top of the personnel riding vehicle body (1) is connected to the bottom of the flight power and flight control device (2), and the bottom of the personnel riding vehicle body (1) is provided with a ground moving device (3) which is used for driving the personnel riding vehicle body (1) to move;
tandem wings (10) are respectively arranged on two sides of the flight power and flight control device (2), and ducted fans (11) for providing flight power and attitude control are arranged at the wing tips of the end parts of the tandem wings (10);
the manned airborne vehicle executes the manned airborne shock task through the flight power and the flight control device (2) connected with the top of the personnel riding vehicle body (1), and releases the connection between the personnel riding vehicle body (1) and the flight power and the flight control device (2) after the personnel riding vehicle body (1) is airborne and landed, and drives the personnel riding vehicle body (1) to move on the ground through the ground moving device (3).
2. Manned airborne vehicle according to claim 1, characterized in that the front and sides of the frame-like compartment of the passenger vehicle body (1) are provided with personnel protection armour (4) for protecting the airborne personnel from safe landing.
3. The people mover according to claim 1, characterized in that task load compartments (5) are provided in the passenger body (1) for loading corresponding items according to different task types.
4. The manned airborne vehicle of claim 1, characterized in that a limit locking mechanism (6) is arranged at the top of the passenger vehicle body (1), a slide rail (7) is arranged at the bottom of the flight power and flight control device (2), and the limit locking mechanism (6) realizes the detachable connection of the passenger vehicle body (1) and the flight power and flight control device (2) by embedding or sliding out the slide rail (7).
5. A passenger airborne vehicle according to claim 1, characterized in that the ground moving means (3) comprises a chassis at the bottom of the passenger ride body (1) and four wheels.
6. The manned airborne vehicle of claim 1, wherein the tandem wing (10) is a foldable wing, the actuation mechanism (8) is connected to the root of the tandem wing (10), the actuation mechanism (8) is driven by a drive motor (9) for switching the tandem wing (10) between a folded state and an extended state, the axis of the tandem wing (10) is parallel to the side edge line of the flight power and flight control device (2) when the tandem wing (10) is in the folded state, and the axis of the tandem wing (10) is perpendicular to the side edge line of the flight power and flight control device (2) when the tandem wing (10) is in the extended state.
7. The passenger airborne vehicle of claim 1, wherein the tandem wing (10) is a retractable wing, and the flight power and flight control apparatus (2) has an interior cavity for receiving the tandem wing (10), the interior cavity being open at the flight power and flight control apparatus (2), the tandem wing (10) being capable of extending from the interior cavity opening of the flight power and flight control apparatus (2) or being retracted into the interior cavity of the flight power and flight control apparatus (2).
8. Manned airborne vehicle according to claim 1, characterized in that the flight power and flight control means (2) are provided with at least two tandem wings (10) on each side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310187059.5A CN115848080A (en) | 2023-03-02 | 2023-03-02 | Manned airborne vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310187059.5A CN115848080A (en) | 2023-03-02 | 2023-03-02 | Manned airborne vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115848080A true CN115848080A (en) | 2023-03-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310187059.5A Pending CN115848080A (en) | 2023-03-02 | 2023-03-02 | Manned airborne vehicle |
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| Country | Link |
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| CN (1) | CN115848080A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030164426A1 (en) * | 2002-03-01 | 2003-09-04 | Edward Strong | Guided airborne vehicle, cargo and personnel delivery system |
| CN1663883A (en) * | 2004-03-02 | 2005-09-07 | 张宝霖 | Air-landing device and weight air-dropping device for manned military equipment |
| CN104661903A (en) * | 2012-09-20 | 2015-05-27 | 北极星工业有限公司 | Utility vehicle |
| CN109406159A (en) * | 2018-05-23 | 2019-03-01 | 苏州博之盾防护技术有限公司 | A kind of airborne vehicle air-drop simulator of load person |
| CN114212237A (en) * | 2021-12-23 | 2022-03-22 | 中国航空工业集团公司西安飞机设计研究所 | Accurate air-drop/airborne power device |
-
2023
- 2023-03-02 CN CN202310187059.5A patent/CN115848080A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030164426A1 (en) * | 2002-03-01 | 2003-09-04 | Edward Strong | Guided airborne vehicle, cargo and personnel delivery system |
| CN1663883A (en) * | 2004-03-02 | 2005-09-07 | 张宝霖 | Air-landing device and weight air-dropping device for manned military equipment |
| CN104661903A (en) * | 2012-09-20 | 2015-05-27 | 北极星工业有限公司 | Utility vehicle |
| CN109406159A (en) * | 2018-05-23 | 2019-03-01 | 苏州博之盾防护技术有限公司 | A kind of airborne vehicle air-drop simulator of load person |
| CN114212237A (en) * | 2021-12-23 | 2022-03-22 | 中国航空工业集团公司西安飞机设计研究所 | Accurate air-drop/airborne power device |
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Application publication date: 20230328 |