CN113602509B - Stable umbrella framework connecting structure of oiling hose connector - Google Patents

Stable umbrella framework connecting structure of oiling hose connector Download PDF

Info

Publication number
CN113602509B
CN113602509B CN202111002641.7A CN202111002641A CN113602509B CN 113602509 B CN113602509 B CN 113602509B CN 202111002641 A CN202111002641 A CN 202111002641A CN 113602509 B CN113602509 B CN 113602509B
Authority
CN
China
Prior art keywords
stable umbrella
hose connector
double
stable
lug
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.)
Active
Application number
CN202111002641.7A
Other languages
Chinese (zh)
Other versions
CN113602509A (en
Inventor
周学
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC Aerospace Life Support Industries Ltd
Original Assignee
AVIC Aerospace Life Support Industries Ltd
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 AVIC Aerospace Life Support Industries Ltd filed Critical AVIC Aerospace Life Support Industries Ltd
Priority to CN202111002641.7A priority Critical patent/CN113602509B/en
Publication of CN113602509A publication Critical patent/CN113602509A/en
Application granted granted Critical
Publication of CN113602509B publication Critical patent/CN113602509B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D39/00Refuelling during flight
    • B64D39/04Adaptations of hose construction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

The invention discloses a stable umbrella framework connecting structure of a oiling hose joint, which comprises connecting lifting lugs (9), connecting rings (6), double-head threaded sleeves (7), stable umbrella frameworks (1) and limiting bushings (8), wherein the connecting lifting lugs (9) are circumferentially distributed on the oiling joint (4), the connecting rings (6) are provided with openings, threads are arranged at two ends of the connecting rings, the connecting rings (6) are matched with lug holes penetrating through the whole connecting lifting lugs (9), the double-head threaded sleeves (7) are positioned at the openings of the connecting rings (6) and are sleeved at two ends of the connecting rings (6) in a threaded mode, the stable umbrella frameworks (1) and the limiting bushings (8) are matched with each other along the connecting rings (6), and the limiting bushings (8) are used for limiting the stable umbrella frameworks (1) at two ends. The invention has reliable connection, small volume and light weight, and a connection space with double frameworks is reserved.

Description

Stable umbrella framework connecting structure of oiling hose connector
Technical Field
The invention belongs to the technical field of aerial refueling, and particularly relates to a stable umbrella framework connecting structure of a refueling hose connector.
Background
The utility model provides a refuel hose connects stable umbrella is a non-traditional parachute, by the stable umbrella skeleton of rigidity and flexible canopy are constituteed, at present, as shown in fig. 1 and 2, stable umbrella skeleton (1) is connected in the spacing inslot that fixed ring (3) and retainer (2) formed through round pin axle (5), fixed ring (3) and retainer (2) are installed on refuel joint (4), this connection structure is because the spacing stable umbrella skeleton (1) of required retainer (2) and fixed ring (3) and round pin axle (5), result in the product weight heavy, bulky, and the spacing groove size precision assembly requirement to retainer (2) and fixed ring (3) forms is higher, and round pin axle (5) drop from the spacing groove easily, this kind of structure also can't satisfy follow-up double-skeleton connection space requirement.
Disclosure of Invention
The invention aims to provide a stable umbrella framework connecting structure of a refueling hose connector, which is reliable in connection, small in size and light in weight, and a connecting space of double frameworks is reserved.
The technical scheme adopted by the invention is as follows:
the utility model provides a stable umbrella skeleton connection structure of flexible pipe joint refuels, including connecting lug (9), go-between (6), double-end swivel nut (7), stable umbrella skeleton (1) and spacing bush (8), connect lug (9) along circumference distribution on refuel joint (4), go-between (6) have the opening and both ends are equipped with the screw thread, go-between (6) complex pass the earhole of whole circle connection lug (9), double-end swivel nut (7) are located go-between (6) opening part and screw-thread fit's cover at go-between (6) both ends, stable umbrella skeleton (1) and spacing bush (8) all complex cover are along the go-between (6), spacing bush (8) are used for spacing stable umbrella skeleton (1) at both ends.
Further, the earhole is positioned at the upper part of the connecting lifting lug (9), and the lower part of the connecting lifting lug (9) is connected with the oiling joint (4) through a threaded hole.
Further, the threads at the two ends of the connecting ring (6) are opposite to each other.
Further, the connecting ring (6) is made of high-strength steel.
Further, the limiting bushing (8) is matched with the radian of the connecting ring (6) in the axial direction.
The beneficial effects of the invention are as follows:
the connecting ring (6) is provided with an opening, so that the penetration of the stable umbrella framework (1), the double-head threaded sleeve (7), the limiting bushing (8) and the connecting lifting lug (9) is facilitated, the integral connecting ring (6) can effectively provide the connection of the stable umbrella framework (1), and a connection space of the double frameworks is reserved; the limiting bushing (8) can ensure the stable position of the stable umbrella framework (1), replaces the structures of the guard ring (2) and the fixed ring (3), and reduces the structure volume and the weight; the connecting lifting lug (9) has the advantages of small volume, light weight and the like relative to the guard ring (2) and the fixed ring (3).
Drawings
FIG. 1 is a diagram of a current stabilized umbrella frame attachment for a fuel filler hose connector.
FIG. 2 shows a connection mode of the prior stable umbrella framework and the pin shaft.
FIG. 3 is a stabilized umbrella frame attachment structure for a fuel filler hose connector in accordance with an embodiment of the present invention.
Fig. 4 is a schematic view of the installation of a coupling ring and a double-ended screw sleeve in an embodiment of the present invention.
FIG. 5 is a schematic view of the installation of a connecting ring, a spacing sleeve and a double-ended screw sleeve in an embodiment of the invention.
Fig. 6 is a schematic view of the installation of the connecting shackle in an embodiment of the invention.
In the figure: 1-stabilizing an umbrella frame; 2-a retainer; 3-fixing ring; 4-oiling joint; 5-a pin shaft; 6-connecting rings; 7-double-head threaded sleeves; 8-limiting bushings; 9-connecting lifting lugs.
Detailed Description
The invention is further described below with reference to the drawings and examples.
As shown in fig. 3 to 6, the connecting structure of the stable umbrella framework of the oiling hose connector comprises a connecting lifting lug 9, a connecting ring 6, a double-end threaded sleeve 7, the stable umbrella framework 1 and a limiting bush 8, wherein the connecting lifting lug 9 is circumferentially distributed on the oiling connector 4, the connecting ring 6 is provided with an opening, threads are arranged at two ends of the connecting ring 6, the connecting ring 6 is matched with earholes penetrating through the whole ring and connecting lifting lug 9, the double-end threaded sleeve 7 is positioned at the opening of the connecting ring 6 and sleeved at two ends of the connecting ring 6 in a threaded manner, the stable umbrella framework 1 and the limiting bush 8 are sleeved along the connecting ring 6 in a matched manner, and the limiting bush 8 is used for limiting the stable umbrella framework 1 at two ends.
The connecting ring 6 is provided with an opening, so that the penetration of the stable umbrella framework 1, the double-head threaded sleeve 7, the limiting bushing 8 and the connecting lifting lug 9 is facilitated, the integral connecting ring 6 can effectively provide the connection of the stable umbrella framework 1, and a connecting space of the double frameworks is reserved; the limiting bushing 8 can ensure the stable position of the stable umbrella framework 1, replaces the structures of the retainer 2 and the fixed ring 3, and reduces the structural volume and the weight; the connecting lifting lug 9 has the advantages of small volume, light weight and the like relative to the retainer 2 and the fixed ring 3.
In the present embodiment, as shown in fig. 6, the ear hole is located at the upper portion of the connecting shackle 9, and the lower portion of the connecting shackle 9 is connected to the filler neck 4 through a screw hole.
In this embodiment, the threads at the two ends of the connecting ring 6 are opposite to each other; the connecting ring 6 is made of high-strength steel; the limiting bushing 8 is matched with the radian of the connecting ring 6 in the axial direction.
It will be understood that modifications and variations will be apparent to those skilled in the art from the foregoing description, and it is intended that all such modifications and variations be included within the scope of the following claims.

Claims (5)

1. The utility model provides a stable umbrella skeleton connection structure of flexible pipe joint refuels which characterized in that: including connecting lug (9), go-between (6), double-end swivel nut (7), stable umbrella skeleton (1) and spacing bush (8), connect lug (9) along circumference distribution on fuelling joint (4), go-between (6) have the opening and both ends are equipped with the screw thread, go-between (6) complex passes the earhole of whole circle connection lug (9), double-end swivel nut (7) are located go-between (6) opening part and screw thread fit's cover at go-between (6) both ends, stable umbrella skeleton (1) and spacing bush (8) all complex cover are along the go-between (6), spacing bush (8) are used for spacing stable umbrella skeleton (1) at both ends.
2. A fuel filler hose connector stabilizer rib attachment structure as defined in claim 1, wherein: the earhole is positioned at the upper part of the connecting lifting lug (9), and the lower part of the connecting lifting lug (9) is connected with the oiling joint (4) through a threaded hole.
3. A fuel filler hose connector stabilizer rib attachment structure as defined in claim 1, wherein: the threads at the two ends of the connecting ring (6) are opposite to each other.
4. A fuel filler hose connector stabilizer rib attachment structure as defined in claim 1, wherein: the connecting ring (6) is made of high-strength steel.
5. A fuel filler hose connector stabilizer rib attachment structure as defined in claim 1, wherein: the axial direction of the limiting bushing (8) is matched with the radian of the connecting ring (6).
CN202111002641.7A 2021-08-30 2021-08-30 Stable umbrella framework connecting structure of oiling hose connector Active CN113602509B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111002641.7A CN113602509B (en) 2021-08-30 2021-08-30 Stable umbrella framework connecting structure of oiling hose connector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111002641.7A CN113602509B (en) 2021-08-30 2021-08-30 Stable umbrella framework connecting structure of oiling hose connector

Publications (2)

Publication Number Publication Date
CN113602509A CN113602509A (en) 2021-11-05
CN113602509B true CN113602509B (en) 2023-10-10

Family

ID=78309666

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111002641.7A Active CN113602509B (en) 2021-08-30 2021-08-30 Stable umbrella framework connecting structure of oiling hose connector

Country Status (1)

Country Link
CN (1) CN113602509B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115783337A (en) * 2023-02-09 2023-03-14 中国空气动力研究与发展中心空天技术研究所 Active taper sleeve for aerial recovery of unmanned aerial vehicle

Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB232754A (en) * 1924-03-28 1925-04-30 Charles Frederick Love Improved means for locking the rib-carrying sleeve of an umbrella or the like to the handle stick
FR839974A (en) * 1937-06-29 1939-04-17 Parachute training
GB782788A (en) * 1954-09-23 1957-09-11 Richard Fred Patterson Drogue construction
US3048357A (en) * 1961-03-23 1962-08-07 Alfred C Loedding Winglet drogue for aerial refueling
US5871173A (en) * 1995-10-13 1999-02-16 Gec-Marconi Limited Drag-producing aerodynamic device
US5911233A (en) * 1998-03-18 1999-06-15 Wu; Tzun-Zong Safety umbrella runner
US5921294A (en) * 1998-03-04 1999-07-13 The United States Of America As Represented By The Secretary Of The Navy Air refueling drogue
CN1252033A (en) * 1997-03-04 2000-05-03 飞行添加燃料有限公司 Drogue assembly for in-flight refuelling
DE202004004350U1 (en) * 2003-03-21 2004-05-19 Chen, Fengchun Portable large umbrella
CN2799003Y (en) * 2005-06-10 2006-07-26 王文祥 Umbrella for fleeing from storied building
US7152828B1 (en) * 2002-11-01 2006-12-26 Sargent Fletcher, Inc. Method and apparatus for the hookup of unmanned/manned (“hum”) multi purpose vehicles with each other
TWM328809U (en) * 2007-08-24 2008-03-21 Urbane Brothers Corp Improved structure of umbrella
US7406976B1 (en) * 2007-03-29 2008-08-05 Chiaphua Components Limited Winch-actuated umbrella
CN203126453U (en) * 2013-03-01 2013-08-14 重庆北奔汽车有限公司 Connecting structure for stabilizer bar and stabilizer bar bushing
CN106005436A (en) * 2016-08-06 2016-10-12 赵世龙 Stabilizing parachute
CN106207483A (en) * 2016-06-29 2016-12-07 西安空间无线电技术研究所 A kind of multi-fold umbrella reflector
CN212637924U (en) * 2020-06-23 2021-03-02 中国空气动力研究与发展中心低速空气动力研究所 Self-adaptive variable-resistance stabilizing umbrella
CN112591117A (en) * 2020-12-30 2021-04-02 航宇救生装备有限公司 Full speed variable resistance characteristic refueling hose joint stabilizing umbrella
CN112957630A (en) * 2021-02-05 2021-06-15 首都经济贸易大学 Directional cross-country auxiliary rescue equipment

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6512726B2 (en) * 2015-03-26 2019-05-15 アロヴィア,インコーポレイテッド Automatic pop-up display device
WO2017178042A1 (en) * 2016-04-12 2017-10-19 Royal Botania A strutless umbrella frame for supporting a canopy

Patent Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB232754A (en) * 1924-03-28 1925-04-30 Charles Frederick Love Improved means for locking the rib-carrying sleeve of an umbrella or the like to the handle stick
FR839974A (en) * 1937-06-29 1939-04-17 Parachute training
GB782788A (en) * 1954-09-23 1957-09-11 Richard Fred Patterson Drogue construction
US3048357A (en) * 1961-03-23 1962-08-07 Alfred C Loedding Winglet drogue for aerial refueling
US5871173A (en) * 1995-10-13 1999-02-16 Gec-Marconi Limited Drag-producing aerodynamic device
CN1252033A (en) * 1997-03-04 2000-05-03 飞行添加燃料有限公司 Drogue assembly for in-flight refuelling
US5921294A (en) * 1998-03-04 1999-07-13 The United States Of America As Represented By The Secretary Of The Navy Air refueling drogue
US5911233A (en) * 1998-03-18 1999-06-15 Wu; Tzun-Zong Safety umbrella runner
US7152828B1 (en) * 2002-11-01 2006-12-26 Sargent Fletcher, Inc. Method and apparatus for the hookup of unmanned/manned (“hum”) multi purpose vehicles with each other
DE202004004350U1 (en) * 2003-03-21 2004-05-19 Chen, Fengchun Portable large umbrella
CN2799003Y (en) * 2005-06-10 2006-07-26 王文祥 Umbrella for fleeing from storied building
US7406976B1 (en) * 2007-03-29 2008-08-05 Chiaphua Components Limited Winch-actuated umbrella
TWM328809U (en) * 2007-08-24 2008-03-21 Urbane Brothers Corp Improved structure of umbrella
CN203126453U (en) * 2013-03-01 2013-08-14 重庆北奔汽车有限公司 Connecting structure for stabilizer bar and stabilizer bar bushing
CN106207483A (en) * 2016-06-29 2016-12-07 西安空间无线电技术研究所 A kind of multi-fold umbrella reflector
CN106005436A (en) * 2016-08-06 2016-10-12 赵世龙 Stabilizing parachute
CN212637924U (en) * 2020-06-23 2021-03-02 中国空气动力研究与发展中心低速空气动力研究所 Self-adaptive variable-resistance stabilizing umbrella
CN112591117A (en) * 2020-12-30 2021-04-02 航宇救生装备有限公司 Full speed variable resistance characteristic refueling hose joint stabilizing umbrella
CN112957630A (en) * 2021-02-05 2021-06-15 首都经济贸易大学 Directional cross-country auxiliary rescue equipment

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
加油机伞抗撞击性能仿真;胡斌;黄其青;周昊;;航空制造技术(第23期);全文 *
周学.加油机稳定伞可变阻力特征技术研究.第六届中国航空学会青年科技论坛.2014,全文. *
国外空中加油技术的现状及发展;徐干,曹近齐;航空科学技术(第01期);全文 *

Also Published As

Publication number Publication date
CN113602509A (en) 2021-11-05

Similar Documents

Publication Publication Date Title
CN113602509B (en) Stable umbrella framework connecting structure of oiling hose connector
CN104691746A (en) Single-wheel strut landing gear structure for large wingspan lightweight unmanned aerial vehicle
CN216611582U (en) Unmanned aerial vehicle wing and unmanned aerial vehicle
CN112623182B (en) Wing body connection structure and contain wing body connection structure's unmanned aerial vehicle
CN214523226U (en) Universal trailer towing bar for special vehicle
CN211684561U (en) Stabilizer bar connecting rod mounting structure
CN219565211U (en) Steering wheel assembly convenient to install
CN208021703U (en) A kind of two degrees of freedom guide rope device for captive balloon
CN112591073A (en) Wing body combines to connect and unmanned aerial vehicle
EP3756905A1 (en) Lightweight wheels and automobile
CN111731492A (en) Fuel tank of aircraft
CN214404293U (en) Waterproof durable flange nut
CN218907585U (en) Aircraft fuselage jack nest and tethered joint integrated structure
CN102923558B (en) Combined airplane lifting lug
CN204976515U (en) Car torsion roof beam bush assembly fixture
CN207417170U (en) A kind of adapter assembly
CN215411736U (en) Stage lighting protective structure
CN214505231U (en) Pluggable high-voltage bushing capable of being installed quickly
CN220555979U (en) Engine air inlet pipe
CN217003020U (en) Dedicated derailleur oil drain bolt sleeve of heavy high maneuver tactics vehicle
CN214534436U (en) Metallurgical professional equipment accessory
CN110539599B (en) Assembled suspension control arm structure
CN209743809U (en) Leakage-free oil filling pipe assembly
CN109808419A (en) Shrinkable wheel
CN218316102U (en) Vehicle-mounted universal towing hook

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant