CN104029792A - Aircraft acquirer - Google Patents

Aircraft acquirer Download PDF

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Publication number
CN104029792A
CN104029792A CN201410265527.7A CN201410265527A CN104029792A CN 104029792 A CN104029792 A CN 104029792A CN 201410265527 A CN201410265527 A CN 201410265527A CN 104029792 A CN104029792 A CN 104029792A
Authority
CN
China
Prior art keywords
aircraft
grabber
rotary
bamboo shoot
revolution
Prior art date
Application number
CN201410265527.7A
Other languages
Chinese (zh)
Inventor
王力
叶华林
Original Assignee
天津汉海环保设备有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 天津汉海环保设备有限公司 filed Critical 天津汉海环保设备有限公司
Priority to CN201410265527.7A priority Critical patent/CN104029792A/en
Publication of CN104029792A publication Critical patent/CN104029792A/en

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Abstract

The invention relates to an aircraft acquirer. The aircraft acquirer comprises an acquirer main body, wherein an acquisition releasing mechanism which is in collision contact with an acquisition head at the front end of an aircraft so as to acquire the acquisition head is arranged in the acquirer main body; the acquisition mechanism comprises rotary hooks, and one-way rotary convex bamboo shoots which are movably connected with the rotary hooks, wherein the other ends of the one-way rotary convex bamboo shoots are connected with rotary elements. According to the aircraft acquirer disclosed by the invention, the acquisition mechanism which is in collision contact with the acquisition head at the front end of the aircraft so as to acquire the acquisition head is arranged in the acquirer main body, the acquisition mechanism comprises the rotary hooks, and the one-way rotary convex bamboo shoots which are movably connected with the rotary hooks, wherein the other ends of the one-way rotary convex bamboo shoots are connected with the rotary elements, the acquisition head at the front end of the aircraft can be in collision contact with the rotary hooks, and the acquisition head and the rotary hooks can be jointed together, so that the effective acquisition for the aircraft is realized.

Description

A kind of aircraft grabber
Technical field
The invention belongs to water surface unmanned vehicles and catch release tech field, be specifically related to a kind of aircraft grabber.
Background technology
Water surface unmanned vehicles comprises unmanned boat USV, autonomous underwater vehicle UUV, water surface landing unmanned plane etc.In order to expand the operating range of above-mentioned water surface unmanned vehicles, water surface unmanned vehicles can be carried on a platform, as naval vessel, by being carried at naval vessel lash ship by water surface unmanned vehicles, at preposition, lay and reclaim water surface unmanned vehicles, thereby just expand the operating range of above-mentioned water surface unmanned vehicles, but realize above-mentioned purpose, need to design a set of aircraft acquisition equipment, to realize by automatically water surface unmanned vehicles being caught to recovery at naval vessel lash ship, and can automatically carry out cloth and be put on the water surface.
Summary of the invention
Because in this, the object of the present invention is to provide a kind of aircraft grabber, it can reclaim to realize at needs to water surface unmanned vehicles fast catch recovery, and can when needing cloth to be put on the water surface, can discharge quickly the aircraft cloth of catching and be put on the water surface.
For achieving the above object, the present invention adopts following technical scheme:
A kind of aircraft grabber, comprise grabber body, in described grabber body, be provided with and catch head collision contact to catch the releasing mechanism of catching of head described in catching for aircraft front end, described capture mechanism comprises revolution hook, the protruding bamboo shoot of unidirectional rotary that are flexibly connected with described revolution hook, the other end connection revolving meber of the protruding bamboo shoot of described unidirectional rotary.
Between the protruding bamboo shoot of described unidirectional rotary and described revolution hook, by center of gyration part, revolution hook spring is installed.
Described revolving meber comprises a V-arrangement spring, and described V-arrangement spring fitting is on the protruding bamboo shoot center of gyration of unidirectional rotary part.
Between described revolution hook and the protruding bamboo shoot of described unidirectional rotary, be connected through the hinge.
The rear end of described grabber body is provided with coupling link.
Aircraft grabber of the present invention, by being provided with, for aircraft front end, catch head collision contact to catch the capture mechanism of head described in catching in grabber body, described capture mechanism comprises revolution hook, the protruding bamboo shoot of unidirectional rotary that are flexibly connected with described revolution hook, the other end of the protruding bamboo shoot of described unidirectional rotary connects revolving meber, can be by the catching head collision contact Rotating hook of aircraft front end together with engaging with described revolution hook, thus realized effectively catching aircraft.
Accompanying drawing explanation
Figure 1 shows that the schematic diagram of a kind of aircraft grabber that the embodiment of the present invention provides.
The specific embodiment
Below, in conjunction with example, substantive distinguishing features of the present invention and advantage are further described, but the present invention is not limited to listed embodiment.
Refer to shown in Fig. 1, a kind of aircraft grabber, comprise grabber body 1, in described grabber body 1, be provided with and catch 3 collision contacts to catch 3 the releasing mechanism of catching described in catching for aircraft 2 front ends, described capture mechanism comprises revolution hook 4, links up with the protruding bamboo shoot 6 of 4 unidirectional rotary being flexibly connected with described revolution, and the other end of the protruding bamboo shoot 6 of described unidirectional rotary connects revolving meber 7.
4 of the protruding bamboo shoot 6 of described unidirectional rotary and described revolution hooks are provided with revolution hook spring 5 by center of gyration part.By being provided with revolution hook spring 5, can make the protruding bamboo shoot 6 of unidirectional rotary and described revolution hook 4 keep a position.Center of gyration part makes revolution hook and the relative revolution of turning round between protruding bamboo shoot.
When unmanned water surface aircraft and revolution hook are collided, under the effect of certain impact force, the rotate to an angle unmanned vehicles that is opened of revolution hook enters in hook and is tangled.While laying, the protruding bamboo shoot of unidirectional rotary and outside sear bump against positive opening revolution hook, and unmanned vehicles is released.
Described revolving meber 7 comprises a V-arrangement spring, and described V-arrangement spring fitting is on the protruding bamboo shoot center of gyration of unidirectional rotary part.The Main Function of revolving meber 7 is to guarantee that the protruding bamboo shoot of unidirectional rotary and revolution hook are opened when unmanned vehicles lays, and the protruding bamboo shoot of unidirectional rotary and revolution hook are not opened in removal process.
Described revolution hook 4 and 6, the protruding bamboo shoot of described unidirectional rotary are connected through the hinge.
The rear end of described grabber body is provided with coupling link 8, can be used for connecting traction winch or the draw gear of the described aircraft grabber motion of traction.
Aircraft grabber of the present invention can be installed in aircraft withdrawer, the hauling rope that connects traction winch by coupling link 8, by this traction winch, draw this aircraft grabber, in the slideway of aircraft withdrawer, do back and forth movement, the unmanned boat of the water surface, water land-effect plane etc. are caught by the revolution hook 4 of self, in order to realize after catching the aircraft that can automatically discharge this and catch, can in aircraft withdrawer, be provided with corresponding unhook sear, match with the protruding bamboo shoot 6 of described unidirectional rotary.
Catch and into, navigation unit by water front end, catch head and contact with the collision of revolution hook, enter in revolution hook, become one with turning round to link up with.Aircraft grabber enters in the slideway of aircraft withdrawer aircraft by the traction of winch.While drawing to withdrawer bow point, aircraft and withdrawer are combined as a whole.
During release, after time aircraft receipts device is steady with wave motion, control the inner winch of aircraft withdrawer, the capture mechanism of aircraft withdrawer inside starts along the sear that slides to the setting of withdrawer inside under track beneficial.By sear, contact, by sear, opened the revolution of aircraft capture mechanism and link up with.After revolution hook discharges, aircraft enters by reclaiming Lu's slideway the release that has realized aircraft on sea.
Aircraft grabber of the present invention, by being provided with, for aircraft front end, catch head collision contact to catch the capture mechanism of head described in catching in grabber body, described capture mechanism comprises revolution hook, the protruding bamboo shoot of unidirectional rotary that are flexibly connected with described revolution hook, the other end of the protruding bamboo shoot of described unidirectional rotary connects revolving meber, can be by the catching head collision contact Rotating hook of aircraft front end together with engaging with described revolution hook, thus realized effectively catching aircraft.
The above is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the premise without departing from the principles of the invention; can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.

Claims (5)

1. an aircraft grabber, it is characterized in that, comprise grabber body, in described grabber body, be provided with and catch head collision contact to catch the capture mechanism of head described in catching for aircraft front end, described capture mechanism comprises revolution hook, the protruding bamboo shoot of unidirectional rotary that are flexibly connected with described revolution hook, the other end connection revolving meber of the protruding bamboo shoot of described unidirectional rotary.
2. aircraft grabber as claimed in claim 1, is characterized in that, between the protruding bamboo shoot of described unidirectional rotary and described revolution hook, by center of gyration part, revolution hook spring is installed.
3. aircraft grabber as claimed in claim 2, is characterized in that, described revolving meber comprises a V-arrangement spring, and described V-arrangement spring fitting is on the protruding bamboo shoot center of gyration of unidirectional rotary part.
4. aircraft grabber as claimed in claim 3, is characterized in that, between described revolution hook and the protruding bamboo shoot of described unidirectional rotary, is connected through the hinge.
5. aircraft grabber as described in claim 1~4 any one, is characterized in that, the rear end of described grabber body is provided with coupling link.
CN201410265527.7A 2014-06-13 2014-06-13 Aircraft acquirer CN104029792A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410265527.7A CN104029792A (en) 2014-06-13 2014-06-13 Aircraft acquirer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410265527.7A CN104029792A (en) 2014-06-13 2014-06-13 Aircraft acquirer

Publications (1)

Publication Number Publication Date
CN104029792A true CN104029792A (en) 2014-09-10

Family

ID=51460846

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410265527.7A CN104029792A (en) 2014-06-13 2014-06-13 Aircraft acquirer

Country Status (1)

Country Link
CN (1) CN104029792A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1017263A (en) * 1996-07-02 1998-01-20 Kayaba Ind Co Ltd Boat suspension device
CN101077726A (en) * 2006-05-26 2007-11-28 中国科学院沈阳自动化研究所 Wter surface automatic buttjunction interlockingapparatus
CA2658975A1 (en) * 2006-07-26 2008-01-31 Ifremer-Institut Francais De Recherche Pour L'exploitation De La Mer Apparatus for recovering a surface marine vehicle or an underwater vehicle
CN101804855A (en) * 2010-03-30 2010-08-18 中国船舶重工集团公司第七〇二研究所 Underwater guide capture device of remote-operated vehicle
CN102358434A (en) * 2011-09-15 2012-02-22 中国科学院自动化研究所 Recycling system for aquatic unmanned aerial vehicle
CN203996799U (en) * 2014-06-13 2014-12-10 天津汉海环保设备有限公司 A kind of aircraft grabber

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1017263A (en) * 1996-07-02 1998-01-20 Kayaba Ind Co Ltd Boat suspension device
CN101077726A (en) * 2006-05-26 2007-11-28 中国科学院沈阳自动化研究所 Wter surface automatic buttjunction interlockingapparatus
CA2658975A1 (en) * 2006-07-26 2008-01-31 Ifremer-Institut Francais De Recherche Pour L'exploitation De La Mer Apparatus for recovering a surface marine vehicle or an underwater vehicle
CN101804855A (en) * 2010-03-30 2010-08-18 中国船舶重工集团公司第七〇二研究所 Underwater guide capture device of remote-operated vehicle
CN102358434A (en) * 2011-09-15 2012-02-22 中国科学院自动化研究所 Recycling system for aquatic unmanned aerial vehicle
CN203996799U (en) * 2014-06-13 2014-12-10 天津汉海环保设备有限公司 A kind of aircraft grabber

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Application publication date: 20140910

RJ01 Rejection of invention patent application after publication