EP2586707A1 - Security locking device for the cowl of an engine pod - Google Patents
Security locking device for the cowl of an engine pod Download PDFInfo
- Publication number
- EP2586707A1 EP2586707A1 EP20110382332 EP11382332A EP2586707A1 EP 2586707 A1 EP2586707 A1 EP 2586707A1 EP 20110382332 EP20110382332 EP 20110382332 EP 11382332 A EP11382332 A EP 11382332A EP 2586707 A1 EP2586707 A1 EP 2586707A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- locking device
- security locking
- fan cowl
- security
- indication device
- 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
- 238000012423 maintenance Methods 0.000 description 7
- 230000000007 visual effect Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000011179 visual inspection Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B41/00—Locks with visible indication as to whether the lock is locked or unlocked
Definitions
- the present invention relates to a security locking device for assuring a correct closure of the fan cowl doors of an aircraft power unit nacelle.
- the security locking device of the invention comprises security locking means providing the security alternative latch of the indication device, as these security locking means close automatically over the fan cowl locking means, without the need of further operation on the part of the maintenance personnel. Therefore, the indication device can be fixed by the primary locking device and also by security locking means such that, even if the primary locking device does not properly latch the indication device over the fan cowl doors, the security locking means assure that the indication device is latched over the fan cowl doors, as the security locking means are latched without the need of being operated.
- a security locking device 100 is provided, providing security alternative latching for the correct latch of the cited indication device 40.
- the security locking device 100 of the invention comprises security locking means 102.
- the primary locking device 101 engages the panel 41 of the indication device 40 on one of the fan cowl doors 10 or 20 by rotating on the mentioned rotating means 42, such that the panel 41, once it is engaged by the primary locking device 101, covers at least partially the fan cowl locking means 30.
- the primary locking device 101 is designed having an equilibrated and aligned engaged status, also being of easy and friendly manipulation for the maintenance personnel.
- the security locking means 102 of the invention give a further security latch, preventing the detachment of the panel 41 in the indication device 40 in the case in which primary locking device 101 is not properly latched on the fan cowl door 10 or 20.
- the security locking device 100 in the indication device 40 according to the invention is located next to the primary locking device 101 on the side of the panel 41 facing incoming airflow 90 during flight of the aircraft.
- This security locking device 100 operates when the primary locking device 101 is not working properly (that is, when the primary locking device 101 is not properly latched), so that the security locking device 100 has to ensure that the airflow 90 which enters the region between the fan cowl doors 10, 20 and the panel 41 of the indication device 40 is minimized. This is achieved by ensuring that there is no space between the panel 41 in its closed position and the fan cowl doors 10, 20 on the side facing the incoming airflow 90.
Abstract
Description
- The present invention relates to a security locking device for assuring a correct closure of the fan cowl doors of an aircraft power unit nacelle.
- An aircraft having a power unit supported in the airframe mounted configuration comprises an engine and a nacelle structure housing said engine. The nacelle structure comprises two displaceable parts called fan cowl doors or cowlings which can be opened on the ground during maintenance operations to access the various items of the power unit, the cowlings or fan cowl doors being closed and properly latched during operational conditions of the aircraft, therefore providing aerodynamic continuity for the power unit in flight.
- The nacelle usually comprises fan cowl locking means fixing and latching the fan cowl doors during operation of the aircraft.
- The indication of fan cowl doors not being properly latched is not usually a signal that is sent to the cockpit to avoid false open-door signals. For this reason, a visual inspection of the nacelle is necessary to detect if fan cowl doors are not properly latched.
- Therefore, it is necessary to provide a warning signal with high visibility when the fan cowl doors of an aircraft are not properly latched or locked. For this reason, apart from the fan cowl locking means that fix and latch the fan cowl doors, an indication device is also provided for indicating if these fan cowl locking means are not properly latched. This indication device comprises a panel fixed by rotating means on one of the two fan cowlings, the panel being closed on that one fan cowling by means of several primary locking means by rotating on said rotating means, therefore covering at least partially the fan cowl locking means of the fan cowl doors, such that all the fan cowl locking means have to be properly latched for the panel being closed. If the device is not closed, therefore being the fan cowl locking means not properly latched, the panel hangs vertically from the fan cowl door, providing a high visibility warning signal of the aircraft fan cowl doors not being properly latched or locked. This system is known from document
EP 09784126.6, filed on 9 July, 2009 - However, sometimes the indication device (panel) is not properly latched by its primary locking means along its length, due to pollution (paint or stickers) on the primary locking means, therefore preventing a correct closure of said primary locking means, or because the maintenance personnel operating these latches (primary locking means) are not familiar with them, as these means are not easy to manipulate. Due to these reasons, the indication device (panel) hangs vertically during flight, therefore being blown or torn away in many occasions, as it is not properly latched. It is therefore desirable to prevent the indication device from being lost.
- It is known from document
US 4,531,769 a latch for securing together a pair of hinged cowlings of an aircraft engine, this latch comprising a hook, a hook keeper and a safety lock, such that the safety lock engages the hook in the hook keeper when the latch is in a closed position, engaging the cowlings, and such that the safety lock engages the hook when the latch is in an open position, the cowlings being disengaged. The problem of this known solution is that it is difficult to manipulate and that, for the system to work properly, it is necessary to have an equilibrated and balanced position of the hook keeper and hook, occurring that sometimes, as the vibrations in these parts of the aircraft are very high, it may occur that a misalignment happens with the consequent default in the engaging of the latch, so the cowlings are not properly closed. - It is known from document
US 5,620,212 a hook latch mechanism for joining two members of an engine cowl, comprising a hook latch mechanism on of the members to be joined and a keeper together with a mounting bolt, carried in the second member engaged. This system has the problem of possible misalignment between the bolt and the hook, therefore causing that the latch mechanism is not properly secured. Besides, this mechanism can sometimes be not properly latched due to pollution in the mechanism or due to the maintenance personnel not being familiar with the operation of these systems. - The present invention is oriented to the solution of the above-mentioned drawbacks.
- The present invention relates to a security locking device for assuring a correct closure of the fan cowl doors of an aircraft power unit nacelle.
- The fan cowl doors of the nacelle structure of an aircraft housing an engine are closed when the aircraft is in flight by means of fan cowl locking means. Besides, in order to have a visual indication of these fan cowl doors being properly latched, an indication device, rotating over rotating means located in one of the two fan cowl doors, is provided, such that this indication device comprises a panel fixed on one of the two fan cowl doors by means of a primary locking device, such that, by rotating the panel on the rotating means the panel is latched over the fan cowl doors, covering at least partially the fan cowl locking means. According to the invention, a security locking device is provided, providing security alternative latching for the cited indication device.
- The security locking device of the invention comprises security locking means providing the security alternative latch of the indication device, as these security locking means close automatically over the fan cowl locking means, without the need of further operation on the part of the maintenance personnel. Therefore, the indication device can be fixed by the primary locking device and also by security locking means such that, even if the primary locking device does not properly latch the indication device over the fan cowl doors, the security locking means assure that the indication device is latched over the fan cowl doors, as the security locking means are latched without the need of being operated.
- The primary locking device fixes the panel of the indication device on one of the fan cowl doors by rotating on the mentioned rotating means, such that the panel, once it is closed, covers at least partially the fan cowl locking means of the fan cowl doors. This primary locking device is designed having an equilibrated and aligned engaged status, also being of easy and friendly manipulation for the maintenance personnel. The security locking means give a further security latch for the indication device, preventing the detachment of the panel in the indication device in the case in which the primary locking device is not actuating properly, that is, in the case in which the primary locking device is not properly latched on the fan cowl door.
- Other features and advantages of the present invention will be disclosed in the following detailed description of an illustrative embodiment of its object in relation to the attached figures.
-
-
Figures 1 a and 1b show the location of the fan cowl doors in a typical aircraft nacelle configuration. -
Figures 2a and 2b show schematically the location of the fan cowl locking means according to the prior art in the fan cowl configuration of an aircraft. -
Figure 3 shows an indication device, according to the known prior art, being latched over the fan cowl doors by a primary locking device. -
Figure 4 shows a perspective view from the inside of the fan cowl doors of the part of the primary locking device located on the panel of the indication device, according to the known prior art. -
Figure 5 shows a perspective view from the inside of the fan cowl doors of the primary locking device and the security locking means when the indication device is in a closed position in an aircraft power unit nacelle according to the invention. -
Figures 6a and6b show perspective views of the inside of the fan cowl doors of the part of the security locking means located on the panel of the indication device and located on the fan cowl doors, respectively. -
Figures 7a ,7b and 7c show different views of the part of the security locking means located in the indication device, for the fan cowl doors of an aircraft power unit nacelle according to the present invention. -
Figures 8a and 8b show different views of the part of the security locking means located in the fan cowl doors, for the fan cowl doors of an aircraft power unit nacelle according to the present invention. -
Figure 9 shows a plan view of the panel of an indication device according to the known prior art. -
Figure 10 shows a plan view of the panel of the indication device on which the security locking device of the present invention is located, this panel being thicker than the panel used in the prior art, as a primary locking device and a security locking device are comprised in it.. -
Figure 11 shows a plan view of the fan cowl door over which a panel with an indication device according to the known prior is engaged. -
Figure 12 shows a plan view of the fan cowl door over which a panel with a security locking device according to the invention is engaged. -
Figures 13 shows a schematic view of the indication device comprising a primary locking device and security locking means according to the invention, subjected to an air flow in flight. -
Figure 14a shows a schematic view of the indication device according to the prior art closed by its primary locking device, in its nominal closed position. -
Figure 14b shows a schematic view of the indication device according to the prior art closed by a security locking device according to the present invention, in the position in which the panel load is supported by said security locking device according to the present invention. -
Figure 14c shows a schematic view of the indication device according to the present invention closed by the security locking device according to the present invention, in the position in which the panel load is supported by said security locking device according to the present invention. - The present invention relates to a security locking device 100 for assuring a correct closure of the
fan cowl doors - According to the known prior art, as it can be seen in
Figures 1a, 1b ,2a 2b and3 , thefan cowl doors fan cowl doors indication device 40 is provided, such that thisindication device 40 comprises apanel 41 fixed by rotatingmeans 42 on one of the twofan cowl doors panel 41 is fixed on one of thefan cowl doors primary locking device 101. - According to the invention, a security locking device 100 is provided, providing security alternative latching for the correct latch of the cited indication device 40.The security locking device 100 of the invention comprises security locking means 102. The
primary locking device 101 engages thepanel 41 of theindication device 40 on one of thefan cowl doors rotating means 42, such that thepanel 41, once it is engaged by theprimary locking device 101, covers at least partially the fan cowl locking means 30. Theprimary locking device 101 is designed having an equilibrated and aligned engaged status, also being of easy and friendly manipulation for the maintenance personnel. The security locking means 102 of the invention give a further security latch, preventing the detachment of thepanel 41 in theindication device 40 in the case in whichprimary locking device 101 is not properly latched on thefan cowl door - The security locking means 102 of the invention act as a safety device, providing a positive lock or latch of the
panel 41 over thefan cowl door panel 41, when thispanel 41 is slammed without any further operation or actuation. Therefore, the security locking device 100of the invention avoids possible failures in cases where the fan cowl locking means 30 or theprimary locking device 101 are not properly latched, as the security locking means 102 are latched automatically as thepanel 41 in theindication device 40 is closed, without the need of further operation on the part of the maintenance personnel. The security locking means 102 comprise engagingmeans 50 located in thepanel 41 engaging with receivingmeans 60 located in the fan cowl doors, 10 or 20 (seeFigures 6a and6b ). - The
primary locking device 101 will preferably have a design based on a pressure relief latch design, comprising an opening 6, typically a slot, than can be operated by means of a screwdriver, and adjusting means 7, typically a bolt, for setting the grip of thepanel 41, preferably varying from 7 mm up to 12 mm. The kinematics of theprimary locking device 101 is such that it ensures no contact in neither the opening nor in the closing sequences of operation of thepanel 41 in the worst case of tolerances. - In a embodiment of the invention, the
engaging means 50 in the security locking means 102 comprise ahook 51 rotating around apin 52 bysupport bushings 53 and aspring 55, located on asupport 54 installed in the panel 41 (seeFigures 7a ,7b and 7c ). This configuration allows a maximum mechanical rotation of thehook 51 that is calculated so that it is limited in such a way that an extra rotation from the operation personnel would not damage the engagingmeans 50. Typically, the maximum mechanical rotation of thehook 51 is of about 30°. The value of the elastic constant K of thespring 55 and thehook 51 inertia are selected such that the resonance frequency has a different value than the oscillation frequency of the engine, therefore avoiding coupling in frequencies with the engine. Preferably, the value of the elastic constant K of thespring 55 and the value of thehook 51 inertia are selected such that they avoid resonance frequencies under about 60 Hz. - The receiving means 60 located in the fan cowl doors, 10 or 20, comprise a catching
element 61, preferably an axis or mounting bolt, over which thehook 51 engages, this catchingelement 61 being fixed to abracket 63 by bushings 62 (seeFigures 8a and 8b ). - According to the invention, the cut-out of the
fan cowl door panel 41 is engaged by means of the security locking device100, has to be increased circumferentially in order to accommodate both theprimary locking device 101 and the security locking means 102 (seeFigures 11 and12 ), the surrounding parts in the fan cowl being modified accordingly, and the attaching points for the lightning protection being also consequently relocated. - As it can be seen in
Figure 10 , thepanel 41 comprises a new cut-out 205 for accommodating the security locking means 102. Furthermore, anew strip 200 is preferably provided, apart from thestrip parts panel 41 is locally increased, around the area where the security locking device 100 is located, avoiding possible gaps between thepanel 41 and thefan cowl doors panel 41. - The security locking device 100 in the
indication device 40 according to the invention is located next to theprimary locking device 101 on the side of thepanel 41 facingincoming airflow 90 during flight of the aircraft. The reason for this is that this security locking device 100 operates when theprimary locking device 101 is not working properly (that is, when theprimary locking device 101 is not properly latched), so that the security locking device 100 has to ensure that theairflow 90 which enters the region between thefan cowl doors panel 41 of theindication device 40 is minimized. This is achieved by ensuring that there is no space between thepanel 41 in its closed position and thefan cowl doors incoming airflow 90. -
Figure 14a , represents anindication device 40 with apanel 41 according to the known prior art, thepanel 41 being closed by a primary locking device 101: this Figure shows theprimary locking device 101 in its nominal closed position over thefan cowl doors panel 41 and thefan cowl doors airflow 90. - The security locking device 100 of the invention is therefore designed so that it only supports the load of the
panel 41 when theprimary locking device 101 is not properly latching thepanel 41, so thepanel 41 is either supported by theprimary locking device 101 or by the security locking means 102. As the security locking means 102 are a security measure, they are located in such a way that thehook 51 and the catchingelement 61 only enter into contact when thepanel 41 falls from its nominal position (where it is latched to thefan cowl doors panel 41 of theindication device 40, when thispanel 41 is supported by the security locking means 102, juts out from the aerodynamic surface of thefan cowl doors Figure 14b . To avoid any flow of air from theairflow 90 from entering the space between thefan cowl doors panel 41, thepanel 41 is thickened locally, around the area where the security locking device 100 is located, as it is clearly represented inFigure 14c . - The security locking means 102 are preferably located, together with the
primary locking device 101, close to the edge of the indication device 40 (panel 41) facing the airflow 90.The reason is that the incorrect closure of theprimary locking device 101 is what causes the existence of a gap between thepanel 41 and thefan cowl doors airflow 90 makes thepanel 41 and theindication device 40 lift up and get lost in flight. - Modifications comprised within the scope defined by the following claims can be introduced in the preferred embodiments which have just been described.
Claims (13)
- Security locking device(100) for an indication device (40), the indication device (40) providing a warning signal when the fan cowl doors (10, 20) on an aircraft power unit nacelle are not properly latched, the indication device (40) being latched to the fan cowl doors by a primary locking device (101), characterized in that the security locking device (100)comprises security locking means (102) providing a security alternative latch of the indication device (40) over the fan cowl doors (10, 20), such that the security locking means (102) are latched only by closing the indication device (40) over the fan cowl doors (10, 20), without the need of any further operation.
- Security locking device (100) according to claim 1, located close to the edge of the indication device (40) facing an airflow (90).
- Security locking device (100) according to any of claims 1-2, wherein the security locking means (102) comprise engaging means (50) and receiving means (60), the engaging means (50) being located in the indication device (40) and engaging with the receiving means (60) located in the fan cowl doors (10, 20).
- Security locking device (100) according to claim 3, wherein the engaging means (50) comprise a hook (51) and a spring (55), such that the value of the elastic constant (K) of the spring (55) and the value of the hook (51) inertia are selected such that they avoid the resonance frequencies of the aircraft engine.
- Security locking device (100) according to claim 4, wherein the value of the elastic constant (K) of the spring (55) and the value of the hook (51) inertia are selected such that they avoid resonance frequencies under 60 Hz.
- Security locking device (100) according to any of claims 4-5, wherein the maximum mechanical rotation of the hook (51) is calculated so that it is limited in such a way that an extra rotation from the operation personnel would not damage the engaging means (50).
- Security locking device (100) according to claim 6, wherein the maximum rotation of the hook (51) is of 30°.
- Security locking device (100) according to any of the preceding claims, wherein the indication device (40) comprises a panel (41) having increased thickness locally, around the area where the security locking device (100) is located.
- Security locking device (100) according to any of claims 3-8, wherein the receiving means (60) comprise a catching element (61), over which the hook (51) engages, the catching element (61) being an axis or a mounting bolt.
- Security locking device (100) according to any of the preceding claims, designed in such a way that it only supports the load of the indication device (40) in the case in which the primary locking device (101) is not properly latching the indication device (40).
- Fan cowl doors for an aircraft power unit comprising a security locking device (100) according to any of claims 1-10.
- Aircraft comprising an indication device (40) providing a warning signal when the fan cowl doors (10, 20) on the aircraft power unit nacelle are not properly latched, such that it also comprises a security locking device (100) according to any of claims 1-10.
- Aircraft according to claim 12, wherein the security locking device (100) comprises a hook (51) and a spring (55), the elastic constant (K) of the spring (55) and the inertia of the hook (51) being selected such that they avoid the resonance frequencies of the aircraft engine.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES11382332.2T ES2569127T3 (en) | 2011-10-27 | 2011-10-27 | Safety lock for the gondola hood of an aircraft power unit |
EP11382332.2A EP2586707B1 (en) | 2011-10-27 | 2011-10-27 | Security locking device for the cowl of an engine pod |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11382332.2A EP2586707B1 (en) | 2011-10-27 | 2011-10-27 | Security locking device for the cowl of an engine pod |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2586707A1 true EP2586707A1 (en) | 2013-05-01 |
EP2586707B1 EP2586707B1 (en) | 2016-01-20 |
Family
ID=45063073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11382332.2A Active EP2586707B1 (en) | 2011-10-27 | 2011-10-27 | Security locking device for the cowl of an engine pod |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2586707B1 (en) |
ES (1) | ES2569127T3 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015010271A1 (en) * | 2013-07-24 | 2015-01-29 | Mra Systems, Inc. | Engine door and latch assembly |
WO2017058860A1 (en) * | 2015-09-30 | 2017-04-06 | Alcoa Inc. | Pressure relief door |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4531769A (en) | 1982-08-25 | 1985-07-30 | The Boeing Company | Hook latch for an engine cowling |
US5620212A (en) | 1995-08-28 | 1997-04-15 | Hartwell Corporation | Low profile hook latch assembly |
EP1091059A2 (en) * | 1999-10-05 | 2001-04-11 | Hartwell Corporation | Latch with sensor providing visual indication of the latch position |
EP1270406A2 (en) * | 2001-06-20 | 2003-01-02 | Hartwell Corporation | Blowout latch |
US20040104583A1 (en) * | 2001-11-27 | 2004-06-03 | Alain Porte | Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle |
FR2916425A1 (en) * | 2007-05-25 | 2008-11-28 | Aircelle Sa | DEVICE FOR LOCKING AN OPENING PART OF A TURBOJET NACELLE WITH RESPECT TO A FIXED PART, AND A NACELLE COMPRISING SUCH A DEVICE |
EP2348171A1 (en) * | 2010-01-21 | 2011-07-27 | Eurocopter | Device for locking a structural element against an adjacent structure, aircraft equipped with said device and extraction method implemented by said device |
-
2011
- 2011-10-27 EP EP11382332.2A patent/EP2586707B1/en active Active
- 2011-10-27 ES ES11382332.2T patent/ES2569127T3/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4531769A (en) | 1982-08-25 | 1985-07-30 | The Boeing Company | Hook latch for an engine cowling |
US5620212A (en) | 1995-08-28 | 1997-04-15 | Hartwell Corporation | Low profile hook latch assembly |
EP1091059A2 (en) * | 1999-10-05 | 2001-04-11 | Hartwell Corporation | Latch with sensor providing visual indication of the latch position |
EP1270406A2 (en) * | 2001-06-20 | 2003-01-02 | Hartwell Corporation | Blowout latch |
US20040104583A1 (en) * | 2001-11-27 | 2004-06-03 | Alain Porte | Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle |
FR2916425A1 (en) * | 2007-05-25 | 2008-11-28 | Aircelle Sa | DEVICE FOR LOCKING AN OPENING PART OF A TURBOJET NACELLE WITH RESPECT TO A FIXED PART, AND A NACELLE COMPRISING SUCH A DEVICE |
EP2348171A1 (en) * | 2010-01-21 | 2011-07-27 | Eurocopter | Device for locking a structural element against an adjacent structure, aircraft equipped with said device and extraction method implemented by said device |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015010271A1 (en) * | 2013-07-24 | 2015-01-29 | Mra Systems, Inc. | Engine door and latch assembly |
CN105378201A (en) * | 2013-07-24 | 2016-03-02 | Mra系统有限公司 | Engine door and latch assembly |
CN105378201B (en) * | 2013-07-24 | 2017-09-15 | Mra系统有限责任公司 | Start gate and latch assembly |
US11060331B2 (en) | 2013-07-24 | 2021-07-13 | Mra Systems, Llc | Engine door and latch assembly |
WO2017058860A1 (en) * | 2015-09-30 | 2017-04-06 | Alcoa Inc. | Pressure relief door |
US10240389B2 (en) | 2015-09-30 | 2019-03-26 | Arconic Inc. | Pressure relief door |
Also Published As
Publication number | Publication date |
---|---|
ES2569127T3 (en) | 2016-05-06 |
EP2586707B1 (en) | 2016-01-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103168143B (en) | Locking device with mechanical detection of closing and opening | |
US6824175B2 (en) | Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle | |
US5518206A (en) | Closure default indicator | |
US9701413B2 (en) | Locking device with mechanical detection of closure and opening | |
RU2500586C2 (en) | Turbojet nacelle air intake lock system | |
EP3115562B1 (en) | Pressure relief door assembly | |
US9624790B2 (en) | Fan cowl locking system | |
EP3339181B1 (en) | Apparatuses and methods for cowl latch indication | |
US7204458B2 (en) | Closing system interposed between two elements | |
US20100314501A1 (en) | Locking system for air intake structure for turbojet engine nacelle | |
CN103967373B (en) | Aircraft electronic hatch door safety control system and control method thereof | |
US11685538B2 (en) | Propulsion unit for an aircraft, connected to the fuselage of said aircraft | |
GB2481523A (en) | Ram air turbine with locking support structure | |
US20160201371A1 (en) | Quick release hinge | |
US20050082433A1 (en) | Cockpit door of aircraft | |
EP2314509B1 (en) | Device for an aircraft propulsion unit | |
EP2586707B1 (en) | Security locking device for the cowl of an engine pod | |
US10710736B2 (en) | Latch indication system and method for a fan cowl of an air vehicle | |
EP3650334B1 (en) | Pressure relief assembly | |
CN109306827A (en) | Cabin door open and close error protection mechanism | |
GB2267122A (en) | Closure fault indicator | |
EP3747774B1 (en) | Latch and method for operating said latch | |
US20220267018A1 (en) | High visibility hook latch | |
CN215803929U (en) | Inside hatch door stop device of cargo airplane | |
CN220054132U (en) | Automatic locking and opening warning device for nacelle fairing of aircraft engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
17P | Request for examination filed |
Effective date: 20131104 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
17Q | First examination report despatched |
Effective date: 20131220 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20150724 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: AIRBUS DEFENCE AND SPACE SA |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 771590 Country of ref document: AT Kind code of ref document: T Effective date: 20160215 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602011022787 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2569127 Country of ref document: ES Kind code of ref document: T3 Effective date: 20160506 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D Ref country code: NL Ref legal event code: MP Effective date: 20160120 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 771590 Country of ref document: AT Kind code of ref document: T Effective date: 20160120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160421 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160420 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160520 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160520 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602011022787 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
26N | No opposition filed |
Effective date: 20161021 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160420 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161027 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161027 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20111027 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 Ref country code: MT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160120 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231020 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20231227 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231025 Year of fee payment: 13 Ref country code: DE Payment date: 20231020 Year of fee payment: 13 |