ES2569127T3 - Safety lock for the gondola hood of an aircraft power unit - Google Patents
Safety lock for the gondola hood of an aircraft power unit Download PDFInfo
- Publication number
- ES2569127T3 ES2569127T3 ES11382332.2T ES11382332T ES2569127T3 ES 2569127 T3 ES2569127 T3 ES 2569127T3 ES 11382332 T ES11382332 T ES 11382332T ES 2569127 T3 ES2569127 T3 ES 2569127T3
- Authority
- ES
- Spain
- Prior art keywords
- gondola
- doors
- panel
- safety
- power unit
- 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
Links
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
Abstract
Unidad de potencia de una aeronave, que comprende: - puertas (10, 20) de una góndola, - medios de cierre de la góndola (30) para la fijación y el bloqueo de las puertas (10, 20) de la góndola, - un dispositivo de indicación (40) para proporcionar una señal de advertencia cuando las puertas (10, 20) de la góndola no estén adecuadamente bloqueadas, que comprende: o un panel (41) fijado sobre una de las puertas (10, 20) de la góndola, o un dispositivo de bloqueo primario (101) para la fijación del panel (41) a las puertas (10, 20) de la góndola, o unos medios de rotación (42) localizados en una de las puertas (10, 20) de la góndola para la rotación del panel (41) de modo que mediante la rotación del panel (41), éste se bloquea sobre las puertas (10, 20) de la góndola cubriendo parcialmente los medios de cierre de la góndola (30), caracterizado por - un cierre de seguridad (100) que comprende medios de bloqueo de seguridad (102) que proporcionan un bloqueo alternativo de seguridad del dispositivo de indicación (40) sobre las puertas (10, 20) de la góndola, donde los medios de bloqueo de seguridad (102) comprenden medios de acoplamiento (50) y medios de recepción (60), los medios de acoplamiento (50) estando localizados en el dispositivo de indicación (40) y acoplándose con los medios de recepción (60) localizados en las puertas de la góndola (10, 20), donde los medios de acoplamiento (50) comprenden un gancho rotativo (51) y un resorte (55), ambos localizados sobre un soporte instalado en el panel, los medios de seguridad (102) estando configurados de tal manera que estén cerrados sólo por el cierre del dispositivo de indicación (40) sobre las puertas (10, 20) de la góndola, sin necesidad de ninguna operación adicional.Power unit of an aircraft, comprising: - doors (10, 20) of a gondola, - means of closing the gondola (30) for fixing and blocking the doors (10, 20) of the gondola, - an indication device (40) for providing a warning signal when the doors (10, 20) of the gondola are not properly locked, comprising: or a panel (41) fixed on one of the doors (10, 20) of the gondola, or a primary locking device (101) for fixing the panel (41) to the doors (10, 20) of the gondola, or rotating means (42) located in one of the doors (10, 20 ) of the gondola for the rotation of the panel (41) so that by rotating the panel (41), it is locked on the doors (10, 20) of the gondola partially covering the gondola closing means (30) , characterized by - a safety lock (100) comprising security locking means (102) that provide an alternative locking of safety of the indicating device (40) on the doors (10, 20) of the gondola, where the safety locking means (102) comprise coupling means (50) and receiving means (60), the coupling means ( 50) being located in the indicating device (40) and engaging with the receiving means (60) located in the doors of the gondola (10, 20), where the coupling means (50) comprise a rotating hook (51) and a spring (55), both located on a support installed in the panel, the safety means (102) being configured such that they are closed only by the closing of the indicating device (40) on the doors (10, 20 ) of the gondola, without the need for any additional operation.
Description
Claims (1)
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 (1)
| Publication Number | Publication Date |
|---|---|
| ES2569127T3 true ES2569127T3 (en) | 2016-05-06 |
Family
ID=45063073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES11382332.2T Active ES2569127T3 (en) | 2011-10-27 | 2011-10-27 | Safety lock for the gondola hood of an aircraft power unit |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP2586707B1 (en) |
| ES (1) | ES2569127T3 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11060331B2 (en) | 2013-07-24 | 2021-07-13 | Mra Systems, Llc | Engine door and latch assembly |
| EP3356628B1 (en) * | 2015-09-30 | 2022-01-19 | Howmet Aerospace Inc. | Pressure relief door |
Family Cites Families (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 |
| US6279971B1 (en) * | 1999-10-05 | 2001-08-28 | Hartwell Corporation | Latch with sensor |
| US6755448B2 (en) * | 2001-06-20 | 2004-06-29 | Hartwell Corporation | Blowout latch |
| FR2832752B1 (en) * | 2001-11-27 | 2004-08-06 | Airbus France | DEVICE FOR INDICATING FAULT IN THE CLOSING OF AT LEAST ONE LOCKING MECHANISM INTERPOSED BETWEEN TWO ELEMENTS |
| FR2916425B1 (en) * | 2007-05-25 | 2009-07-03 | 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 |
| FR2955347B1 (en) * | 2010-01-21 | 2012-01-27 | Eurocopter France | DEVICE FOR LOCKING AN ELEMENT AGAINST AN ADJACENT AIRCRAFT STRUCTURE PROVIDED WITH SAID DEVICE AND EXTRACTION METHOD THEREFOR |
-
2011
- 2011-10-27 ES ES11382332.2T patent/ES2569127T3/en active Active
- 2011-10-27 EP EP11382332.2A patent/EP2586707B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| EP2586707A1 (en) | 2013-05-01 |
| EP2586707B1 (en) | 2016-01-20 |
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