In-flight leveling system

• US 9,884,684 B2
• Filed: 10/23/2015
• Issued: 02/06/2018
• Est. Priority Date: 10/23/2014
• Status: Active Grant

• Current Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Original Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Inventors: Drew, Dale, Whalen, Jr., Patrick Thomas
• Primary Examiner(s): Ijaz, Muhammad
• Application Number:
  US14/921,147
• Publication Number:
  US 20160114893A1
• Time in Patent Office: 837 Days
• Field of Search: 2441186, 297 1, 297313, 297317, 297322, 297326, 297327, 297335, 29734422, 248394-397, 248419
• CPC Class Codes: B60N 2/10 tiltable B60N2/12 , B60N2/2875 take precedence
• CPC Class Codes: B60N 2/1835 pivoting about an axis located in the front
• CPC Class Codes: B60N 2/1885 with weight compensating means
• CPC Class Codes: B60N 2/1892 characterised by a lock
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats
• CPC Class Codes: B64D 11/0696 Means for fastening seats to floors, e.g. to floor rails

Abstract

The disclosed embodiments relate to an aircraft having an in-flight leveling system for a seat onboard the aircraft that includes a swivel mechanism providing selective rotational movement of the a rear portion of the seat to compensate for an angle of inclination of the aircraft during flight. A locking mechanism is coupled to the swivel mechanism to retain the seat in a first position for use on the ground and a second position for use during flight. An actuator moves the locking mechanism between a locked condition and an unlocked condition permitting the seat to move between the first position to the second position enabling the seat to be substantially level when the aircraft is on the ground and during flight.

Claims

1. An in-flight leveling system for a seat onboard an aircraft, the seat having a seat cushion and a seat back and the aircraft traveling at an angle of inclination during flight, comprising:

a swivel mechanism having a front pivot point and providing selective arcuate movement of an aft portion of the seat to compensate for the angle of inclination of the aircraft during the flight, the swivel mechanism comprising;

a front pivot rod extending between a pair of spaced apart support base risers;

a rear slide rod extending between the pair of spaced apart support base risers and guided by arcuate slots formed in the pair of spaced apart support base risers; and

a sector pivotally coupled to one of the pair of spaced apart support base risers, the sector having an arcuate toothed rack and an opening for receiving the rear slide rod;

a locking mechanism coupled to the swivel mechanism to retain the seat in a first position and a second position the locking mechanism comprising a pawl having teeth to selectively engage the arcuate toothed rack of the sector; and

an actuator for moving the locking mechanism between a locked condition and an unlocked condition permitting the aft portion of the seat to move between the first position to the second position the actuator comprising a lever causing a cam to move the pawl toward or away from the arcuate toothed rack of the sector;

whereby, the actuator moves the locking mechanism from the locked condition to the unlocked condition permitting the aft portion of the seat to move from the first position to the second position to remain substantially level during the flight due to the swivel mechanism compensating for the angle of inclination of the aircraft during the flight.

2. The in-flight leveling system for the seat onboard the aircraft during flight of claim 1, further comprising a piston coupled to the swivel mechanism to bias the aft portion of the seat from the first position toward the second position.

3. The in-flight leveling system for the seat onboard the aircraft during flight of claim 1, wherein the angle of inclination of the aircraft during the flight is approximately 3-4.5 degrees.

4. The in-flight leveling system for the seat onboard the aircraft during flight of claim 1, wherein the aft portion of the seat is raised approximately one-half inch in the second position relative to the first position.

5. An in-flight leveling system for a seat onboard an aircraft, the seat having a seat cushion and a seat back and the aircraft traveling at an angle of inclination during flight, comprising:

a pair of spaced apart support base risers;

a front pivot rod extending between the pair of spaced apart support base risers, the front pivot rod facilitating a front portion of the seat to selectively pivot;

a rear slide rod extending between the pair of spaced apart support base risers and guided by arcuate slots formed in the pair of spaced apart support base risers, the rear slide rod moving in the arcuate slots between a first position and a second position causing a rear portion the seat to rise when the rear slide rod moves from the first position toward the second position;

a track and swivel assembly coupled to the front pivot rod and the rear slide rod;

a sector pivotally coupled to one of the pair of spaced apart support base risers, the sector having an arcuate toothed rack and an opening for receiving the rear slide rod;

a locking mechanism coupled adjacent to the sector for selectively engaging the arcuate toothed rack; and

an actuator for moving the locking mechanism between a locked condition and an unlocked condition permitting the rear slide rod to move within the arcuate slots between the first position and the second position;

whereby, the actuator moves the locking mechanism from the locked condition to the unlocked condition permitting the rear slide rod to move from the first position to the second position raising the rear portion of the seat to be substantially level during the flight in the second position.

6. The in-flight leveling system for the seat onboard the aircraft during flight of claim 5, further comprising a piston coupled to the sector for biasing the sector and the rear slide rod to move within the arcuate slots from the first position to the second position.

7. The in-flight leveling system for the seat onboard the aircraft during flight of claim 5, wherein the locking mechanism comprises a pawl having teeth to selectively engage the arcuate toothed rack of the sector.

8. The in-flight leveling system for the seat onboard the aircraft during flight of claim 5, wherein the actuator for moving the locking mechanism comprises a lever causing a cam to move a pawl toward or away from the arcuate toothed rack of the sector.

9. The in-flight leveling system for the seat onboard the aircraft during flight of claim 5, wherein the second position compensates for the angle of inclination of the aircraft during the flight of approximately 3-4.5 degrees.

10. The in-flight leveling system for the seat onboard the aircraft during flight of claim 5, wherein the rear portion of the seat is raised approximately one-half inch in the second position as compared to the first position.

11. An in-flight leveling system for a seat onboard an aircraft, the seat having a seat cushion and a seat back and the aircraft traveling at an angle of inclination during flight, comprising:

a pair of spaced apart support base risers;

a front pivot rod extending between the pair of spaced apart support base risers;

a rear slide rod extending between the pair of spaced apart support base risers and guided by arcuate slots formed in the pair of spaced apart support base risers;

a seat mount coupled to the front pivot rod and the rear slide rod configured to selective permit a front portion of the seat to pivot about the front pivot rod and a rear portion of the seat to arcuately rise from a first position to a second position;

a sector pivotally coupled to one of the pair of spaced apart support base risers, the sector having an arcuate toothed rack and an opening for receiving the rear slide rod;

a locking mechanism coupled adjacent to the sector for selectively engaging the arcuate toothed rack;

an actuator for moving the locking mechanism between a locked condition and an unlocked condition permitting the rear slide rod to move within the arcuate slots between a first position and a second position;

whereby, the actuator moves the locking mechanism from the locked condition to the unlocked condition permitting the rear slide rode to move from the first position to the second position arcuately raising the rear portion of the seat to be substantially level during the flight in the second position.

12. The in-flight leveling system for the seat onboard the aircraft during flight of claim 11, further comprising a piston coupled to the sector for biasing the sector and the rear slide rod to move within the arcuate slots from the first position to the second position.

13. The in-flight leveling system for the seat onboard the aircraft during flight of claim 11, wherein the locking mechanism comprises a pawl having teeth to selectively engage the arcuate toothed rack of the sector.

14. The in-flight leveling system for the seat onboard the aircraft during flight of claim 11, wherein the actuator mechanism comprises a lever causing a cam to move a pawl toward or away from the arcuate toothed rack of the sector.

15. The in-flight leveling system for the seat onboard the aircraft during flight of claim 11, wherein the second position compensates for the angle of inclination of the aircraft during the flight of approximately 3-4.5 degrees.