Aerial externally hung target drone nacelle
A target and aviation technology, applied in the direction of target, movable target, attack equipment, etc., can solve the problem of high breakage rate of target cable
Active Publication Date: 2017-05-31
河北环航科技股份有限公司
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Problems solved by technology
[0004] However, the inventors of the present application found that in the prior art, the retracting and unwinding of the target cable is usually performed manually, and due to the unavoidable uncertainty in the manual operation, the breakage rate of the target cable is relatively high
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[0030] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0031] An embodiment of the present invention provides an aviation external nacelle, the aviation external nacelle is suspended on an aircraft for suspending and dragging a target, such as figure 1 and image 3 As shown, a control module is installed on the aircraft, and a target setting button and a target receiving button are arranged in the cockpit of the aircraft, and the aviation external nacelle includes a target cabin. Wherein, from the no...
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The invention discloses an aerial externally hung target drone nacelle, and relates to the technical field of target drone hanging. The aerial externally hung target drone nacelle is used for reducing the break rate of a target cable. The aerial externally hung target drone nacelle comprises a target cabin, wherein a turbine, an air door mechanism, an air door motor, a reduction gearbox and a winding drum are successively arranged in the target cabin; the air door motor is connected with the air door mechanism; a first rotating shaft is arranged between the turbine and the reduction gearbox; the turbine sleeves one end of the first rotating shaft; the other end of the first rotating shaft is connected with a high-speed shaft of the reduction gearbox; a second rotating shaft is arranged between the winding drum and the air door motor; the winding drum sleeves the second rotating shaft; one end of the second rotating shaft is connected with a low-speed shaft of the reduction gearbox; a self-locking mechanism which is used for locking a target drone is arranged at the bottom of the target cabin; a target cable is further arranged in the target cabin; one end of the target cable is wound on the winding drum while the other end of the target cable extends out of the target cabin and is connected with the target drone; and a target cable retracting and releasing speed sensor is further mounted on the target cable in the target cabin. The aerial externally hung target drone nacelle is used for hanging and dragging the target drone.
Description
technical field [0001] The invention relates to the technical field of target suspension, in particular to an aerial external target nacelle. Background technique [0002] The aerial target nacelle is a device installed on the aircraft for hanging and towing the target. It is usually equipped with a winch and a target cable. One end of the target cable is wound on the winch, and the other end is connected to the target. [0003] When shooting a target, the winch releases the target through the target cable, and after the target is shot, the winch recovers the target through the target cable. Because this process is carried out in the state of high-speed flight of the aircraft, the target cable bears a large dynamic load. If the dynamic load is too large, the target cable will break. [0004] However, the inventors of the present application have found that in the prior art, retracting and unwinding of the target cable is usually performed manually, and some uncertainties in...
Claims
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IPC IPC(8): F41J9/10
CPCF41J9/10
Inventor 常铁铮王玉镇池震宇乔晓辉杨富
Owner 河北环航科技股份有限公司