IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0628171
(2000-07-31)
|
발명자
/ 주소 |
- Brundrett, Robert L.
- Mascarella, Stephen A.
- Corio, Lawrence F.
- Christ, Franklin C.
|
출원인 / 주소 |
- The B. F. Goodrich Company
|
대리인 / 주소 |
Renner, Otto, Boisselle & Sklar, LLP
|
인용정보 |
피인용 횟수 :
3 인용 특허 :
9 |
초록
▼
An electrically actuated aircraft brake and method characterized by the use actuator modules which can be easily and quickly replaced as a unit. Quick and easy replacement of the actuator modules can be effected without disassembly of the overall brake and wheel assembly. Accordingly, brake manufact
An electrically actuated aircraft brake and method characterized by the use actuator modules which can be easily and quickly replaced as a unit. Quick and easy replacement of the actuator modules can be effected without disassembly of the overall brake and wheel assembly. Accordingly, brake manufacturing, repair costs, overhaul, parts stocking and maintenance costs and requirements are minimized and/or greatly simplified compared to integrated brake designs used in the prior art. Also, a malfunctioning actuator module on an aircraft can be replaced and preferably quickly enough to allow the aircraft to remain in scheduled service and/or with a minimum of downtime.
대표청구항
▼
An electrically actuated aircraft brake and method characterized by the use actuator modules which can be easily and quickly replaced as a unit. Quick and easy replacement of the actuator modules can be effected without disassembly of the overall brake and wheel assembly. Accordingly, brake manufact
An electrically actuated aircraft brake and method characterized by the use actuator modules which can be easily and quickly replaced as a unit. Quick and easy replacement of the actuator modules can be effected without disassembly of the overall brake and wheel assembly. Accordingly, brake manufacturing, repair costs, overhaul, parts stocking and maintenance costs and requirements are minimized and/or greatly simplified compared to integrated brake designs used in the prior art. Also, a malfunctioning actuator module on an aircraft can be replaced and preferably quickly enough to allow the aircraft to remain in scheduled service and/or with a minimum of downtime. ding away from the plank at an approximate 90° angle with the first flange, said second flange having a plane parallel with the plane of the plank lower surface, said second flange terminates in a third flange extending upwardly away from the second flange at an approximate 90° angle, said third flange having a plane parallel with the plane of the first flange, said three flanges forming a rectangular channel with the first and third flanges forming vertical sides, the second flange forming a horizontal bottom, and the channel having an open top, said second long edge first flange having an elongated, horizontal, central aperture formed therein, said aperture having a longitudinal axis parallel to the longitudinal axis of the plank, said second long edge third flange having an elongated, horizontal, central aperture formed therein, said aperture having a longitudinal axis parallel to the longitudinal axis of the plank, said apertures being parallel to each other; a back support attached to said plank assembly, comprising: a lower engagement portion comprising: a rectangular box having a top surface, bottom surface, two interconnecting, opposing parallel sides, and two opposing, parallel ends, said ends defining a box longitudinal axis, said box longitudinal axis being parallel to the longitudinal axis of the plank, wherein the box is adapted to fit into the said plank assembly channel, said box sides being positioned adjacent the second long edge first and third flanges, said box bottom surface being adjacent the second long edge second flange; and a plurality of side pins extending through each of the box sides, said side pins protruding from the sides and engaging the second long edge first and third flange apertures; an upper portion comprised of: a vertical post extending upwardly from the lower engagement portion box top surface; a sleeve slidably affixed to said post; a curved waist grip attached to the sleeve. 2. A safety ladder scaffold as recited in claim 1, further comprising: a plurality of pin apertures formed in said post; a locking pin adapted to being inserted through said sleeve and engaging one of said pin apertures. 3. A safety ladder scaffold as recited in claim 2, further comprising: a brake assembly comprised of an elongated arm pivotally attached to the post, said elongated arm having a bottom terminating in a spike adapted for engagement with one of a plurality of holes formed in the second long edge third flange beneath the elongated aperture. 4. A safety ladder scaffold as recited in claim 3, wherein: said metallic plank is made from aluminum. 5. A safety ladder scaffold in combination with and attached to a pair of ladders by a ladder jack installed on each ladder, said ladder jacks adapted for supporting the scaffold in an elevated horizontal position intermediate the two spaced apart ladders resting on the ground and leaning against a generally flat wall surface, comprising: a plank assembly attached to said ladder jacks, said plank assembly comprising: a rectangular plank having an upper surface and a lower surface, said surfaces adapted to be lying in planes positioned horizontally and parallel with respect to the ground, said plank having a first long edge and a second long edge, said first long edge adapted to be nearest to the wall surface, said plank having a first lateral end opposite a second lateral end, said lateral ends defining a longitudinal axis of the plank, said plank longitudinal axis adapted to be lying horizontally parallel to said wall surface; an elongated, rectangular box fixedly attached to the plank lower surface, along and adjacent to the plank second long edge, said rectangular box having a top side attached to the plank lower surface, an opposite bottom side, a first open side, an opposite second side, said second side having an elongated, horizontal aperture formed therein, a first end and an opposite second end, said ends defining
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