CN108639353A - A kind of self balancing safety seat of aircraft - Google Patents
A kind of self balancing safety seat of aircraft Download PDFInfo
- Publication number
- CN108639353A CN108639353A CN201810492448.8A CN201810492448A CN108639353A CN 108639353 A CN108639353 A CN 108639353A CN 201810492448 A CN201810492448 A CN 201810492448A CN 108639353 A CN108639353 A CN 108639353A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- protective cover
- seat
- safety seat
- guard ring
- 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.)
- Pending
Links
- 230000001681 protective effect Effects 0.000 claims abstract description 68
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 15
- 230000009429 distress Effects 0.000 claims description 15
- 239000001301 oxygen Substances 0.000 claims description 15
- 229910052760 oxygen Inorganic materials 0.000 claims description 15
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 10
- 238000001514 detection method Methods 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 7
- 230000005484 gravity Effects 0.000 claims description 6
- 239000003651 drinking water Substances 0.000 claims description 3
- 235000020188 drinking water Nutrition 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 claims 1
- 208000027418 Wounds and injury Diseases 0.000 abstract description 4
- 230000006378 damage Effects 0.000 abstract description 4
- 208000014674 injury Diseases 0.000 abstract description 3
- 230000008878 coupling Effects 0.000 description 12
- 238000010168 coupling process Methods 0.000 description 12
- 238000005859 coupling reaction Methods 0.000 description 12
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 239000002775 capsule Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 206010052428 Wound Diseases 0.000 description 1
- 210000001015 abdomen Anatomy 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- -1 temperature Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0619—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with energy absorbing means specially adapted for mitigating impact loads for passenger seats, e.g. at a crash
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
The present invention relates to safety seat fields, more particularly to a kind of self balancing safety seat of aircraft, the safety seat of aircraft includes shell, protective cover, parachute, seat, buffer unit, shell, protective cover and buffer unit constitute space cabin structure, parachute is set to outside protective cover, and seat is set in protective cover, and guard ring is equipped between seat and protective cover, seat is connected with guard ring by the first attachment device, and seat is with guard ring around the first attachment device relative rotation；Guard ring is connect with protective cover by the second attachment device, and guard ring is with protective cover around the second attachment device relative rotation；Seat, guard ring, protective cover constitute gimbals structure by the first attachment device and the second attachment device；Compared with prior art, even if safety seat of aircraft of the invention bounces again when landing, what is rolled is only external protective cover and base portion, and the seat for carrying passenger remains horizontal until landing completely, will not cause secondary injury to passenger.
Description
Technical field
The present invention relates to safety seat fields, more particularly to a kind of self balancing safety seat of aircraft.
Background technology
Aircraft is one of the means of transport of contemporary most convenient, and high speed is conveniently its great advantage, but present aircraft
Security performance is very poor, if aircraft meets with accident in flight, often fatal crass；It is most of when accident occurs
Captain can control aircraft and fly to sea, can thus reduce damage of the aircraft to above ground structure, and survive across the sea
Probability be much larger than ground, if however cannot be succoured in time behind airplane falling sea, people still can be swallowed by seawater,
Loss of life.
To solve the above problems, Chinese invention CN201410478221.X discloses a kind of safe airplane, including aircraft,
Safety belt, air bag, oxygen and oxygen mask, seat protective cover, parachute, floatation pad, micro computer, definition space component are high
Spend positioning component, information receiver transmitter component, infrared induction component, micro- spray propeller, sliding rail, pulley, hatch door of escaping, electricity
Turn axis, protective cover stretchable layer, safety seat, stand-by power supply etc., all aircraft seats make one it is intelligentized small-sized
The escape hatch door of sealed space capsule, aircraft can be located at the abdomen of aircraft, tail portion or be the same internal weapon bays of fighter plane
Formula installs four pulleys at the angle of the bottom of every seat of aircraft four, and pulley is usually fixed on inside sliding rail, installation inside seat
Configure safety guard plate, oxygen, temperature, air pressure, air bag, parachute, floatation pad, micro- spray propeller, infrared induction, nothing
Line receives sending assembly, intelligent microcomputer, space probe, highly automated measuring appliance, safety belt.
The space capsule of for example same intelligentized small hermetic of the aircraft seat of the safe airplane, by escape compartment when escape
Door skids off aircraft and realizes safe falling by parachute；The aircraft seat bottom is equipped with air bag and floatation pad, falls in water
When on face, it can swim on the water surface；But fall at land, when landing under the action of impulse force, the buffering of air bag
Aircraft seat may be caused to bounce again and occur to roll in the air, cause the secondary injury to passenger.
In view of this, the present inventor especially has developed a kind of self balancing safety seat of aircraft, thus this case generates.
Invention content
To solve the above problems, the present invention provides a kind of self balancing safety seat of aircraft.
To achieve the above object, the technical solution adopted by the present invention is as follows：A kind of self balancing safety seat of aircraft, including
Shell, protective cover, parachute, seat, buffer unit, the shell, protective cover and buffer unit constitute space cabin structure, institute
The parachute stated is set to outside protective cover, and the seat is set in protective cover, and protection is equipped between the seat and protective cover
Circle, the guard ring are arranged around seat；The seat is connected with guard ring by the first attachment device, the seat
With guard ring around the first attachment device relative rotation；The guard ring is connect with protective cover by the second attachment device, described
Guard ring and protective cover around the second attachment device relative rotation；First attachment device and the second attachment device axial direction side
To being mutually perpendicular to, the seat, guard ring, protective cover pass through the first attachment device and constitute balance ring knot with the second attachment device
Structure.
Further, chair back is equipped with intelligence control system, and the intelligence control system includes detection device, control
Device and intelligent processing system, the detection device are used to detect aircraft safety state and monitor the shape of safety seat of aircraft itself
State, the control device are connected with each device on safety seat of aircraft, and the intelligent processing system is sent out for disaster
Escape state is formed by each device of control device intelligent control safety seat of aircraft when raw.
Further, chair back is equipped with oxygen generator, positioning device and distress signal sending device, the oxygen
Gas generating means, positioning device and distress signal sending device are connected with control device, and the oxygen generator is used for
Oxygen is conveyed when protective cover is closed；The positioning device is used to position the position of safety seat of aircraft；The distress signal hair
Send device for sending distress signal.
Further, seat includes pedestal, backrest, cushion, handrail, safety belt；The safety belt is for fixing passenger
Body；The backrest and cushion are separately positioned, and the handrail is equipped with control panel, the control panel and control
Device is connected, and when being used for special circumstances, manually controls each device of safety seat of aircraft.
Further, it is set equipped with pendant refitting in pedestal and the center of gravity for stable chair is set in containing cavities, the pendant refitting,
Maintain the balance of seat；Wilderness lore equipment, food, drinking-water are equipped in the containing cavities.
Further, protective cover is made of high tenacity, deformable memory material, and the protection cover outer surface is covered with
High-temperature-resistant layer.
Further, buffer unit is made of soft floating material, the bottom of protective cover is set to, for serving as aircraft safety
The pedestal of chair；It is equipped with pendant refitting in the buffer unit to set, the center of gravity for stablizing buffer unit, dimension are set in the pendant refitting
Hold the balance of buffer unit.
Further, buffer unit is equipped with the locking device coordinated with protective cover bottom, for lockking the protection closed
It covers, there is protective cover to release the button on the locking device.
Further, buffer unit bottom is equipped with multiple wheel groups, and the wheel group maintains safety seat of aircraft balance, described
Wheel group is used to connect the sliding rail for leading to escape hatch door on aircraft.
Further, shell is equipped with protective cover storage tank, and the protective cover storage tank is flexible for serving as protective cover
Protective cover when track and accommodating open state.
By the above-mentioned description of this invention it is found that compared with prior art, self balancing safety seat of aircraft of the invention
When landing, it still may again be bounced due to landing impulse force and occur to roll in the air, but the self balancing aircraft peace of the present invention
Full chair is designed as gimbals structure, and seat is detached with exterior protection cover, bounced again, and what is rolled is only external protective cover
And base portion, the seat for carrying passenger remain horizontal until landing completely, secondary injury will not be caused to passenger, is safeguarded
The life security of passenger.
Description of the drawings
Fig. 1 is the structural schematic diagram of the self balancing safety seat of aircraft of the present invention；
Fig. 2 is the side view of the self balancing safety seat of aircraft landing state of the present invention；
Fig. 3 is the front view of the self balancing safety seat of aircraft landing state of the present invention.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, is clearly and completely retouched to the technical solution in the present invention
It states, it is clear that the described embodiments are merely a part of the embodiments of the present invention, instead of all the embodiments.
It is structural schematic diagram, the landing state of the self balancing safety seat of aircraft of the present invention shown in referring to Fig.1~Fig. 3
The front view of side view and state of landing discloses a kind of self balancing safety seat of aircraft, including shell 1, protective cover 2, drop
Umbrella 3, seat 4, buffer unit 5 are fallen, the shell 1, protective cover 2 and buffer unit 5 constitute space cabin structure；The protection
Cover 2 is made of high tenacity, deformable memory material, and 2 outer surface of protective cover is covered with high-temperature-resistant layer；The landing
Umbrella 3 is set to outside protective cover 2, and the seat 4 is set in protective cover 2；4 bottom of seat is equipped with pendant refitting and sets 41, institute
The center of gravity that the pendant refitting stated sets 41 for stable chair 4, to maintain the balance of seat 4；It is set between the seat 4 and protective cover 2
There are guard ring 6, the guard ring 6 to be arranged around seat 4；The seat 4 and guard ring 6 is connected by the first attachment device 7
It connects, the seat 4 is with guard ring 6 around 7 relative rotation of the first attachment device；The guard ring 6 passes through second with protective cover 2
Attachment device 8 connects, and the guard ring 6 is with protective cover 2 around 8 relative rotation of the second attachment device；The first connection dress
It sets 7 to be mutually perpendicular to 8 axial direction of the second attachment device, the seat 4, guard ring 6, protective cover 2 are filled by the first connection
Set 7 and second attachment device 8 constitute gimbals structure.
First attachment device 7 includes the connecting shaft 71 for running through seat 4, is arranged on guard ring 6 and distribution is present
4 both sides of chair, two connecting shafts 72 corresponding with connecting shaft 71 and be distributed in 4 both sides of seat connection connecting shaft 71, connecting shaft 72 two
Group shaft coupling 73；The connecting shaft 71 is connected with seat 4, and seat 4 is rotated with the rotation of connecting shaft 71；The company
By the connecting shaft 72 of shaft coupling 73 and both sides relative rotation can occur for spindle 71.
Second attachment device 8 includes the connecting shaft 81 for being correspondingly arranged at 6 both ends of guard ring, is arranged in protective cover 2
Upper connecting shaft 82 corresponding with connecting shaft 81 is arranged on shell 1 connecting shaft 83 corresponding with connecting shaft 81, connects connecting shaft 81
And connecting shaft 82 shaft coupling 84, connection connecting shaft 81 and connecting shaft 83 shaft coupling 85；The connecting shaft 81 and guard ring 6
It is connected, guard ring 6 is rotated with the rotation of connecting shaft 81；The connecting shaft 81 by shaft coupling 84 and shaft coupling 85 with
Relative rotation can occur for connecting shaft 82, the connecting shaft 83 of both sides；The shaft coupling 84 is separated into be connected with connecting shaft 81
The coupling assembly 841 connect and the coupling assembly 842 being connected with connecting shaft 82, the coupling assembly 841, shaft coupling
Component 842 can reformulate shaft coupling 84 when docking.
The shell 1 is equipped with protective cover storage tank 11, and the protective cover storage tank 11 is stretched for serving as protective cover
Protective cover 2 when contracting track and accommodating open state.
The buffer unit 5 is made of soft floating material, the bottom of protective cover 2 is set to, for serving as aircraft safety
The pedestal of chair, the buffer unit 5 is interior to set 51 equipped with pendant refitting, and the pendant, which is reset, sets 51 centers of gravity for being used for buffer unit 5,
To maintain the balance of buffer unit 5 and the protective cover being connected with buffer unit 52；The buffer unit 5 is equipped with and prevents
The locking device 52 of 2 bottom of shield cooperation has protective cover unlatching for lockking the protective cover closed on the locking device 52
Button 521；5 bottom of buffer unit is equipped with multiple wheel groups 9, and the wheel group 9 is distributed in triangle disposition, for remaining winged
Machine safe chair balances, and the wheel group 9 is used to connect the sliding rail for leading to escape hatch door on aircraft.
The seat 4 is equipped with seat harness 42, the body for fixing passenger；It is set in 4 pedestal of seat
There are containing cavities 43, wilderness lore equipment, food, drinking-water etc. are equipped in the containing cavities 43；4 back of seat is equipped with intelligence
Can control system 10, the intelligence control system includes detection device 101, control device 102 and intelligent processing system 103,
The detection device 101 is used to detect aircraft safety state and monitor the state of safety seat of aircraft itself, control dress
It sets 102 with each device on safety seat of aircraft to be connected, the running for controlling these devices, the intelligent processing system
103 are used to pass through when disaster occurs each device formation escape state of 102 intelligent control safety seat of aircraft of control device.
4 back of seat is equipped with oxygen generator 44, positioning device 45 and distress signal sending device 46, the oxygen
Generating means 44, positioning device 45 and distress signal sending device 46 are connected with control device 102, and the oxygen fills
44 are set to be used to convey oxygen when protective cover 2 is closed；The positioning device 45 is used to position the position of safety seat of aircraft；Described
Distress signal sending device 46 is for sending distress signal；Seat 4 includes pedestal, backrest, cushion, handrail, in the pedestal
It is set equipped with pendant refitting, the backrest and cushion are separately positioned, and the handrail 47 is equipped with control panel 471, the control
Panel 471 processed is connected with control device 102, when being used for special circumstances, manually controls each device of safety seat of aircraft.
The self balancing safety seat of aircraft of the present invention when in use, pacify by the flight of the constantly detection aircraft of detection device 101
Total state, when accident occurs, detection device 101 is by the data feedback detected to intelligent processing system 103, intelligent processing system
103 automatically fall off protective cover 2 by control device 102 and start oxygen generator 44, and the wheel group 9 of 5 bottom of buffer unit is logical
It crosses sliding rail and slides to escape hatch door and flee from wrecked aircraft, in descent, intelligent processing system 103 calculates descent altitude and simultaneously beats in due course
Open parachute, in descent, seat 4 and protective cover 2 maintain balance in the air under the action of pendant refitting is set.
When safety seat of aircraft drops to the water surface, the cavity that the soft floating material and protective cover of buffer unit 5 are formed generates
Buoyancy holds up safety seat of aircraft, is allowed to swim on the water surface；Meanwhile positioning device 45 positions the position of safety seat of aircraft and incites somebody to action
The position is sent to location-server terminal, and distress signal sending device 46 sends distress signal, searched convenient for rescue worker
It rescues.
When safety seat of aircraft drops to land, buffer unit 5 realizes the soft landing of safety seat of aircraft, when bouncing again,
Gimbals structure on safety seat of aircraft makes seat 4 remain balance, until landing completely static；Meanwhile positioning device 45
It positions the position of safety seat of aircraft and the position is sent to location-server terminal, distress signal sending device 46 sends emergency
Signal is searched and rescued convenient for rescue worker.
By the above-mentioned description of this invention it is found that compared with prior art, self balancing safety seat of aircraft of the invention
When landing, it still may again be bounced due to landing impulse force and occur to roll in the air, but the self balancing aircraft peace of the present invention
Full chair is designed as gimbals structure, and seat 4 is detached with exterior protection cover 2, and when bouncing again, what is rolled is only the anti-of outside
Shield 2 and base portion, the seat 4 for carrying passenger remain horizontal until landing completely, secondary wound will not be caused to passenger
Evil, safeguards the life security of passenger.
The preferred embodiment of the present invention is above are only, but the design concept of the present invention is not limited thereto, all profits
The change for carrying out unsubstantiality to the present invention with this design, should all belong to the behavior for invading the scope of the present invention.
Claims (10)
1. a kind of self balancing safety seat of aircraft, including shell, protective cover, parachute, seat, buffer unit, described is outer
Shell, protective cover and buffer unit constitute space cabin structure, and the parachute is set to outside protective cover, it is characterised in that：It is described
Seat be set to protective cover in, between the seat and protective cover be equipped with guard ring, the guard ring around seat be arranged；Institute
The seat stated is connected with guard ring by the first attachment device, and the seat and guard ring are around the opposite rotation of the first attachment device
Turn；The guard ring is connect with protective cover by the second attachment device, and the guard ring connect dress with protective cover around second
Set relative rotation；First attachment device is mutually perpendicular to the second attachment device axial direction, the seat, protection
Circle, protective cover constitute gimbals structure by the first attachment device and the second attachment device.
2. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The chair back is equipped with intelligence
Control system, the intelligence control system include detection device, control device and intelligent processing system, the detection device
For detecting aircraft safety state and monitoring the state of safety seat of aircraft itself, on the control device and safety seat of aircraft
Each device is connected, and the intelligent processing system passes through control device intelligent control safety seat of aircraft when occurring for disaster
Each device forms escape state.
3. self balancing safety seat of aircraft as claimed in claim 2, it is characterised in that：The chair back is equipped with oxygen
Generating means, positioning device and distress signal sending device, the oxygen generator, positioning device and distress signal are sent
Device is connected with control device, and the oxygen generator conveys oxygen when closed for protective cover；The positioning dress
Set the position for positioning safety seat of aircraft；The distress signal sending device is for sending distress signal.
4. self balancing safety seat of aircraft as claimed in claim 2, it is characterised in that：The seat includes pedestal, leans on
The back of the body, cushion, handrail, safety belt；The safety belt is used to fix the body of passenger；The backrest and cushion are separately positioned,
The handrail is equipped with control panel, and the control panel is connected with control device, when being used for special circumstances, controls manually
Each device of safety seat of aircraft processed.
5. self balancing safety seat of aircraft as claimed in claim 4, it is characterised in that：Pendant refitting is equipped in the pedestal
It sets and containing cavities, the pendant refitting sets the center of gravity for stable chair, maintain the balance of seat；It is equipped in the containing cavities
Wilderness lore equipment, food, drinking-water.
6. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The protective cover by high tenacity,
Deformable memory material is made, and the protection cover outer surface is covered with high-temperature-resistant layer.
7. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The buffer unit is by soft drift
Floating material is made, and is set to the bottom of protective cover, the pedestal for serving as safety seat of aircraft；Pendant weight is equipped in the buffer unit
Device, the pendant refitting set the center of gravity for stablizing buffer unit, maintain the balance of buffer unit.
8. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The buffer unit be equipped with
The locking device of protective cover bottom cooperation, have for lockking the protective cover closed, on the locking device protective cover unlatching by
Button.
9. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The buffer unit bottom is equipped with
Multiple wheel groups, the wheel group maintain safety seat of aircraft balance, and the wheel group, which is used to connect, leads to escape hatch door on aircraft
Sliding rail.
10. self balancing safety seat of aircraft as described in claim 1, it is characterised in that：The shell is equipped with protection
Cover storage tank, the protective cover storage tank are used to serve as protective cover when protective cover expansion rail and accommodating open state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810492448.8A CN108639353A (en) | 2018-05-22 | 2018-05-22 | A kind of self balancing safety seat of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810492448.8A CN108639353A (en) | 2018-05-22 | 2018-05-22 | A kind of self balancing safety seat of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108639353A true CN108639353A (en) | 2018-10-12 |
Family
ID=63757520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810492448.8A Pending CN108639353A (en) | 2018-05-22 | 2018-05-22 | A kind of self balancing safety seat of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108639353A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878738A (en) * | 2019-03-07 | 2019-06-14 | 苏州昊信精密机械有限公司 | A kind of aero seat angle adjustment device |
| CN109927913A (en) * | 2019-04-26 | 2019-06-25 | 上海盛昌文化传播有限公司 | A kind of aircraft intelligent escape seat |
| CN109986583A (en) * | 2019-05-09 | 2019-07-09 | 贵州理工学院 | A kind of landslide geological disaster rescue intelligent robot |
| CN111268139A (en) * | 2020-02-05 | 2020-06-12 | 绍兴裕铭机械科技有限公司 | External escape device on water of airborne vehicle |
-
2018
- 2018-05-22 CN CN201810492448.8A patent/CN108639353A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878738A (en) * | 2019-03-07 | 2019-06-14 | 苏州昊信精密机械有限公司 | A kind of aero seat angle adjustment device |
| CN109927913A (en) * | 2019-04-26 | 2019-06-25 | 上海盛昌文化传播有限公司 | A kind of aircraft intelligent escape seat |
| CN109927913B (en) * | 2019-04-26 | 2023-03-24 | 上海盛昌文化传播有限公司 | Intelligent escape seat for airplane |
| CN109986583A (en) * | 2019-05-09 | 2019-07-09 | 贵州理工学院 | A kind of landslide geological disaster rescue intelligent robot |
| CN111268139A (en) * | 2020-02-05 | 2020-06-12 | 绍兴裕铭机械科技有限公司 | External escape device on water of airborne vehicle |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20181012 |
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| WD01 | Invention patent application deemed withdrawn after publication |