Helicopter with Wing Augmented Lift
US-2018281936-A1 · Oct 4, 2018 · US
Droop panel linkage
US9079652B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9079652-B2 |
| Application number | US-201013699025-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 21, 2010 |
| Priority date | May 21, 2010 |
| Publication date | Jul 14, 2015 |
| Grant date | Jul 14, 2015 |
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- Title
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Abstract
Official abstract text for this publication.
A droop panel linkage for aircraft includes a lever arm, a main lever, a main tube and at least one drive strut. The lever arm is pivotally attached at a first end to a flap and is pivotally connected at a second end to a first end of the main lever. A second end of the main lever is provided with a first engagement element for engaging with a second engagement element incorporated into or associated with the main tube. The main tube is pivotally connected to a proximal end of the drive strut. A distal end of the drive strut is pivotally attached to the droop panel.
First claim
Opening claim text (preview).
The invention claimed is: 1. A droop panel linkage, comprising: a lever arm, a main lever, a main tube, and at least one drive strut, said lever arm is pivotally attached at a first end to a flap and is pivotally connected at a second end to a first end of the main lever, wherein a second end of said main lever is provided with a first engagement means for engaging with a second engagement means incorporated into or associated with the main tube, said main tube being pivot…
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Frequently asked questions
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- What does patent US9079652B2 cover?
- A droop panel linkage for aircraft includes a lever arm, a main lever, a main tube and at least one drive strut. The lever arm is pivotally attached at a first end to a flap and is pivotally connected at a second end to a first end of the main lever. A second end of the main lever is provided with a first engagement element for engaging with a second engagement element incorporated into or asso…
- Who is the assignee on this patent?
- Yue Haikou, Airbus Sas
- What technology area does this patent fall under?
- Primary CPC classification B64C9/04. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Jul 14 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).