IP Library Granted Patent US 8,322,670
Granted Patent B2
US 8,322,670 · App. 12/750,205 · Granted Dec 4, 2012

Deployment apparatuses

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Quick Facts
Patent No.
US 8,322,670
App. No.
12/750,205
Granted
Dec 4, 2012
Kind
B2
Abstract

Embodiments of the present invention include a deployment apparatus comprising a deployment object, a deployment arm, a deployment link, a pivot housing, at least two linear guides, and a gas spring. The deployment object is coupled to the deployment arm, which is pivotally coupled to the deployment link. An opposing end of the deployment link is fixedly coupled to a structure. The pivot housing is adjacent the connection between the deployment link and the deployment arm. The pivot housing is slidingly engaged with the at least two linear guides. The gas spring is coupled to the pivot housing, which pushes the pivot housing to an upper end of the at least two linear guides and causes the deployment link to rotate the deployment arm from a stowed angle to a released angle and results in a displaced vertical distance.

Claims (17)

1. A method of deploying a deployment apparatus, wherein the deployment apparatus comprises (i) a deployment object, (ii) a deployment arm coupled to the deployment object, (iii) a deployment link, wherein an end of the deployment link comprises a mating surface that confronts a mating surface of the deployment arm and an opposing end of the deployment link is coupled in a fixed location to a deployment arm mount, (iv) a pivot housing, wherein the pivot housing is adjacent the mating surfaces of the deployment link and the deployment arm, and (v) at least two linear guides, wherein the at least two linear guides are coupled to the deployment arm mount and comprise at least two tracks that are slidingly engaged with a plurality of linear bearings on the surface of the pivot housing, comprising the steps of:

a. providing a gas spring, wherein the gas spring is coupled at one end to the pivot housing and coupled at an opposing end to the deployment arm mount;

b. providing a locking arm, wherein the locking arm is releasably coupled to a latch pin positioned on the deployment arm;

c. releasing the latch pin from the locking arm;

d. releasing the gas spring;

e. raising the pivot housing to an upper end of the at least two linear guides;

f. providing a rotation limiting pin, wherein the rotation limiting pin is coupled to the mating surface of the deployment arm;

g. positioning the deployment link adjacent the rotation limiting pin; and

h. rotating the deployment arm from a stowed angle to a released angle, wherein the stowed angle is an angle formed between the deployment arm and a vertical axis, and wherein the released angle is an angle formed between the deployment arm and the stowed angle.

2. The method of claim 1 , wherein the stowed angle has a range of 0 to 90 degrees.

3. The method of claim 1 , wherein the released angle is at least 10 degrees from the stowed angle.

4. The method of claim 1 , further comprising the steps of:

i. providing a spring coupled to an end of the locking arm and a projection on the pivot housing; and

compressing the spring by raising the end of the locking arm to release the latch pin from the locking arm.

5. The method of claim 1 , wherein the deployment object is a member of the group consisting of a display monitor, a tray table, and a cocktail table.

6. The method of claim 1 , wherein the deployment apparatus has a displaced vertical distance of at least 0.5 inches.

7. The method of claim 1 , wherein the deployment apparatus has a displaced vertical distance of at least 1.5 inches.

Assignments (2)
CHANGE OF NAME Recorded Apr 4, 2019
From: ZODIAC SEATS US LLC
To: SAFRAN SEATS USA LLC
Reel/Frame 049535/0876 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 25, 2011
From: WESTERINK, RIK
To: WEBER AIRCRAFT LLC
Reel/Frame 026639/0151 →