CN104691769A - Novel unmanned aerial vehicle airborne pod hanging frame - Google Patents
Novel unmanned aerial vehicle airborne pod hanging frame Download PDFInfo
- Publication number
- CN104691769A CN104691769A CN201510117529.6A CN201510117529A CN104691769A CN 104691769 A CN104691769 A CN 104691769A CN 201510117529 A CN201510117529 A CN 201510117529A CN 104691769 A CN104691769 A CN 104691769A
- Authority
- CN
- China
- Prior art keywords
- hanger
- hook
- gondola
- rocking arm
- aerial vehicle
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
Landscapes
- Forklifts And Lifting Vehicles (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention provides an unmanned aerial vehicle airborne pod hanging frame. The unmanned aerial vehicle airborne pod hanging frame comprises an outer hanging frame fixed to the bottom wing surface of a wing, an inner hanging frame with a cavity, a front lifting and pulling bolt and a rear lifting and pulling bolt which are arranged in the cavity of the inner hanging frame, a front hook connected to the lower end of the front lifting and pulling bolt, a rear hook connected to the lower end of the rear lifting and pulling bolt, a front transmission mechanism connected to the front hook and the inner hanging frame, a rear transmission mechanism connected to the rear hook and the outer hanging frame, a balance connecting rod connecting the front transmission mechanism and the rear transmission mechanism, and a locking mechanism preventing the front transmission mechanism from moving. The unmanned aerial vehicle airborne pod hanging frame can complete the locking of a task pod by applying less torque to the side of the task pod in a task pod installation process so as to quickly and accurately fix a hanging object to the bottom of the wing of an unmanned aerial vehicle, thereby facilitating operations for persons.
Description
Technical field
The present invention relates to field of aviation machinery, particularly a kind of unmanned aerial vehicle onboard gondola hanger.
Background technology
At present, unmanned plane has been widely used in the numerous areas such as tactics investigation, target positioning, target Damage assessment, electronic countermeasure, communication repeating.The large-scale unmanned plane of, boat duration far away for voyage, below unmanned plane of being everlasting, symmetrical additional fuel tank of carrying additionally is to increase voyage to greatest extent.For delivery type unmanned plane, need square installation function gondola under the wings of an airplane.The task device of these heavy lifts needs to adopt firm connection mode, to prevent standby the generation in launch and flight process of task from rocking, thus produces serious disturbance to unmanned plane normal flight.
In prior art, how with bolts the connection mode of the heavy lift equipment such as unmanned plane personage gondola and wing is, be connected with suspension with the mode of tie bolt as relate to a kind of suspension ring that adopt in patent CN203048392U, but quickly retracting function can not be realized during suspension installation or removal.Patent CN102442435B proposes a kind ofly has the aviation gondola hanger packing up guide function, and this hanger is a tower structure, has guide function.Although have the existing techniques in realizing connection of unmanned plane wing and gondola, but still there is following problem in prior art: (1) bolt connects and frame-type is connected in task gondola folding and unfolding process and can not locates with installation by quick-detachment, this connection mode is usually when daily workout and pop-up mission, can not respond fast, substantially prolongs unmanned plane setup time, thus bungle the chance of winning a battle; (2) more personnel are usually needed to coordinate when installing or removing, equal existing defects or inconvenience in personnel, setup time and method of operation.
Summary of the invention
In order to overcome prior art Problems existing, the invention provides a kind of hanger that can realize Fast Installation and the airborne task gondola function of dismounting.
A kind of novel unmanned aerial vehicle onboard gondola hanger, comprise: be arranged to the pylon being fixed on wing, be provided with cavity and rear and front end, bottom surface is provided with for before gondola, rear hanger stretches into the interior hanger of the mounting groove of cavity, to stretch in interior hanger cavity and the front lift bolt of axial motion and load and rear lift bolt are provided, the front hook be connected with front lift bolt lower end, the aft hook be connected with rear lift bolt lower end, be arranged to the front transmission mechanism connecting front hook and interior hanger, be arranged to the rear transmission device connecting front hook and interior hanger, be arranged to the balanced connecting rod connecting front transmission mechanism and rear transmission device, be arranged to the lockout mechanism stoping front transmission mechanism motion.Described front transmission mechanism orders about front hook and to lock with hanger before gondola to rotate for the center of circle with front lift bolt junction or be separated, and described rear transmission device orders about aft hook and to lock with hanger after gondola to rotate for the center of circle with rear lift bolt junction or be separated.
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, described front transmission mechanism comprises: the first front rod of front end and front hook pinned connection, second front rod of front end and the first front rod rear end pinned connection, be arranged to the front arm of hanger inwall and the first front rod, the second front rod junction bearing pin in connecting, the first central rotating shaft be set and be provided with the locking rocking arm to the first rocking arm of three directions extensions, the second rocking arm and arc lock hook centered by the first central rotating shaft.Described central rotating shaft and interior hanger inwall are by the 6th pinned connection, the first rocking arm and the second front rod rear end pinned connection.
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, described rear transmission device comprises: the first rear linking rod of rear end and aft hook pinned connection, second rear linking rod of rear end and the first rear linking rod rear end pinned connection, be arranged to the rear arm of hanger inwall and the first rear linking rod, the second rear linking rod junction bearing pin in connecting, the second central rotating shaft be set and be provided with centered by the second central rotating shaft to the 3rd rocking arm of both direction extension and the rocking arm of unblanking of the 4th rocking arm.Described second central rotating shaft and interior hanger inwall pass through the 9th pinned connection, the 4th rocking arm and the second rear linking rod front end pinned connection;
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, described balanced connecting rod one end and the second rocking arm pinned connection, the other end and the 3rd rocking arm pinned connection.
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, before described, lift bolt stretches into the cavity of hanger by the front lining being positioned at hanger and front end is connected with front hook, the front lift bolt outer wall being positioned at hanger outside is provided with Acme thread, and front hexagonal nut thread is connected to and is positioned on the front lift bolt of hanger outside.
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, described rear lift bolt stretches into the cavity of hanger by the back bush being positioned at hanger and front end is connected with aft hook, the rear lift bolt outer wall being positioned at hanger outside is provided with Acme thread, and rear hexagonal nut is threadedly connected to and is positioned on the rear lift bolt of hanger outside.
According to the unmanned aerial vehicle onboard gondola hanger of the above-mentioned proposition of the present invention, described blocking device comprises: the lock hole and the open keyhole that are positioned at pylon side, 6th bearing pin is provided with in the face of the bottom surface of interior hanger inwall the first locked groove mated with obturator hernia, be positioned at hanger cavity and front end is provided with hook formation, middle part is connected with the cavity wall of interior hanger by the 8th bearing pin, the latch hook that afterbody is connected with the cavity wall of interior hanger by extension spring, described hook formation and arc lock hook match, described 8th bearing pin is provided with in the face of the bottom surface of interior hanger inwall the second locked groove mated with open keyhole.
As a modification of the present invention, unmanned aerial vehicle onboard gondola hanger also comprises safety device, comprising: the safe lockhole being arranged at pylon side, is arranged at interior hanger and the safe pin-and-hole mated with safe lockhole, and safety pin; When hook formation and arc lock hook are locked, safety pin is against latch hook lower end through safe lockhole and safe pin-and-hole, prevents latch hook from rotating.
The present invention compared with prior art, have the following advantages: task gondola is in installation process, apply less moment of torsion to task gondola side just can to finish the work the locking of gondola, thus fast and accurately suspension is fixed on below unmanned plane wing, convenient operation human users.
Below in conjunction with Figure of description, the present invention is described further.
Accompanying drawing explanation
Fig. 1 is the structural representation that the present invention connects wing and task gondola;
Fig. 2 is the pylon structural representation that the present invention is furnished with forward and backward fairing;
Fig. 3 is pylon structural representation of the present invention;
Fig. 4 is pylon of the present invention and interior hanger assembling schematic diagram;
Fig. 5 is structural representation in hanger inner chamber in the present invention;
Fig. 6 is the partial enlarged drawing (with balanced connecting rod) of A in Fig. 5;
Fig. 7 is the partial enlarged drawing (without balanced connecting rod) of A in Fig. 5;
Fig. 8 is locking rocker structure schematic diagram of the present invention;
Fig. 9 is latch hook structure schematic diagram of the present invention;
Figure 10 is that the present invention lifts bolt arrangement schematic diagram.
Detailed description of the invention
Composition graphs 1, a kind of novel unmanned aerial vehicle onboard gondola hanger 2, is arranged to and connects wing 1 and task gondola 3, and it is connected with wing 1 bolt with hanging point after wing 5 by hanging point 4 before wing.
Unmanned aerial vehicle onboard gondola hanger 2 comprises pylon 7 and interior hanger 9.
Composition graphs 2 and Fig. 3, pylon 7 adopts mechanical processing technique to be formed by metallic material, and its rear and front end is provided with front fairing 6 and rear fairing 8, and front fairing 6 and rear fairing 8 are fixed on pylon 7 by screw.Pylon 9 one middle side part is provided with lock hole 11, safe lockhole 12 and open keyhole 13 near bottom surface.
Composition graphs 4, interior hanger 9 housing is fixed in the housing of pylon 7 by 4 locating dowel pins of four focuses.Interior hanger 9 is provided with cavity and rear and front end, bottom surface is provided with the opening of inserting cavity for the forward and backward hanger of gondola 3.On front side of the front opening of interior hanger 9 bottom surface and rear side be respectively equipped with before only pendulum device 10 and rear only pendulum device 14, before described, only pendulum device 10 and rear only pendulum device 14 include tangent with gondola 3 profile and are connected to become lambdoid two blocks.
Following mechanism is provided with in the cavity of interior hanger 9:
(1) to insert in interior hanger 9 cavity and the front lift bolt 15 of axial motion and load and rear lift bolt 23 are provided;
(2) front hook 24 be connected with front lift bolt 15 lower end;
(3) aft hook 36 be connected with rear lift bolt 23 lower end;
(4) be arranged to the front transmission mechanism connecting front hook 24 and interior hanger 9, and front transmission mechanism orders about front hook 24 locks to rotate for the center of circle with front lift bolt 15 junction with hanger before gondola 3 or be separated;
(5) be arranged to the rear transmission device connecting front hook 36 and interior hanger 9, and rear transmission device order about aft hook 36 with rear lift bolt 23 junction for the center of circle rotates with gondola 3 afterwards hanger lock or be separated;
(6) balanced connecting rod 17 connecting front transmission mechanism and rear transmission device is arranged to;
(7) blocking device stoping front transmission mechanism motion is arranged to.
In conjunction with Figure 10, described front lift bolt 15 is identical with rear lift bolt 23 structure, and lower end has ears, afterbody outer wall is provided with outside thread, and described ears are provided with through hole, and hexagonal nut is threadedly connected to afterbody outer wall and is provided with on outside thread.Before described, lift bolt 15 stretches into the cavity of hanger 9 by the front lining 16 being positioned at hanger 9, and rear lift bolt 23 stretches into the cavity of hanger 9 by the back bush 38 being positioned at hanger 9.Cause task gondola 3 and gondola hanger to depart to prevent lift bolt and hexagonal nut from loosening, the screw thread of the two junction adopts Acme thread.
Composition graphs 5, the upper end of front hook 24 is provided with through hole, just has the mode of bolt to be connected with the through hole on front lift bolt 15 ears; The upper end of aft hook 36 is provided with through hole, just has the mode of bolt to be connected with the through hole on rear lift bolt 23 ears.The direction extension that device 10 is only put forward in front hook 24 lower end is provided with hook formation, can lock with hanger before the task gondola of inserting in interior hanger 9 cavity or be separated; The direction extension that aft hook 36 lower end only puts device 14 is backward provided with hook formation, can lock with the rear hanger of the task gondola of inserting in interior hanger 9 cavity or be separated.Only pendulum device prevents from departing from hanger because interference in air flow causes task gondola 3 double swerve in task process.
Composition graphs 5, Fig. 6, Fig. 7, described front transmission mechanism comprises:
(1) front end and front hook 24 pass through the first front rod 25 of pinned connection;
(2) undertaken by the second bearing pin the second front rod 27 of being connected front end and the first front rod 25 rear end;
(3) front arm 26 connecting interior hanger 9 inwall and the first front rod 25, second front rod 27 junction bearing pin is arranged to; Front arm 26 and interior hanger 9 inwall by the 3rd pinned connection, described first front rod 25 and the second front rod 27 junction with the 3rd bearing pin be the center of circle, with front arm 26 for radius rotates;
(3) the first central rotating shaft 28-1 is set and is provided with the locking rocking arm 28 to the first rocking arm 28-2 of three directions extensions, the second rocking arm 28-3 and arc lock hook 28-4 centered by the first central rotating shaft 28-1; Described central rotating shaft 28-1 and interior hanger 9 inwall pass through the 6th pinned connection, the first rocking arm 28-2 and the second front rod 27 rear end pinned connection; In the present invention, arc lock hook 28-4 is 1/4 arc-shaped structure, and described arcwall face is to latch hook 29, and the angle between the first rocking arm 28-2 and the second rocking arm 28-3 is 90 °, and the angle between the first rocking arm 28-2 and arc lock hook 28-4 is 135 °.
Composition graphs 5, Fig. 6, Fig. 7, rear transmission device comprises:
(1) the first rear linking rod 35 of rear end and aft hook 36 pinned connection,
(2) the second rear linking rod 33 of rear end and the first rear linking rod 35 rear end pinned connection,
(3) rear arm 34 connecting interior hanger 9 inwall and the first rear linking rod 35, second rear linking rod 33 junction bearing pin is arranged to, rear arm 34 is connected with interior hanger 9 by the 12 bearing pin, described first rear linking rod 35 and the second rear linking rod 33 junction with the 12 bearing pin be the center of circle, with rear arm 34 for radius rotates;
(4) the second central rotating shaft 32-1 is set and is provided with centered by the second central rotating shaft 32-1 to the 3rd rocking arm 32-2 of both direction extension and the rocking arm 28 of unblanking of the 4th rocking arm 32-3; Described second central rotating shaft 32-1 and interior hanger 9 inwall pass through the 9th pinned connection, the 4th rocking arm 32-3 and the second rear linking rod 33 front end pinned connection.
Composition graphs 6, described balanced connecting rod 17 one end and the second rocking arm 28-3 pinned connection, the other end and the 3rd rocking arm 32-2 pinned connection, balanced connecting rod 17 plays equilibrium activity in the power of forward and aft hanger.
Composition graphs 4, Fig. 5, Fig. 6, Fig. 7, described lockout mechanism comprises:
(1) lock hole 11 of pylon 7 side is positioned at;
(2) open keyhole 13 of pylon 7 and lock hole 11 the same side is positioned at,
(3) the 6th bearing pins are provided with in the face of the bottom surface of interior hanger 9 inwall the first locked groove 28-5 mated with obturator hernia 11;
(4) hanger 9 cavity is positioned at and front end is provided with hook formation 29-2, middle part is connected with the cavity wall of hanger 9 by the 8th bearing pin, afterbody is connected with the cavity wall of hanger 9 by extension spring 18 latch hook 29; Described hook formation 29-2 and arc lock hook 28-4 matches, and described 8th bearing pin is provided with in the face of the bottom surface of interior hanger 9 inwall the second locked groove 29-1 mated with open keyhole 13.
Composition graphs 7, described 3rd rocking arm 32-2 is connected with interior hanger 9 cavity wall with stage clip axle center 22 by stage clip 20, stage clip axle sleeve 21.Described stage clip 20 is enclosed within stage clip axle sleeve 21; Stage clip axle sleeve 21 is fixed on the cavity wall of interior hanger 9 relative to the far-end of the 3rd rocking arm 32-2; Stage clip axle 22 one end is connected with the 3rd rocking arm 32-2, and the other end inserts stage clip axle sleeve 21 relative to the 3rd rocking arm 32-2 near-end.
Composition graphs 4, Fig. 5, Fig. 6, Fig. 7, as a modification of the present invention, in order to prevent in the process of executing the task, impact due to environment causes task gondola 3 and hanger to come off, unmanned aerial vehicle onboard gondola hanger also comprises safety gear, and described safety gear comprises: (1) is arranged at the safe lockhole 12 of pylon 7 side; (2) interior hanger 9 is arranged at and the safe pin-and-hole mated with safe lockhole 12; (3) safety pin 42; When hook formation 29-2 and arc lock hook 28-4 locks, safety pin 42 is against latch hook 29 lower end through safe lockhole 12 and safe pin-and-hole, prevents latch hook 29 from rotating.
Composition graphs 5, Fig. 6, Fig. 7, as a modification of the present invention, in order to prevent latch hook 29 inordinate rotation, according to actual conditions, interior hanger 9 cavity wall is provided with the limited post 30 of restriction latch hook 29 rotational angle in the lower end of latch hook 29.
In the present invention, described first locked groove 28-5, the second locked groove 29-1 are interior hexagonal spill locked groove.
Principle of work of the present invention is: when needs wing 1 time configuration task gondola, and stop before being first placed in by task gondola 3 below rocker 10 and rear only rocker 14, front and back hanger is inserted in the cavity of interior hanger 9; Then the torque-indicating wrench front hexagonal nut 37 of twisting and rear hexagonal nut 39 is used to drive front lift bolt 15 and rear lift bolt 23 upward movement, under the effect of front transmission mechanism and rear transmission device, front hook 24 and aft hook 36 do clockwise movement and counterclockwise movement respectively, when hook is hung in task gondola and the task gondola of drive rises to and the effect of only putting the tangent position of device and stopping hexagonal nut; Rotating the second locked groove 29-1 is with moveable lock hook 29 rotate clockwise and be connected on arc lock hook 28-4; Rotate the first locked groove 28-5, locked locking rocking arm 28 thus locked whole transmission device.
When needs unload task gondola 3, first rotate the first locked groove 28-5, unlock locking rocking arm 28; Rotating the second locked groove 29-1 is with moveable lock hook 29 rotate counterclockwise and depart from from arc lock hook 28-4; The torque-indicating wrench front hexagonal nut 37 of twisting and rear hexagonal nut 39 is used to drive front lift bolt 15 and rear lift bolt 23 upward movement, under the effect of front transmission mechanism and rear transmission device, front hook 24 and aft hook 36 do counterclockwise movement and clockwise movement respectively, thus hook is departed from from the hanger of task gondola; Finally unload task gondola.
Claims (10)
1. a novel unmanned aerial vehicle onboard gondola hanger, is characterized in that, comprising:
Pylon (7), is fixed on wing (1) lower aerofoil,
Interior hanger (9), has cavity and rear and front end, bottom surface is provided with the mounting groove (43) of inserting cavity for gondola (3) forward and backward hanger,
Front lift bolt (15) and rear lift bolt (23), to insert in interior hanger (9) cavity and to provide axial motion and load,
Front hook (24), is connected with front lift bolt (15) lower end,
Aft hook (36), is connected with rear lift bolt (23) lower end,
Front transmission mechanism, be arranged to and connect front hook (24) and interior hanger (9), it is that the center of circle is rotated and locked with gondola (3) front hanger or be separated that described front transmission mechanism orders about front hook (24) with itself and front lift bolt (15) junction
Rear transmission device, be arranged to and connect front hook (36) and interior hanger (9), described rear transmission device order about aft hook (36) with itself and rear lift bolt (23) junction be the center of circle rotate with gondola (3) afterwards hanger lock or be separated
Balanced connecting rod (17), is arranged to and connects front transmission mechanism and rear transmission device,
Lockout mechanism, is arranged to and stops front transmission mechanism motion.
2. novel unmanned aerial vehicle onboard gondola hanger according to claim 1, is characterized in that,
Front transmission mechanism comprises:
First front rod (25), its front end and front hook (24) middle part pinned connection,
Second front rod (27), its front end and the first front rod (25) rear end pinned connection,
Front arm (26), is arranged to hanger (9) inwall and the first front rod (25), the second front rod (27) junction bearing pin in connecting,
Locking rocking arm (28), be provided with the first central rotating shaft (28-1) and be provided with the first rocking arm (28-2), the second rocking arm (28-3) and the arc lock hook (28-4) that extend to three directions centered by the first central rotating shaft (28-1), described central rotating shaft (28-1) passes through the 6th pinned connection with interior hanger (9) inwall, the first rocking arm (28-2) and the second front rod (27) rear end pinned connection;
Rear transmission device comprises:
First rear linking rod (35), rear end and aft hook (36) middle part pinned connection,
Second rear linking rod (33), rear end and the first rear linking rod (35) rear end pinned connection,
Rear arm (34), is arranged to hanger (9) inwall and the first rear linking rod (35), the second rear linking rod (33) junction bearing pin in connecting,
To unblank rocking arm (28), be provided with the second central rotating shaft (32-1) and be provided with centered by the second central rotating shaft (32-1) to the 3rd rocking arm (32-2) of both direction extension and the 4th rocking arm (32-3), described second central rotating shaft (32-1) passes through the 9th pinned connection with interior hanger (9) inwall, the 4th rocking arm (32-3) and the second rear linking rod (33) front end pinned connection;
Described balanced connecting rod (17) one end and the second rocking arm (28-3) pinned connection, the other end and the 3rd rocking arm (32-2) pinned connection.
3. novel unmanned aerial vehicle onboard gondola hanger according to claim 1 and 2, is characterized in that,
Front lift bolt (15) stretches into the cavity of hanger (9) by the front lining (16) being positioned at hanger (9), its lower end is provided with the ears with through hole, the front lift bolt (15) being positioned at hanger (9) outside is provided with trapezoidal outside thread, and front hexagonal nut (37) is threadedly connected to and is positioned on the outside front lift bolt (15) of hanger (9); Described front hook (24) upper end be placed in before lift bolt (15) lower end ears and with front lift bolt (15) pinned connection;
Rear lift bolt (23) stretches into the cavity of hanger (9) by the back bush (38) being positioned at hanger (9), its lower end is provided with the ears with through hole, the rear lift bolt (23) being positioned at hanger (9) outside is provided with Acme thread, and rear hexagonal nut (39) is threadedly connected to and is positioned on the outside rear lift bolt (23) of hanger (9); Described aft hook (36) upper end be placed in rear lift bolt (23) lower end ears and with rear lift bolt (23) pinned connection.
4. novel unmanned aerial vehicle onboard gondola hanger according to claim 1 and 2, it is characterized in that, described lockout mechanism comprises:
Be positioned at lock hole (11) and the open keyhole (13) of pylon (7) side,
6th bearing pin is provided with in the face of the bottom surface of interior hanger (9) inwall the first locked groove (28-5) mated with obturator hernia (11),
Be positioned at hanger (9) cavity and front end is provided with hook formation (29-2), middle part is connected with the cavity wall of hanger (9) by the 8th bearing pin, afterbody passes through the latch hook (29) that is connected with the cavity wall of hanger (9) of extension spring (18), described hook formation (29-2) and arc lock hook (28-4) match, and described 8th bearing pin is provided with in the face of the bottom surface of interior hanger (9) inwall the second locked groove (29-1) mated with open keyhole (13).
5. novel unmanned aerial vehicle onboard gondola hanger according to claim 2, it is characterized in that, described 3rd rocking arm (32-2) is connected with interior hanger (9) cavity wall with stage clip axle center (22) by stage clip (20), stage clip axle sleeve (21)
Described stage clip (20) is enclosed within stage clip axle sleeve (21),
Described stage clip axle sleeve (21) is fixed on the cavity wall of interior hanger (9) relative to the far-end of the 3rd rocking arm (32-2),
Described stage clip axle (22) one end is connected with the 3rd rocking arm (32-2), and the other end inserts stage clip axle sleeve (21) relative to the 3rd rocking arm (32-2) near-end.
6. novel unmanned aerial vehicle onboard gondola hanger according to claim 4, it is characterized in that, unmanned aerial vehicle onboard gondola hanger also comprises safety gear, comprising:
Be arranged at the safe lockhole (12) of pylon (7) side,
Be arranged at interior hanger (9) and the safe pin-and-hole mated with safe lockhole (12), and
Safety pin (42);
When hook formation (29-2) and arc lock hook (28-4) are locked, safety pin (42) is against latch hook (29) lower end through safe lockhole (12) and safe pin-and-hole, prevents latch hook (29) from rotating.
7. novel unmanned aerial vehicle onboard gondola hanger according to claim 4, it is characterized in that, interior hanger (9) cavity wall is provided with the limited post (30) of restriction latch hook (29) rotational angle in the lower end of latch hook (29).
8. novel unmanned aerial vehicle onboard gondola hanger according to claim 1, it is characterized in that, erecting by overhang also comprises:
Be arranged at before on front side of the front opening of interior hanger (9) bottom surface and only put device (10), only put device (10) before described and comprise and be connected two chevron pointing blocks tangent with gondola (3) profile,
To be arranged on rear side of the open rearward end of interior hanger (9) bottom surface and be connected with gondola only put device (14) afterwards, only put device (14) after described and comprise and be connected two chevron pointing blocks tangent with gondola (3) profile.
9. novel unmanned aerial vehicle onboard gondola hanger according to claim 4, it is characterized in that, arc lock hook (28-4) is 1/4 arc-shaped structure, described arcwall face is to latch hook (29), angle between first rocking arm (28-2) and the second rocking arm (28-3) is 90 °, and the angle between the first rocking arm (28-2) and arc lock hook (28-4) is 135 °.
10. novel unmanned aerial vehicle onboard gondola hanger according to claim 4, is characterized in that, the first locked groove (28-5), the second locked groove (29-1) are interior hexagonal spill locked groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510117529.6A CN104691769B (en) | 2015-03-17 | 2015-03-17 | Novel unmanned aerial vehicle airborne pod hanging frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510117529.6A CN104691769B (en) | 2015-03-17 | 2015-03-17 | Novel unmanned aerial vehicle airborne pod hanging frame |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104691769A true CN104691769A (en) | 2015-06-10 |
| CN104691769B CN104691769B (en) | 2017-05-10 |
Family
ID=53339405
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510117529.6A Active CN104691769B (en) | 2015-03-17 | 2015-03-17 | Novel unmanned aerial vehicle airborne pod hanging frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104691769B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890877A (en) * | 2015-06-19 | 2015-09-09 | 中国航空工业集团公司西安飞机设计研究所 | Ladder hanging rack structure |
| CN106628213A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Quick disassembling device for mission loads of unmanned aerial vehicle |
| CN107444650A (en) * | 2017-07-14 | 2017-12-08 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of anti-sway retainer of airborne stores |
| CN107685869A (en) * | 2017-08-23 | 2018-02-13 | 天津津航技术物理研究所 | A kind of large photoelectric gondola installing mechanism |
| CN107697294A (en) * | 2017-10-20 | 2018-02-16 | 上海优伟斯智能***有限公司 | A kind of amphibious fixed-wing logistics aircraft of wing carry goods |
| CN109606686A (en) * | 2018-12-10 | 2019-04-12 | 彩虹无人机科技有限公司 | A kind of universal unmanned plane emitter switching beam |
| CN112208770A (en) * | 2020-10-10 | 2021-01-12 | 江西洪都航空工业集团有限责任公司 | Linkage retraction device for cabin door of exposed equipment of airplane |
| CN113998119A (en) * | 2021-02-25 | 2022-02-01 | 陈坤 | Double-wing aircraft with external hanging rack |
| CN114084371A (en) * | 2021-12-02 | 2022-02-25 | 中国船舶工业***工程研究院 | Flexible interface seat and unmanned aerial vehicle load bearing bracket applied by same |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3503576A (en) * | 1967-11-10 | 1970-03-31 | Alkan R & Cie | Automatic-release retaining device for jettisonable aircraft cargo |
| US20040011926A1 (en) * | 2002-07-22 | 2004-01-22 | Shay William F. | System and method for loading stores on an aircraft |
| US20100301159A1 (en) * | 2009-06-01 | 2010-12-02 | Israel Aerospace Industries Ltd. | Mounting set, system and method |
| CN203127147U (en) * | 2013-01-15 | 2013-08-14 | 长安大学 | Unmanned aerial vehicle pod |
| CN103754366A (en) * | 2014-01-10 | 2014-04-30 | 大连理工大学 | Pneumatic high-speed catapult for embedded loads |
-
2015
- 2015-03-17 CN CN201510117529.6A patent/CN104691769B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3503576A (en) * | 1967-11-10 | 1970-03-31 | Alkan R & Cie | Automatic-release retaining device for jettisonable aircraft cargo |
| US20040011926A1 (en) * | 2002-07-22 | 2004-01-22 | Shay William F. | System and method for loading stores on an aircraft |
| US20100301159A1 (en) * | 2009-06-01 | 2010-12-02 | Israel Aerospace Industries Ltd. | Mounting set, system and method |
| CN203127147U (en) * | 2013-01-15 | 2013-08-14 | 长安大学 | Unmanned aerial vehicle pod |
| CN103754366A (en) * | 2014-01-10 | 2014-04-30 | 大连理工大学 | Pneumatic high-speed catapult for embedded loads |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890877A (en) * | 2015-06-19 | 2015-09-09 | 中国航空工业集团公司西安飞机设计研究所 | Ladder hanging rack structure |
| CN106628213A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Quick disassembling device for mission loads of unmanned aerial vehicle |
| CN107444650A (en) * | 2017-07-14 | 2017-12-08 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of anti-sway retainer of airborne stores |
| CN107444650B (en) * | 2017-07-14 | 2020-07-03 | 中国航空工业集团公司沈阳飞机设计研究所 | Anti-swing stopper for airborne suspended object |
| CN107685869A (en) * | 2017-08-23 | 2018-02-13 | 天津津航技术物理研究所 | A kind of large photoelectric gondola installing mechanism |
| CN107697294A (en) * | 2017-10-20 | 2018-02-16 | 上海优伟斯智能***有限公司 | A kind of amphibious fixed-wing logistics aircraft of wing carry goods |
| CN109606686A (en) * | 2018-12-10 | 2019-04-12 | 彩虹无人机科技有限公司 | A kind of universal unmanned plane emitter switching beam |
| CN112208770A (en) * | 2020-10-10 | 2021-01-12 | 江西洪都航空工业集团有限责任公司 | Linkage retraction device for cabin door of exposed equipment of airplane |
| CN113998119A (en) * | 2021-02-25 | 2022-02-01 | 陈坤 | Double-wing aircraft with external hanging rack |
| CN113998119B (en) * | 2021-02-25 | 2023-10-20 | 陈坤 | Double-wing aircraft with externally hung hanging frame |
| CN114084371A (en) * | 2021-12-02 | 2022-02-25 | 中国船舶工业***工程研究院 | Flexible interface seat and unmanned aerial vehicle load bearing bracket applied by same |
| CN114084371B (en) * | 2021-12-02 | 2023-05-16 | 中国船舶工业***工程研究院 | Flexible interface seat and unmanned aerial vehicle carrying bracket applied to same |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104691769B (en) | 2017-05-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104691769A (en) | Novel unmanned aerial vehicle airborne pod hanging frame | |
| US10829233B2 (en) | Engine assembly for an aircraft comprising a front engine attachment which facilitates its assembly | |
| CN101519119B (en) | Fast-disassembly method of aeroplane access cover and bearing lock | |
| CN101973501B (en) | Fan integral installation rotating holding mechanism | |
| US20170113780A1 (en) | A passenger aircraft with a downwardly foldable wing tip device | |
| US9790926B2 (en) | Counterweighting a wind turbine hub | |
| US10486819B2 (en) | Method and device for mounting an engine on an aircraft pylon | |
| CN103410896B (en) | A kind of 2 D photoelectric turntable locking device | |
| RU2428356C2 (en) | Nut system and aircraft engine strut with said system | |
| DE102012025316A1 (en) | Missile container | |
| CN201357942Y (en) | Quick release force bearing lock of airplane hatch cover | |
| CN110536831A (en) | Aircraft stopping sliding door and its application method with plane internal load transmission capacity | |
| CN109774922A (en) | It is a kind of become grounding point master play landing gear | |
| US10982805B2 (en) | Ergonomic device for suspending aircraft flight control apparatuses | |
| CN208906777U (en) | A kind of wing stable rotation and self-locking collapsible unmanned plane | |
| CN214690264U (en) | End shield and one-level integrally-recycled suborbital carrier rocket | |
| CN102278021B (en) | Door lock device of railway freight open wagon | |
| CN205768905U (en) | Vehicular oil engine shelter damping device | |
| CN103753207B (en) | For the turning device of wind driven generator principal shaft | |
| US9802697B2 (en) | Aircraft landing gear | |
| CN109204815A (en) | A kind of wing stable rotation and self-locking collapsible unmanned plane | |
| CN214869990U (en) | Maintenance tool for middle ejector pin of container lifting appliance of quayside container | |
| KR101192497B1 (en) | Rotating test module for aircraft rotor having balance weight | |
| CN111169624B (en) | Landing gear upper lock structure for aviation emergency | |
| CN107575547A (en) | A kind of split type tail pylon latch gear electric transmission machanism and its locking taper method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |